command: 
 ./cs_solver --param HPC.xml --mpi

***************************************************************

                                  (R)
                      Code_Saturne

                      Version 4.0.8


  Copyright (C) 1998-2016 EDF S.A., France

  revision 4.0.8
  build Fri 18 Aug 2017 18:24:24 BST
  MPI version 3.0 (Open MPI 1.8.8)


  The Code_Saturne CFD tool  is free software;
  you can redistribute it and/or modify it under the terms
  of the GNU General Public License as published by the
  Free Software Foundation; either version 2 of the License,
  or (at your option) any later version.

  The Code_Saturne CFD tool is distributed in the hope that
  it will be useful, but WITHOUT ANY WARRANTY; without even
  the implied warranty of MERCHANTABILITY or FITNESS FOR A
  PARTICULAR PURPOSE.  See the GNU General Public License
  for more details.

***************************************************************


Local case configuration:

  Date:                Sat 02 Sep 2017 01:03:33 BST
  System:              Linux 2.6.32-696.3.2.el6.x86_64
  Machine:             node190
  Processor:           model name	: Intel(R) Xeon(R) CPU E5-2650 v2 @ 2.60GHz
  Memory:              64497 MB
  User:                mep16kc (K. Chinembiri)
  Directory:           /data/mep16kc/HRN_RSM_MODEL/Case_1/RESU/20170902-0059
  MPI ranks:           130 (appnum attribute: 0)
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)
  I/O rank step:        1

  External libraries for partitioning:
    PT-SCOTCH 6.0.3

 Reading metadata from file: "mesh_input/mesh_01"
 Reading metadata from file: "mesh_input/mesh_02"
 Reading metadata from file: "mesh_input/mesh_03"
 Reading metadata from file: "mesh_input/mesh_04"

===============================================================

                   CALCULATION PREPARATION
                   =======================


 ===========================================================




 No error detected during the data verification
                          cs_user_parameters.f90 and others).


 ===========================================================

               CALCULATION PARAMETERS SUMMARY
               ==============================

 -----------------------------------------------------------


 ** DIMENSIONS
    ----------

 --- Physics
       NVAR   =             12 (Nb variables                )
       NSCAL  =              1 (Nb scalars                  )
       NSCAUS =              0 (Nb user scalars             )
       NSCAPP =              1 (Nb specific physics scalars )
       NPROCE =              7 (Nb cell properties          )


 -----------------------------------------------------------


 ** PHYSICAL PROPERTIES
    -------------------

       GX     =    0.00000E+00 (Gravity x component         )
       GY     =    0.00000E+00 (Gravity y component         )
       GZ     =    0.00000E+00 (Gravity z component         )

       ICORIO =          0 (Coriolis source terms       )

  -- Continuous phase:

       RO0    =    0.39268E+02 (Reference density           )
       VISCL0 =    0.23144E-04 (Ref. molecular dyn. visc.   )
       CP0    =    0.10970E+04 (Ref. specific heat          )
       ICP    =              7 (> 0: variable CP (usphyv)   )
       P0     =    0.35000E+07 (Ref. total pressure         )
       PRED0  =    0.00000E+00 (Ref. reduced pressure       )
       T0     =    0.29315E+03 (Ref. temperature            )

       IROVAR =              1 (Density constant(0) or not(1)
       IVIVAR =              1 (Molec. visc cst.(0) or not(1)

       Initial reference point for pressure
       XYZP0  =    0.00000E+00   0.00000E+00   0.00000E+00

 -----------------------------------------------------------


 ** HOMOGENEOUS MIXTURE MODEL FOR CAVITATION
    ----------------------------------------

       ICAVIT =             -1 (-1: single phase flow       )
                               ( 0: no vap./cond. model     )
                               ( 1: Merkle's model        )


 -----------------------------------------------------------


 ** THERMAL MODEL
    -------------
 --- Continuous phase:

   - Commons
       ITHERM =              1 (0: no thermal model         )
                               (1: temperature              )
                               (2: enthalpy                 )
                               (3: total energy             )
       ITPSCL =              2 (0: none                     )
                               (1: temperature in Kelvin    )
                               (2: temperature in Celsius   )
       ISCALT =              1 (Thermal scalar number       )


 ** TURBULENCE
    ----------

 --- Continuous phase:

   - Commons
       ITURB  =             31 (Turbulence model            )
       IDEUCH =              2 (0: one-scale model          )
                               (1: two-scale model          )
                               (2: invariant wall function  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.10880E+02 (Limit Y+                    )
       ILOGPO =              1 (0: power law (forbidden for
                                              k-epsilon)    )
                               (1: one-scale log law        )
       IGRHOK =              0 (1: computed Grad(rho k)     )

   - SSG Rij-epsilon     (ITURB = 31)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       IRIJNU =              0 (Matrix stabilization        )
       IRIJRB =              0 (Reconstruct at boundaries   )
       IGRARI =              0 (Account for gravity         )
       ICLSYR =              1 (Symmetry implicitation      )
       ICLPTR =              0 (Wall implicitation          )

 --- Constants

   - Commons
       XKAPPA =    0.42000E+00 (Von Karman constant         )
       CSTLOG =    0.52000E+01 (U+=Log(y+)/kappa +CSTLOG    )
       APOW   =    0.83000E+01 (U+=APOW (y+)**BPOW (W&W law))
       BPOW   =    0.14286E+00 (U+=APOW (y+)**BPOW (W&W law))

   - SSG Rij-epsilon     (ITURB = 31)
       CSSGS1 =    0.17000E+01 (Cs1 coeff.                  )
       CSSGS2 =   -0.10500E+01 (Cs2 coeff.                  )
       CSSGR1 =    0.90000E+00 (Cr1 coeff.                  )
       CSSGR2 =    0.80000E+00 (Cr2 coeff.                  )
       CSSGR3 =    0.65000E+00 (Cr3 coeff.                  )
       CSSGR4 =    0.62500E+00 (Cr4 coeff.                  )
       CSSGR5 =    0.20000E+00 (Cr5 coeff.                  )
       CSRIJ  =    0.22000E+00 (Rij Cs diffusion coeff.     )
       CRIJ3  =    0.55000E+00 (Gravity term coeff.         )
       Ce1    =    0.14400E+01 (Ceps1 coeff.                )
       CSSGE2 =    0.18300E+01 (Ceps2 coeff.                )
       SIGMAE =    0.12200E+01 (sigma_eps coeff.            )
       CMU    =    0.90000E-01 (Cmu constant                )


 -----------------------------------------------------------


 ** SECONDARY VISCOSITY
    -------------------

 --- Continuous phase:
       IVISSE =              1 (1: accounted for            )


 -----------------------------------------------------------


 ** TIME STEPPING
    -------------

    UNSTEADY ALGORITHM

 --- Time step parameters

       IDTVAR =              2 (0 cst; 1,2 var (t, t-space  )
       IPTLRO =              0 (1: rho-related DT clipping  )
       COUMAX =    0.60000E+00 (Maximum target CFL          )
       FOUMAX =    0.10000E+02 (Maximum target Fourier      )
       VARRDT =    0.10000E+00 (For var. DT, max. increase  )
       DTMIN  =    0.10000E-06 (Minimum time step           )
       DTMAX  =    0.10000E-02 (Maximum time step           )
       DTREF  =    0.10000E-05 (Reference time step         )

       With a non-constant time step (IDTVAR = 1 or 2),
         when the value of COUMAX or FOUMAX is negative
         or zero, the associated time step limitation (for
         CFL and Fourier respectively) is ignored.

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

------------------------------------
 Variable          ISTAT      CDTVAR
------------------------------------
 Velocity              1  0.1000E+01
 Pressure              0  0.1000E+01
 r11                   1  0.1000E+01
 r22                   1  0.1000E+01
 r33                   1  0.1000E+01
 r12                   1  0.1000E+01
 r13                   1  0.1000E+01
 r23                   1  0.1000E+01
 epsilon               1  0.1000E+01
 TempC                 1  0.1000E+01
----------------------------

       ISTAT  =  0 ou  1       (1 for unsteady              )
       CDTVAR >  0             (time step multiplier        )

 --- Order of base time stepping scheme
       ISCHTP =              1 (1: order 1; 2: order 2      )
                                                             

 -----------------------------------------------------------


 ** CONVECTION - DIFFUSION
    ----------------------

---------------------------------------------------------------------
 Variable          ICONV  IDIFF IDIFFT ISCHCV ISSTPC   BLENCV  THETAV
---------------------------------------------------------------------
 Velocity              1      1      1      0      0 0.10E+01 0.10E+01
 Pressure              0      1      1      1      0 0.00E+00 0.10E+01
 r11                   1      1      1      1      0 0.00E+00 0.10E+01
 r22                   1      1      1      1      0 0.00E+00 0.10E+01
 r33                   1      1      1      1      0 0.00E+00 0.10E+01
 r12                   1      1      1      1      0 0.00E+00 0.10E+01
 r13                   1      1      1      1      0 0.00E+00 0.10E+01
 r23                   1      1      1      1      0 0.00E+00 0.10E+01
 epsilon               1      1      1      1      0 0.00E+00 0.10E+01
 TempC                 1      1      1      0      0 0.10E+01 0.10E+01
-------------------------------------------------------------

       ICONV  =  0 ou  1       (1 for convection active     )
       IDIFF  =  0 ou  1       (1 for total diffusion active)
       IDIFFT =  0 ou  1       (1 for turbulent diff. active)
       ISCHCV =  0 ou  1       (SOLU or CD                  )
       ISSTPC =  0 ou  1       (1: no slope test            )
       BLENCV =  [0.;1.]       (1-upwind proportion         )
       THETAV =  [0.;1.]       (0.5 Crank-Nicolson/AB       )
                               (theta for convection-       )
                               (diffusion terms uses        )
                               ((1-theta).old+theta.new     )


 -----------------------------------------------------------


 ** STOKES
    ------
       IDILAT =              1 (1 : without unsteady term
                                    in the continuity equation
                                2 : with unsteady term in 
                                    the continuity equation)
       IPOROS =              0 (0 : without porous media
                                1 : with porous media)
       IPHYDR =              0 (1: account for explicit
                                   balance between pressure
                                   gradient, gravity source
                                   terms, and head losses     )
       ICALHY =              0 (1: compute hydrastatic
                                   pressure for Dirichlet
                                   conditions for pressure
                                   on outlet                  )
       IPRCO  =              1 (1: pressure-continuity        )
       IPUCOU =              0 (1: reinforced U-P coupling    )
       NTERUP =              5 (n: n sweeps on navsto for
                                   velocity/pressure coupling )

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

       RELAXV =    0.40000E+00 for pressure (relaxation)
       ARAK   =    0.10000E+01 (Arakawa factor              )

       ISTMPF =              1 (time scheme for flow
                               (0: explicit (THETFL = 0     )
                               (1: std scheme (Saturne 1.0  )
                               (2: 2nd-order (THETFL = 0.5  )
       THETFL =   -0.99900E+03 (theta for mass flow         )
       IROEXT =              0 (density extrapolation
                               (0: explicit
                               (1: n+thetro with thetro=1/2
                               (2: n+thetro with thetro=1
       THETRO =    0.00000E+00 (theta for density
                               ((1+theta).new-theta.old
       IVIEXT =              0 (total viscosity extrapolation
                               (0: explicit
                               (1: n+thetvi with thetro=1/2
                               (2: n+thetvi with thetro=1
       THETVI =    0.00000E+00 (theta for total viscosity
                               ((1+theta).new-theta.old
       ICPEXT =              0 (specific heat extrapolation
                               (0: explicit
                               (1: n+thetcp with thetro=1/2
                               (2: n+thetcp with thetro=1
       THETCP =    0.00000E+00 (specific heat theta-scheme
                               ((1+theta).new-theta.old
       THETSN =    0.00000E+00 (Nav-Stokes S.T. theta scheme)
                               ((1+theta).new-theta.old
       THETST =    0.00000E+00 (Turbulence S.T. theta-scheme)
                               ((1+theta).new-theta.old
       EPSUP  =    0.10000E-04 (Velocity/pressure coupling
                                stop test                   )


 -----------------------------------------------------------


 ** GRADIENTS CALCULATION
    ---------------------

       IMRGRA =             -2 (Reconstruction mode         )
       ANOMAX =    0.78540E+00 (Non-ortho angle: limit for  )
                               (least squares ext. neighbors)

-------------------------------------------------------------------
 Variable         NSWRGR NSWRSM      EPSRGR      EPSRSM      EXTRAG
-------------------------------------------------------------------
 Velocity            100      2  0.1000E-04  0.1000E-06  0.0000E+00
 Pressure            100      2  0.1000E-04  0.1000E-04  0.0000E+00
 r11                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 r22                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 r33                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 r12                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 r13                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 r23                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 epsilon             100      1  0.1000E-04  0.1000E-06  0.0000E+00
 TempC               100      2  0.1000E-04  0.1000E-06  0.0000E+00
-----------------------------------------------------------

-------------------------------------------
 Variable         IRCFLU IMLIGR      CLIMGR
-------------------------------------------
 Velocity              1      1  0.1500E+01
 Pressure              1      1  0.1500E+01
 r11                   0      1  0.1500E+01
 r22                   0      1  0.1500E+01
 r33                   0      1  0.1500E+01
 r12                   0      1  0.1500E+01
 r13                   0      1  0.1500E+01
 r23                   0      1  0.1500E+01
 epsilon               0      1  0.1500E+01
 TempC                 1      1  0.1500E+01
-----------------------------------

       NSWRGR =                (nb sweep gradient reconstr. )
       NSWRSM =                (nb sweep rhs reconstrcution )
       EPSRGR =                (grad. reconstruction prec.  )
       EPSRSM =                (rhs   reconstruction prec.  )
       EXTRAG =  [0.;1.]       (gradients extrapolation     )
       IRCFLU =  0 ou  1       (flow reconstruction         )
       IMLIGR =  < 0, 0 ou 1   (gradient limitation method  )
       CLIMGR =  > 1 ou 1      (gradient limitation coeff.  )


 -----------------------------------------------------------


 ** FACE INTERPOLATION
    ------------------
       IMVISF =              0 (0 arithmetic                )


 -----------------------------------------------------------


 ** BASE ITERATIVE SOLVERS
    ----------------------

------------------------------------
 Variable              EPSILO IDIRCL
------------------------------------
 Velocity          0.1000E-07      1
 Pressure          0.1000E-05      1
 r11               0.1000E-07      1
 r22               0.1000E-07      1
 r33               0.1000E-07      1
 r12               0.1000E-07      1
 r13               0.1000E-07      1
 r23               0.1000E-07      1
 epsilon           0.1000E-07      1
 TempC             0.1000E-07      1
------------------------------------

       IRESOL =            -1  (automatic solver choice     )
                IPOL*1000 + 0  (p conjuguate gradient       )
                            1  (Jacobi                      )
                IPOL*1000 + 2  (bicgstab                    )
                  avec IPOL    (preconditioning degree      )
       NITMAX =                (max number of iterations    )
       EPSILO =                (resolution precision        )
       IDIRCL = 0 ou 1         (shift diagonal if   
                                ISTAT=0 and no Dirichlet    )


 -----------------------------------------------------------


 ** SCALARS
    -------

       ITBRRB =              0 (T or H reconstruction at bdy)

-------------------------------------------------------------
 Variable         Number ISCACP ITURT      VISLS0      SIGMAS
-------------------------------------------------------------
 TempC                 1      1      0  0.3700E-01  0.1000E+01
---------------------------------------------------------------------

------------------------------------
 Variable         Number      RVARFL
------------------------------------
 TempC                 1  0.8000E+00
-------------------------------------------

-------------------------------------------------------
 Variable         Number ICLVFL      SCAMIN      SCAMAX
-------------------------------------------------------
 TempC                 1     -1 -0.2731E+03  0.1000E+13
-------------------------------------------------------

-------------------------------------------------------------

       For each scalar, the number indicates it's rank
         in the list of all scalars. User scalars are placed
         first, from 1 to NSCAUS. Specific physics scalars
         are placed at the end, from
         NSCAUS+1 to NSCAPP+NSCAUS=NSCAL.

       ISCACP = 0 or 1     2   (use Cp or not               )
       VISLS0 = >0             (Reference viscosity         )
       SIGMAS = >0             (Schmidt                     )
       RVARFL = >0             (Rf, cf variance dissipation )
       ICLVFL = 0, 1 or 2      (Variance clipping mode      )
       SCAMIN =                (Min authorized value        )
       SCAMAX =                (Max authorized value        )
        For variances, SCAMIN is ignored and SCAMAX is used
          only if ICLVFL = 2

------------------------------------------------------
   Scalar        THETSS    IVSEXT      THETVS
------------------------------------------------------
          1  0.0000E+00         0  0.0000E+00
------------------------------------------------------

       THETSS =                (theta for source terms      )
                               ((1+theta).new-theta.old     )
       IVSEXT =                (extrap. total viscosity     )
                               (0: explicit                 )
                               (1: n+thetvs with thetvs=1/2 )
                               (2: n+thetvs with thetvs=1   )
       THETVS =                (theta for scalar diffusivity
                               ((1+theta).new-theta.old     )


 -----------------------------------------------------------


 ** CALCULATION MANAGEMENT
    ----------------------

 --- Restarted calculation
       ISUITE =              1 (1: restarted calculation    )
       ILEAUX =              1 (1: read  restart/auxiliary  )
       IECAUX =              1 (1: write checkpoint/auxiliary)


 --- Calculation time
     The numbering of time steps and the measure of simulated
       physical time are absolute values, and not values
       relative to the current calculation.

       INPDT0 =              0 (1: 0 time step calcuation   )
       NTMABS =          20000 (Final time step required    )

 --- CPU time margin
       TMARUS =   -0.10000E+01 (CPU time margin before stop )


 -----------------------------------------------------------


 ** INPUT-OUTPUT
    ------------

 --- Restart file
       NTSUIT =              0 (Checkpoint frequency )

 --- Post-processed variables


Velocity
Pressure
r11
r22
r33
r12
r13
r23
epsilon
TempC
Density
Boundary Density
LamVisc
TurbVisc
CourantNb
FourierNb
total_pressure
SpecHeat
Local Time Step
ThermalCond
         --           --

 --- Probe history files
       NTHIST =              1 (Output frequency     )
       FRHIST =     -.10000E+01 (Output frequency (s) )
       NCAPT  =             25 (Number of probes     )
       NTHSAV =             -1 (Checkpoint frequency )

       Number Name                  Nb. probes (-1: all)
         2 Velocity[X]                   -1
         3 Velocity[Y]                   -1
         4 Velocity[Z]                   -1
         5 Pressure                      -1
         6 r11                           -1
         7 r22                           -1
         8 r33                           -1
         9 r12                           -1
        10 r13                           -1
        11 r23                           -1
        12 epsilon                       -1
        13 TempC                         -1
        14 Density                       -1
        15 LamVisc                       -1
        16 TurbVisc                      -1
        17 CourantNb                     -1
        18 FourierNb                     -1
        19 total_pressure                -1
        20 SpecHeat                      -1
        21 Local Time Step               -1
        22 ThermalCond                   -1
         --           --                --

 --- Log files
       NTLIST =              1 (Output frequency     )

       Number Name                IWARNI verbosity level
                                      (-999: not applicable)

         2 Velocity                       0
         5 Pressure                       0
         6 r11                            0
         7 r22                            0
         8 r33                            0
         9 r12                            0
        10 r13                            0
        11 r23                            0
        12 epsilon                        0
        13 TempC                          0
        14 Density                     -999
        15 LamVisc                     -999
        16 TurbVisc                    -999
        17 CourantNb                   -999
        18 FourierNb                   -999
        19 total_pressure              -999
        20 SpecHeat                    -999
        21 Local Time Step             -999
        22 ThermalCond                 -999
         --           --                --

 --- Additional post-processing variables (ipstdv)
       ipstfo =              7 (Force exerted by the
                                     fluid on the boundary)
       ipstft =              1 (Thermal flux   at boundary)
       ipsttb =              1 (Temperature    at boundary)
       ipstnu =              0 (Dimensionless thermal
                                          flux at boundary)


 -----------------------------------------------------------


 ** ALE METHOD (MOVING MESH)
    -----------

       IALE   =              0 (1: activated                )
       NALINF =              0 (Fluid initialization
                                                  iterations)
       IFLXMW =              0 (ALE mass flux computation
                                0: thanks to vertices
                                1: thanks to mesh velocity)


 -----------------------------------------------------------


Postprocessing output writers:
------------------------------

  -1: name: results
      directory: postprocessing
      format: EnSight Gold
      options: binary
      time dependency: fixed mesh
      output: at calculation end

   1: name: writer(1)
      directory: postprocessing
      format: EnSight Gold
      options: 
      time dependency: fixed mesh
      output: at calculation end

   2: name: writer(2)
      directory: postprocessing
      format: EnSight Gold
      options: 
      time dependency: fixed mesh
      output: at calculation end


 Reading file:        mesh_input/mesh_01
 Finished reading:    mesh_input/mesh_01

 Reading file:        mesh_input/mesh_02
 Finished reading:    mesh_input/mesh_02

 Reading file:        mesh_input/mesh_03
 Finished reading:    mesh_input/mesh_03

 Reading file:        mesh_input/mesh_04
 Finished reading:    mesh_input/mesh_04
 No "partition_input/domain_number_130" file available;

 ----------------------------------------------------------

 Partitioning by space-filling curve: Morton (in bounding box).
  Number of cells per domain (histogramm):
    [      89172 ;      89173 ] =        130

 Partitioning finished (24.4 s)


 -------------------------------------------------------
  Joining number 1:

  Selection criteria: "OUTLET_1 or INLET_2"

  Parameters for the joining operation:
    Shortest incident edge fraction:           0.10000
    Maximum angle between joined face planes: 25.00000

  Advanced joining parameters:
    Verbosity level:                                 1
    Visualization level:                             1
    Deepest level reachable in tree building:       30
    Max boxes by leaf:                              25
    Max ratio of linked boxes / init. boxes:   5.00000
    Max ratio of boxes for distribution:       2.00000
    Merge step tolerance multiplier:           1.00000
    Pre-merge factor:                          0.05000
    Tolerance computation mode:                      1
    Intersection computation mode:                   1
    Max. number of equiv. breaks:                  500
    Max. number of subfaces by face:               200

  Before joining
     Number of cells:          11592377
     Number of interior faces: 25589139
     Number of boundary faces: 545368
     Number of vertices:       4282991

  Global number of boundary faces selected for joining:      11224

  Global number of single vertices found:     16
  Global number of single edges found:        14

  Element selection successfully done.
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

    1368204 |    0.000022 |  5.0084061018e-03   6.4104674806e-03   2.0000000000e+00 | ORI
    2701839 |    0.000174 |  4.1973208668e-02   4.2100525484e-02   2.0000000000e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 2D

  Global number of intersections detected:       258426
    Vertex-Vertex intersections:          258426
    Other intersections:                       0

  Joining operation is conforming.

  Edge intersections and vertex creation done.

  Pre-merge for 16592 global element couples.

  Max size of a merge set of vertices: 2

  Excessive transitivity for 0 set(s) of vertices.

  Synchronization of the "single" elements after the merge step.

  Edge removed for 0 faces (global).
  Join mesh cleaning done.

  Edge removed for 0 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

  Global number of faces after splitting:       5612

  Global configuration after the joining operation:
     Global number of border faces to add:          0

  Mesh cleaning done for degenerate faces.
    Global number of cleaned interior faces:        0
    Global number of cleaned border faces:          0

  After joining
     Number of cells:          11592377
     Number of interior faces: 25594751
     Number of boundary faces: 534144
     Number of vertices:       4278984


  Joining  1 completed (6.48 s).

 -------------------------------------------------------
  Joining number 2:

  Selection criteria: "OUTLET_2 or INLET_3"

  Parameters for the joining operation:
    Shortest incident edge fraction:           0.10000
    Maximum angle between joined face planes: 25.00000

  Advanced joining parameters:
    Verbosity level:                                 1
    Visualization level:                             1
    Deepest level reachable in tree building:       30
    Max boxes by leaf:                              25
    Max ratio of linked boxes / init. boxes:   5.00000
    Max ratio of boxes for distribution:       2.00000
    Merge step tolerance multiplier:           1.00000
    Pre-merge factor:                          0.05000
    Tolerance computation mode:                      1
    Intersection computation mode:                   1
    Max. number of equiv. breaks:                  500
    Max. number of subfaces by face:               200

  Before joining
     Number of cells:          11592377
     Number of interior faces: 25594751
     Number of boundary faces: 534144
     Number of vertices:       4278984

  Global number of boundary faces selected for joining:      10164

  Global number of single vertices found:     32
  Global number of single edges found:        34

  Element selection successfully done.
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

    1360702 |    0.000013 |  5.0445467954e-03   8.1018128135e-03   2.5000000000e+00 | ORI
      70828 |    0.000179 |  7.4855220770e-02   2.8503858338e-02   2.5000000000e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 2D

  Global number of intersections detected:       229388
    Vertex-Vertex intersections:          229388
    Other intersections:                       0

  Joining operation is conforming.

  Edge intersections and vertex creation done.

  Pre-merge for 12856 global element couples.

  Max size of a merge set of vertices: 2

  Excessive transitivity for 0 set(s) of vertices.

  Synchronization of the "single" elements after the merge step.

  Edge removed for 0 faces (global).
  Join mesh cleaning done.

  Edge removed for 0 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

  Global number of faces after splitting:       5082

  Global configuration after the joining operation:
     Global number of border faces to add:          0

  Mesh cleaning done for degenerate faces.
    Global number of cleaned interior faces:        0
    Global number of cleaned border faces:          0

  After joining
     Number of cells:          11592377
     Number of interior faces: 25599833
     Number of boundary faces: 523980
     Number of vertices:       4275254


  Joining  2 completed (5.97 s).

 -------------------------------------------------------
  Joining number 3:

  Selection criteria: "OUTLET_3 or INLET_4"

  Parameters for the joining operation:
    Shortest incident edge fraction:           0.10000
    Maximum angle between joined face planes: 25.00000

  Advanced joining parameters:
    Verbosity level:                                 1
    Visualization level:                             1
    Deepest level reachable in tree building:       30
    Max boxes by leaf:                              25
    Max ratio of linked boxes / init. boxes:   5.00000
    Max ratio of boxes for distribution:       2.00000
    Merge step tolerance multiplier:           1.00000
    Pre-merge factor:                          0.05000
    Tolerance computation mode:                      1
    Intersection computation mode:                   1
    Max. number of equiv. breaks:                  500
    Max. number of subfaces by face:               200

  Before joining
     Number of cells:          11592377
     Number of interior faces: 25599833
     Number of boundary faces: 523980
     Number of vertices:       4275254

  Global number of boundary faces selected for joining:      11180

  Global number of single vertices found:     19
  Global number of single edges found:        18

  Element selection successfully done.
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

      22838 |    0.000022 |  5.0084061018e-03   6.4104674806e-03   3.0000000000e+00 | ORI
       4542 |    0.000180 |  5.7382201215e-02   1.5321108347e-02   3.0000000000e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 2D

  Global number of intersections detected:       245583
    Vertex-Vertex intersections:          245583
    Other intersections:                       0

  Joining operation is conforming.

  Edge intersections and vertex creation done.

  Pre-merge for 13188 global element couples.

  Max size of a merge set of vertices: 2

  Excessive transitivity for 0 set(s) of vertices.

  Synchronization of the "single" elements after the merge step.

  Edge removed for 0 faces (global).
  Join mesh cleaning done.

  Edge removed for 0 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

  Global number of faces after splitting:       5590

  Global configuration after the joining operation:
     Global number of border faces to add:          0

  Mesh cleaning done for degenerate faces.
    Global number of cleaned interior faces:        0
    Global number of cleaned border faces:          0

  After joining
     Number of cells:          11592377
     Number of interior faces: 25605423
     Number of boundary faces: 512800
     Number of vertices:       4271258


  Joining  3 completed (5.91 s).

  All joining operations successfully finished:

    Wall clock time:                  18.4


 ----------------------------------------------------------

 Halo construction with extended neighborhood
 ============================================

 Face interfaces creation
 Vertex interfaces creation
 Halo creation
 Halo definition
    Local halo definition
    Distant halo creation
    Updating the faces -> cells connectivity
 Extended neighborhood structures definition

 Histogram of the number of cells per rank:

    minimum value =              89172
    maximum value =              89173

      1 : [      89172 ;      89173 ] =        130

 ----------------------------------------------------------

 Histogram of the number of standard + halo cells per rank:

    minimum value =              96318
    maximum value =             188921

      1 : [      96318 ;     114838 [ =         10
      2 : [     114838 ;     133359 [ =         22
      3 : [     133359 ;     151879 [ =         36
      4 : [     151879 ;     170400 [ =         36
      5 : [     170400 ;     188921 ] =         26

 ----------------------------------------------------------

 Histogram of the number of ghost cells per rank:

    minimum value =               7146
    maximum value =              99748

      1 : [       7146 ;      25666 [ =         10
      2 : [      25666 ;      44186 [ =         22
      3 : [      44186 ;      62707 [ =         36
      4 : [      62707 ;      81227 [ =         36
      5 : [      81227 ;      99748 ] =         26

 Histogram of the number of ghost cells
 in the standard neighborhood per rank:

    minimum value =               4466
    maximum value =              37175

      1 : [       4466 ;      11007 [ =          4
      2 : [      11007 ;      17549 [ =         18
      3 : [      17549 ;      24091 [ =         30
      4 : [      24091 ;      30633 [ =         46
      5 : [      30633 ;      37175 ] =         32

 ----------------------------------------------------------

 Histogram of the number of interior faces per rank:

    minimum value =             188842
    maximum value =             249741

      1 : [     188842 ;     201021 [ =         39
      2 : [     201021 ;     213201 [ =         63
      3 : [     213201 ;     225381 [ =          8
      4 : [     225381 ;     237561 [ =          8
      5 : [     237561 ;     249741 ] =         12

 ----------------------------------------------------------

 Histogram of the number of boundary faces per rank:

    minimum value =                  0
    maximum value =              15618

      1 : [          0 ;       3123 [ =         63
      2 : [       3123 ;       6247 [ =         44
      3 : [       6247 ;       9370 [ =         17
      4 : [       9370 ;      12494 [ =          4
      5 : [      12494 ;      15618 ] =          2

 ----------------------------------------------------------

 Histogram of the number of interior faces per cell:

    minimum value =                  3
    maximum value =                  6

      1 : [          3 ;          4 [ =        160
      2 : [          4 ;          5 [ =    8119631
      3 : [          5 ;          6 ] =    3472586

 ----------------------------------------------------------

 Histogram of the number of neighboring domains per rank:

    minimum value =                  4
    maximum value =                 31

      1 : [          4 ;          9 [ =          8
      2 : [          9 ;         14 [ =         19
      3 : [         14 ;         20 [ =         58
      4 : [         20 ;         25 [ =         30
      5 : [         25 ;         31 ] =         15

 ----------------------------------------------------------

 Global definition of the number of elements (cells, vertices, faces...)
Synchronizing cell families

 Writing file:        mesh_output
 Finished writing:    mesh_output

 ----------------------------------------------------------

 Partitioning 11592377 cells to 130 domains on 130 ranks
   (SCOTCH_dgraphPart).

  wall-clock time: 224.165709 s

  Number of cells per domain (histogramm):
    [      85734 ;      86420 [ =          9
    [      86420 ;      87106 [ =         10
    [      87106 ;      87792 [ =         15
    [      87792 ;      88478 [ =         17
    [      88478 ;      89164 [ =         19
    [      89164 ;      89850 [ =         12
    [      89850 ;      90536 [ =         11
    [      90536 ;      91222 [ =         13
    [      91222 ;      91908 [ =         17
    [      91908 ;      92594 ] =          7

 Partitioning finished (225 s)

 ----------------------------------------------------------

 Halo construction with extended neighborhood
 ============================================

 Face interfaces creation
 Vertex interfaces creation
 Halo creation
 Halo definition
    Local halo definition
    Distant halo creation
    Updating the faces -> cells connectivity
 Extended neighborhood structures definition

 Histogram of the number of cells per rank:

    minimum value =              85734
    maximum value =              92594

      1 : [      85734 ;      87106 [ =         19
      2 : [      87106 ;      88478 [ =         32
      3 : [      88478 ;      89850 [ =         31
      4 : [      89850 ;      91222 [ =         24
      5 : [      91222 ;      92594 ] =         24

 ----------------------------------------------------------

 Histogram of the number of standard + halo cells per rank:

    minimum value =              94240
    maximum value =             111073

      1 : [      94240 ;      97606 [ =          5
      2 : [      97606 ;     100973 [ =         26
      3 : [     100973 ;     104339 [ =         59
      4 : [     104339 ;     107706 [ =         38
      5 : [     107706 ;     111073 ] =          2

 ----------------------------------------------------------

 Histogram of the number of ghost cells per rank:

    minimum value =               6713
    maximum value =              23566

      1 : [       6713 ;      10083 [ =         22
      2 : [      10083 ;      13454 [ =         38
      3 : [      13454 ;      16824 [ =         53
      4 : [      16824 ;      20195 [ =         15
      5 : [      20195 ;      23566 ] =          2

 Histogram of the number of ghost cells
 in the standard neighborhood per rank:

    minimum value =               2852
    maximum value =               8833

      1 : [       2852 ;       4048 [ =         13
      2 : [       4048 ;       5244 [ =         60
      3 : [       5244 ;       6440 [ =         46
      4 : [       6440 ;       7636 [ =          7
      5 : [       7636 ;       8833 ] =          4

 ----------------------------------------------------------

 Histogram of the number of interior faces per rank:

    minimum value =             180015
    maximum value =             245088

      1 : [     180015 ;     193029 [ =         72
      2 : [     193029 ;     206044 [ =         33
      3 : [     206044 ;     219058 [ =          0
      4 : [     219058 ;     232073 [ =          5
      5 : [     232073 ;     245088 ] =         20

 ----------------------------------------------------------

 Histogram of the number of boundary faces per rank:

    minimum value =                959
    maximum value =              12117

      1 : [        959 ;       3190 [ =         61
      2 : [       3190 ;       5422 [ =         40
      3 : [       5422 ;       7653 [ =          9
      4 : [       7653 ;       9885 [ =         17
      5 : [       9885 ;      12117 ] =          3

 ----------------------------------------------------------

 Histogram of the number of interior faces per cell:

    minimum value =                  3
    maximum value =                  6

      1 : [          3 ;          4 [ =        160
      2 : [          4 ;          5 [ =    8119631
      3 : [          5 ;          6 ] =    3472586

 ----------------------------------------------------------

 Histogram of the number of neighboring domains per rank:

    minimum value =                  4
    maximum value =                 13

      1 : [          4 ;          5 [ =          9
      2 : [          5 ;          7 [ =         48
      3 : [          7 ;          9 [ =         36
      4 : [          9 ;         11 [ =         30
      5 : [         11 ;         13 ] =          7

 ----------------------------------------------------------

 Global definition of the number of elements (cells, vertices, faces...)
Synchronizing cell families

 Renumbering mesh:

   renumbering for cells:
     pre-numbering:                       none
     cells adjacent to ghost cells last:  no
     numbering:                           none

   renumbering for interior faces:
     cell adjacency pre-ordering:         lowest id first
     faces adjacent to ghost cells last:  no
     numbering:                           none

   renumbering for boundary faces:
     numbering:                           none

 ----------------------------------------------------------

 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =              90328
    maximum value =             108902

      1 : [      90328 ;      94042 [ =          6
      2 : [      94042 ;      97757 [ =         21
      3 : [      97757 ;     101472 [ =         60
      4 : [     101472 ;     105187 [ =         36
      5 : [     105187 ;     108902 ] =          7

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =              15935
    maximum value =              45843

      1 : [      15935 ;      21916 [ =         27
      2 : [      21916 ;      27898 [ =          1
      3 : [      27898 ;      33879 [ =         21
      4 : [      33879 ;      39861 [ =         44
      5 : [      39861 ;      45843 ] =         37

 Mesh coordinates:               minimum    and maximum
                       X :  4.0675000e-03  9.6130000e-02
                       Y : -3.1260947e-18  8.3251022e-02
                       Z :  0.0000000e+00  3.0200000e+00
 Mesh
     Number of cells:          11592377
     Number of interior faces: 25605423
     Number of boundary faces: 512800
     Number of vertices:       4271258

 Groups:
    "ANCI_SYMMETRY_FACES_1"
       boundary faces:        32000
    "ANCI_SYMMETRY_FACES_2"
       boundary faces:        21600
    "ANCI_SYMMETRY_FACES_3"
       boundary faces:        21600
    "ANCI_SYMMETRY_FACES_4"
       boundary faces:          800
    "ANGLED_SYMMETRY_WALL_1"
       boundary faces:        12800
    "ANGLED_SYMMETRY_WALL_2"
       boundary faces:        10302
    "ANGLED_SYMMETRY_WALL_3"
       boundary faces:        10302
    "ANGLED_SYMMETRY_WALL_4"
       boundary faces:          320
    "GUIDETUBEWALL_1"
       boundary faces:         6000
    "GUIDETUBEWALL_2"
       boundary faces:         4050
    "GUIDETUBEWALL_3"
       boundary faces:         4050
    "GUIDETUBEWALL_4"
       boundary faces:          150
    "INLET_1"
       boundary faces:         5612
    "INLET_2"
       interior faces:         5612
    "INLET_3"
       interior faces:         5082
    "INLET_4"
       interior faces:         5590
    "LATERAL_SYMMETRY_WALL_1"
       boundary faces:        12800
    "LATERAL_SYMMETRY_WALL_2"
       boundary faces:        10302
    "LATERAL_SYMMETRY_WALL_3"
       boundary faces:        10302
    "LATERAL_SYMMETRY_WALL_4"
       boundary faces:          320
    "OUTLET_1"
       interior faces:         5612
    "OUTLET_2"
       interior faces:         5082
    "OUTLET_3"
       interior faces:         5590
    "OUTLET_4"
       boundary faces:         5590
    "PINWALL_1"
       boundary faces:       124800
    "PINWALL_2"
       boundary faces:        84240
    "PINWALL_3"
       boundary faces:        84240
    "PINWALL_4"
       boundary faces:         3120
    "SLEEVEWALL_1"
       boundary faces:        20000
    "SLEEVEWALL_2"
       boundary faces:        13500
    "SLEEVEWALL_3"
       boundary faces:        13500
    "SLEEVEWALL_4"
       boundary faces:          500

 --- Information on the volumes
       Minimum control volume      =  1.1343290e-13
       Maximum control volume      =  8.2069719e-09
       Total volume for the domain =  1.1176549e-02

  Criterion 1: Orthogonality:
    Number of bad cells detected: 0 -->   0 %

  Criterion 2: Offset:
    Number of bad cells detected: 637864 -->   6 %

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 32083 -->   0 %

  Criterion 4: Cells Volume Ratio:
    Number of bad cells detected: 14 -->   0 %

  Criterion 5: Guilt by Association:
    Number of bad cells detected: 0 -->   0 %

 Warning:
 --------
    Mesh quality issue has been detected

    The mesh should be re-considered using the listed criteria.

    The calculation will run but the solution quality may be degraded...

 Computing geometric quantities (1.66 s)
                                                             
       ALMAX  =    0.22392E+00 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.

       ALMAX is the length used to initialize the turbulence.

 ----------------------------------------------------------- 

   ** READING MAIN AND AUXILIARY RESTART FILES
      ----------------------------------------


      READING THE MAIN RESTART FILE

 Start reading
 Reading dimensions complete
  Reading the previous time step number (restarting computation)  NTPABS =         9783
  Reading the previous time step number (restarting computation)  TTPABS =   0.9783E-02
 Reading options complete
  Read variables from restart: restart/main
 Reading complete

         READING THE AUXILIARY RESTART FILE             

 Start reading                                          
   Fin de la lecture des options                        

   Apdatation of the reference point for the total pressure  
       by reading the restart file                           
    XYZP0 =    0.57243E-02   0.59277E-02   0.30200E+01

   Fin de la lecture des proprietes physiques           
   Fin de la lecture du pas de temps                    
   Fin de la lecture des flux de masse                  
   Fin de la lecture des conditions aux limites         
   Fin de la lecture des termes sources                 
  restart/auxiliary: section "time_moments:sizes" not present.
 End reading                                            

 ----------------------------------------------------------- 


 -----------------------------------------------------------


 ** VARIABLES INITIALIZATION
    ------------------------

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Velocity         -0.6337E+00  0.6136E+00
  Velocity         -0.5738E+00  0.5444E+00
  Velocity          0.1565E+01  0.5437E+01
  Pressure         -0.3642E+02  0.3601E+03
  r11               0.1057E-02  0.8186E-01
  r22               0.1108E-02  0.8262E-01
  r33               0.1631E-02  0.1743E+00
  r12              -0.1067E-01  0.1357E-01
  r13              -0.4556E-01  0.5278E-01
  r23              -0.4666E-01  0.5117E-01
  epsilon           0.6849E-01  0.2712E+03
  TempC             0.3000E+03  0.3117E+03
 ---------------------------------

                dt  0.1741E-05  0.1000E-02
 ---------------------------------



-------------------------------------------------------------

 ------------------------------------------------------------- 



===============================================================



                       MAIN CALCULATION                      
                       ================                      


===============================================================




===============================================================


 INSTANT    0.978400000E-02   TIME STEP NUMBER            9784
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.3202E+02  0.3272E+02
  molecular_viscos  0.2668E-04  0.2710E-04
  turbulent_viscos  0.5986E-04  0.9917E-02
  specific_heat     0.1093E+04  0.1098E+04
 -----------------------------------------

 --- Diffusivity:
 -----------------------------------------------
 Scalar           Number  Min. value  Max. value
 -----------------------------------------------
 TempC                 1  0.3946E-01  0.4029E-01
 -----------------------------------------------



   ** INFORMATION ON BOUNDARY FACES TYPE
      ----------------------------------

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2        5612
Smooth wall               5      358150
Rough wall                6           0
Symmetry                  4      143448
Free outlet               3        5590
Free inlet               13           0
Convective inlet         15           0
Free surface             14           0
Undefined                 1           0
-------------------------------------------------------------------------



   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.147693565E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100834970E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.348596183E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.498428351E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239888840E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81225E-03   0.45288E-02 0.19921E+01 
c  Velocity[X]                                      0.14174E-03 
c  Velocity[Y]                                      0.13204E-03 
c  Velocity[Z]                                      0.42550E-02 
c  Pressure     0.36781E-04     132   0.93621E-02   0.25945E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.54286E-08   0.16953E-08 0.10242E+00 
c  r22          0.10849E-01      13   0.49489E-08   0.18376E-08 0.10295E+00 
c  r33          0.21854E-01      15   0.54868E-08   0.12567E-07 0.12829E+00 
c  r12          0.93827E-03      18   0.49448E-08   0.31616E-09 0.62604E+00 
c  r13          0.46662E-02      19   0.65803E-08   0.14804E-08 0.19995E+00 
c  r23          0.39963E-02      18   0.65870E-08   0.12871E-08 0.20034E+00 
c  epsilon      0.10972E+02      11   0.33544E-08   0.97227E-02 0.16592E+00 
c  TempC        0.25715E+06      16   0.15154E-04   0.84534E-02 0.43392E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338         0.61362        0.005251       0.0015066
v  Velocity[Y]            -0.57386         0.54459       0.0030763      0.00087291
v  Velocity[Z]              1.5655          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4367          4.3406          4.3632
v  Pressure                -36.467          360.03          87.654          169.86
v  r11                   0.0010571        0.081854        0.013066        0.018282
v  r22                   0.0011076        0.082614        0.013346        0.018642
v  r33                   0.0016309         0.17427        0.027233        0.037198
v  r12                   -0.010672        0.013575     -0.00023362     -0.00030921
v  r13                   -0.045559        0.052784      9.2237e-05       0.0010132
v  r23                   -0.046661        0.051153      2.9786e-05      0.00057418
v  epsilon                0.068495          271.18          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9858e-05       0.0099174      0.00092392       0.0017422
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017894           5.278         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71346         0.85282


 TIME FOR THE TIME STEP             9784:        0.23739E+03

===============================================================


 INSTANT    0.978500000E-02   TIME STEP NUMBER            9785
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.404739814E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.580115760E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.174657516E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.238889330E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178620570E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81043E-03   0.45757E-02 0.20015E+01 
c  Velocity[X]                                      0.13974E-03 
c  Velocity[Y]                                      0.13103E-03 
c  Velocity[Z]                                      0.43049E-02 
c  Pressure     0.36270E-04     132   0.92353E-02   0.25586E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.51834E-08   0.16448E-08 0.10112E+00 
c  r22          0.10849E-01      12   0.66726E-08   0.18613E-08 0.10305E+00 
c  r33          0.21854E-01      15   0.59529E-08   0.12666E-07 0.12860E+00 
c  r12          0.93827E-03      17   0.66991E-08   0.30622E-09 0.61753E+00 
c  r13          0.46662E-02      19   0.60045E-08   0.14981E-08 0.20087E+00 
c  r23          0.39963E-02      19   0.53192E-08   0.12975E-08 0.20146E+00 
c  epsilon      0.10972E+02      11   0.33242E-08   0.97046E-02 0.16460E+00 
c  TempC        0.25715E+06      16   0.15103E-04   0.84183E-02 0.43341E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61364       0.0052511       0.0015066
v  Velocity[Y]            -0.57391         0.54426       0.0030763      0.00087289
v  Velocity[Z]              1.5654          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4367          4.3406          4.3632
v  Pressure                -36.473          360.06          87.688          169.89
v  r11                   0.0010572        0.081853        0.013066        0.018282
v  r22                   0.0011076        0.082614        0.013346        0.018642
v  r33                   0.0016309         0.17425        0.027233        0.037198
v  r12                   -0.010672        0.013583     -0.00023362     -0.00030921
v  r13                   -0.045558        0.052784       9.224e-05       0.0010132
v  r23                   -0.046661        0.051184      2.9787e-05      0.00057418
v  epsilon                0.068496          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9856e-05       0.0099175      0.00092392       0.0017422
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017894           5.278         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7407e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71346         0.85282


 TIME FOR THE TIME STEP             9785:        0.78604E+02

===============================================================


 INSTANT    0.978600000E-02   TIME STEP NUMBER            9786
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.873074348E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.373323246E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319057602E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.142335966E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.597818045E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81062E-03   0.45849E-02 0.20055E+01 
c  Velocity[X]                                      0.14187E-03 
c  Velocity[Y]                                      0.13120E-03 
c  Velocity[Z]                                      0.43118E-02 
c  Pressure     0.36467E-04     132   0.92934E-02   0.25723E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.51254E-08   0.16620E-08 0.10136E+00 
c  r22          0.10849E-01      12   0.66074E-08   0.18203E-08 0.10213E+00 
c  r33          0.21854E-01      15   0.55151E-08   0.12554E-07 0.12792E+00 
c  r12          0.93827E-03      18   0.53921E-08   0.30947E-09 0.61718E+00 
c  r13          0.46662E-02      19   0.61919E-08   0.14910E-08 0.20009E+00 
c  r23          0.39963E-02      19   0.58546E-08   0.12968E-08 0.20110E+00 
c  epsilon      0.10972E+02      11   0.33057E-08   0.97626E-02 0.16436E+00 
c  TempC        0.25715E+06      16   0.15118E-04   0.84828E-02 0.43449E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361         0.61365        0.005251       0.0015066
v  Velocity[Y]            -0.57386          0.5443       0.0030763      0.00087285
v  Velocity[Z]              1.5654          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4367          4.3406          4.3632
v  Pressure                -36.451          360.01          87.663          169.85
v  r11                   0.0010572         0.08186        0.013066        0.018282
v  r22                   0.0011076        0.082614        0.013346        0.018642
v  r33                   0.0016309         0.17427        0.027233        0.037198
v  r12                   -0.010669        0.013582     -0.00023362     -0.00030921
v  r13                   -0.045557        0.052784      9.2242e-05       0.0010132
v  r23                   -0.046661        0.051178      2.9789e-05      0.00057418
v  epsilon                0.068497          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9854e-05       0.0099176      0.00092392       0.0017422
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2786         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71346         0.85281


 TIME FOR THE TIME STEP             9786:        0.81087E+02

===============================================================


 INSTANT    0.978700000E-02   TIME STEP NUMBER            9787
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.472682547E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.557094013E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.669076723E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.172463497E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182434067E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      40   0.81267E-03   0.45526E-02 0.19982E+01 
c  Velocity[X]                                      0.14028E-03 
c  Velocity[Y]                                      0.12998E-03 
c  Velocity[Z]                                      0.42824E-02 
c  Pressure     0.37013E-04     133   0.94171E-02   0.26108E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.52226E-08   0.16668E-08 0.10097E+00 
c  r22          0.10849E-01      13   0.47490E-08   0.18613E-08 0.10327E+00 
c  r33          0.21854E-01      15   0.55346E-08   0.12697E-07 0.12865E+00 
c  r12          0.93827E-03      18   0.58630E-08   0.30234E-09 0.61169E+00 
c  r13          0.46662E-02      19   0.59456E-08   0.14988E-08 0.20113E+00 
c  r23          0.39963E-02      19   0.55369E-08   0.12971E-08 0.20080E+00 
c  epsilon      0.10972E+02      11   0.33531E-08   0.99749E-02 0.16677E+00 
c  TempC        0.25715E+06      16   0.15115E-04   0.84542E-02 0.43369E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63365         0.61366       0.0052511       0.0015066
v  Velocity[Y]            -0.57374         0.54444       0.0030764      0.00087287
v  Velocity[Z]              1.5655          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4367          4.3406          4.3632
v  Pressure                 -36.43          360.05           87.65          169.87
v  r11                   0.0010572        0.081862        0.013066        0.018282
v  r22                   0.0011076        0.082614        0.013346        0.018642
v  r33                    0.001631          0.1743        0.027233        0.037198
v  r12                   -0.010664        0.013584     -0.00023362     -0.00030921
v  r13                   -0.045559        0.052782      9.2245e-05       0.0010132
v  r23                   -0.046661         0.05117       2.979e-05      0.00057418
v  epsilon                0.068497          271.17          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9852e-05       0.0099176      0.00092392       0.0017422
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2783         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7407e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71347         0.85282


 TIME FOR THE TIME STEP             9787:        0.77881E+02

===============================================================


 INSTANT    0.978800000E-02   TIME STEP NUMBER            9788
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.214018941E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.116539493E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934891E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.335588940E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186484251E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.321354130E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81129E-03   0.45630E-02 0.20009E+01 
c  Velocity[X]                                      0.14024E-03 
c  Velocity[Y]                                      0.13018E-03 
c  Velocity[Z]                                      0.42926E-02 
c  Pressure     0.36675E-04     132   0.93379E-02   0.25871E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.50366E-08   0.16076E-08 0.10013E+00 
c  r22          0.10849E-01      13   0.45904E-08   0.17961E-08 0.10204E+00 
c  r33          0.21854E-01      14   0.71964E-08   0.12150E-07 0.12696E+00 
c  r12          0.93827E-03      18   0.52281E-08   0.29524E-09 0.60869E+00 
c  r13          0.46662E-02      19   0.59242E-08   0.14521E-08 0.19899E+00 
c  r23          0.39963E-02      18   0.67772E-08   0.12548E-08 0.19817E+00 
c  epsilon      0.10972E+02      11   0.32094E-08   0.92820E-02 0.16180E+00 
c  TempC        0.25715E+06      16   0.15129E-04   0.84292E-02 0.43326E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61361       0.0052512       0.0015066
v  Velocity[Y]            -0.57386         0.54454       0.0030764      0.00087284
v  Velocity[Z]              1.5656          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4367          4.3406          4.3632
v  Pressure                -36.505          360.01          87.653          169.84
v  r11                   0.0010572        0.081859        0.013066        0.018282
v  r22                   0.0011076        0.082613        0.013346        0.018642
v  r33                    0.001631         0.17429        0.027233        0.037198
v  r12                   -0.010661        0.013586     -0.00023362     -0.00030921
v  r13                   -0.045557        0.052782      9.2246e-05       0.0010132
v  r23                   -0.046662        0.051164      2.9791e-05      0.00057418
v  epsilon                0.068498          271.17          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9849e-05       0.0099175      0.00092392       0.0017422
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2782         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71346         0.85282


 TIME FOR THE TIME STEP             9788:        0.81305E+02

===============================================================


 INSTANT    0.978900000E-02   TIME STEP NUMBER            9789
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.781442378E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.198266422E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.560257890E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.636282778E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.447679872E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81136E-03   0.45770E-02 0.20045E+01 
c  Velocity[X]                                      0.14141E-03 
c  Velocity[Y]                                      0.13104E-03 
c  Velocity[Z]                                      0.43046E-02 
c  Pressure     0.36755E-04     132   0.93565E-02   0.25928E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.53508E-08   0.16478E-08 0.10077E+00 
c  r22          0.10849E-01      13   0.48702E-08   0.18037E-08 0.10188E+00 
c  r33          0.21854E-01      14   0.68816E-08   0.12492E-07 0.12791E+00 
c  r12          0.93827E-03      18   0.54557E-08   0.30079E-09 0.61157E+00 
c  r13          0.46662E-02      19   0.56325E-08   0.14767E-08 0.19981E+00 
c  r23          0.39963E-02      18   0.65176E-08   0.12866E-08 0.20033E+00 
c  epsilon      0.10972E+02      11   0.32526E-08   0.10186E-01 0.17190E+00 
c  TempC        0.25715E+06      16   0.15127E-04   0.85093E-02 0.43536E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379         0.61367       0.0052512       0.0015066
v  Velocity[Y]            -0.57388         0.54429       0.0030764      0.00087288
v  Velocity[Z]              1.5657          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4367          4.3406          4.3632
v  Pressure                -36.445          360.04          87.662          169.87
v  r11                   0.0010572        0.081862        0.013066        0.018282
v  r22                   0.0011076        0.082612        0.013346        0.018642
v  r33                    0.001631         0.17427        0.027233        0.037198
v  r12                   -0.010664        0.013594     -0.00023362     -0.00030921
v  r13                   -0.045558        0.052782      9.2249e-05       0.0010132
v  r23                   -0.046662        0.051199      2.9792e-05      0.00057418
v  epsilon                0.068498          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9847e-05       0.0099176      0.00092392       0.0017422
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2778         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7407e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71347         0.85282


 TIME FOR THE TIME STEP             9789:        0.81796E+02

===============================================================


 INSTANT    0.979000000E-02   TIME STEP NUMBER            9790
 ============================================================= 



 Options set or changed by "control_file":
 -----------------------------------------

  max_time_step                           13000 (current: 9790)

 Finished reading "control_file".



   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.517897933E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.540268518E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110034565E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160223088E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.681002503E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81139E-03   0.45652E-02 0.19995E+01 
c  Velocity[X]                                      0.14058E-03 
c  Velocity[Y]                                      0.13066E-03 
c  Velocity[Z]                                      0.42940E-02 
c  Pressure     0.37071E-04     133   0.94370E-02   0.26149E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.50774E-08   0.16278E-08 0.10002E+00 
c  r22          0.10849E-01      13   0.47158E-08   0.18443E-08 0.10297E+00 
c  r33          0.21854E-01      15   0.54675E-08   0.12615E-07 0.12817E+00 
c  r12          0.93828E-03      18   0.60915E-08   0.29905E-09 0.60834E+00 
c  r13          0.46662E-02      19   0.62141E-08   0.14960E-08 0.20072E+00 
c  r23          0.39963E-02      19   0.53758E-08   0.12755E-08 0.19894E+00 
c  epsilon      0.10972E+02      11   0.33086E-08   0.10144E-01 0.16769E+00 
c  TempC        0.25715E+06      16   0.15106E-04   0.84115E-02 0.43272E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61366       0.0052512       0.0015067
v  Velocity[Y]            -0.57385         0.54426       0.0030763      0.00087284
v  Velocity[Z]              1.5658          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4367          4.3406          4.3632
v  Pressure                -36.491          360.03          87.679          169.88
v  r11                   0.0010572        0.081858        0.013066        0.018282
v  r22                   0.0011077        0.082607        0.013346        0.018642
v  r33                    0.001631         0.17428        0.027233        0.037198
v  r12                   -0.010669        0.013596     -0.00023362     -0.00030921
v  r13                    -0.04556        0.052786      9.2252e-05       0.0010132
v  r23                   -0.046663         0.05119      2.9793e-05      0.00057418
v  epsilon                0.068499          271.16          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9845e-05       0.0099177      0.00092393       0.0017422
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2771         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71347         0.85282


 TIME FOR THE TIME STEP             9790:        0.80702E+02

===============================================================


 INSTANT    0.979100000E-02   TIME STEP NUMBER            9791
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.728815685E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.231766486E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.617138396E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.271655818E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.879990651E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      45   0.81164E-03   0.45823E-02 0.20048E+01 
c  Velocity[X]                                      0.14073E-03 
c  Velocity[Y]                                      0.13067E-03 
c  Velocity[Z]                                      0.43109E-02 
c  Pressure     0.36583E-04     133   0.93122E-02   0.25805E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.54084E-08   0.16613E-08 0.10087E+00 
c  r22          0.10849E-01      13   0.46538E-08   0.18246E-08 0.10215E+00 
c  r33          0.21854E-01      15   0.65387E-08   0.12559E-07 0.12801E+00 
c  r12          0.93828E-03      18   0.57825E-08   0.30485E-09 0.61389E+00 
c  r13          0.46663E-02      20   0.59936E-08   0.14878E-08 0.19984E+00 
c  r23          0.39963E-02      19   0.53298E-08   0.12901E-08 0.20040E+00 
c  epsilon      0.10972E+02      11   0.34205E-08   0.98796E-02 0.16383E+00 
c  TempC        0.25715E+06      16   0.15094E-04   0.84569E-02 0.43415E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61364       0.0052513       0.0015067
v  Velocity[Y]             -0.5738         0.54437       0.0030764      0.00087287
v  Velocity[Z]              1.5653          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4367          4.3406          4.3632
v  Pressure                -36.469          360.07          87.679          169.89
v  r11                   0.0010573        0.081859        0.013066        0.018282
v  r22                   0.0011077        0.082607        0.013346        0.018642
v  r33                   0.0016311          0.1743        0.027233        0.037198
v  r12                   -0.010669        0.013601     -0.00023362     -0.00030921
v  r13                   -0.045558        0.052783      9.2254e-05       0.0010132
v  r23                   -0.046663        0.051175      2.9793e-05      0.00057418
v  epsilon                  0.0685          271.18          7.2634          7.8886
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9845e-05       0.0099178      0.00092393       0.0017422
v  CourantNb               0.44257             0.6         0.59908         0.59839
v  FourierNb             0.0017894           5.277         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71346         0.85281


 TIME FOR THE TIME STEP             9791:        0.81961E+02

===============================================================


 INSTANT    0.979200000E-02   TIME STEP NUMBER            9792
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.143810947E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.509613848E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.274717073E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.185003581E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.189660209E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81159E-03   0.45636E-02 0.20019E+01 
c  Velocity[X]                                      0.14016E-03 
c  Velocity[Y]                                      0.13058E-03 
c  Velocity[Z]                                      0.42928E-02 
c  Pressure     0.36361E-04     131   0.92618E-02   0.25649E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.51764E-08   0.16997E-08 0.10202E+00 
c  r22          0.10849E-01      13   0.50124E-08   0.18604E-08 0.10297E+00 
c  r33          0.21854E-01      15   0.58974E-08   0.12817E-07 0.12926E+00 
c  r12          0.93828E-03      18   0.55517E-08   0.31569E-09 0.62288E+00 
c  r13          0.46662E-02      19   0.67221E-08   0.15122E-08 0.20083E+00 
c  r23          0.39963E-02      19   0.57664E-08   0.13155E-08 0.20270E+00 
c  epsilon      0.10972E+02      11   0.35046E-08   0.99779E-02 0.16631E+00 
c  TempC        0.25715E+06      16   0.15126E-04   0.84963E-02 0.43526E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61368       0.0052513       0.0015067
v  Velocity[Y]            -0.57383         0.54454       0.0030764      0.00087285
v  Velocity[Z]              1.5654          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4366          4.3406          4.3632
v  Pressure                -36.484          360.01          87.635          169.84
v  r11                   0.0010573        0.081854        0.013066        0.018282
v  r22                   0.0011077        0.082607        0.013346        0.018642
v  r33                   0.0016311         0.17429        0.027233        0.037198
v  r12                   -0.010667        0.013607     -0.00023362     -0.00030921
v  r13                   -0.045556        0.052782      9.2256e-05       0.0010132
v  r23                   -0.046664        0.051191      2.9795e-05      0.00057418
v  epsilon                  0.0685          271.18          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9842e-05       0.0099178      0.00092393       0.0017422
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2765         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765         0.71346         0.85282


 TIME FOR THE TIME STEP             9792:        0.82649E+02

===============================================================


 INSTANT    0.979300000E-02   TIME STEP NUMBER            9793
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.857431257E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.310286717E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934910E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149820965E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.595261807E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.758032411E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      40   0.81243E-03   0.45726E-02 0.19986E+01 
c  Velocity[X]                                      0.13956E-03 
c  Velocity[Y]                                      0.13043E-03 
c  Velocity[Z]                                      0.43026E-02 
c  Pressure     0.36455E-04     136   0.92837E-02   0.25715E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.52665E-08   0.17019E-08 0.10245E+00 
c  r22          0.10849E-01      13   0.49492E-08   0.18415E-08 0.10315E+00 
c  r33          0.21854E-01      15   0.62676E-08   0.12761E-07 0.12978E+00 
c  r12          0.93828E-03      18   0.53387E-08   0.31051E-09 0.62014E+00 
c  r13          0.46663E-02      19   0.64386E-08   0.14984E-08 0.20129E+00 
c  r23          0.39963E-02      18   0.64958E-08   0.13279E-08 0.20425E+00 
c  epsilon      0.10972E+02      11   0.33984E-08   0.95862E-02 0.16394E+00 
c  TempC        0.25715E+06      16   0.15096E-04   0.83802E-02 0.43178E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61369       0.0052512       0.0015066
v  Velocity[Y]            -0.57368         0.54434       0.0030763      0.00087285
v  Velocity[Z]              1.5653          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4366          4.3406          4.3632
v  Pressure                -36.441          360.04          87.666          169.87
v  r11                   0.0010573        0.081856        0.013066        0.018282
v  r22                   0.0011077        0.082608        0.013346        0.018642
v  r33                   0.0016311         0.17426        0.027233        0.037198
v  r12                   -0.010664        0.013612     -0.00023362     -0.00030921
v  r13                    -0.04556        0.052781      9.2259e-05       0.0010132
v  r23                   -0.046664        0.051168      2.9796e-05      0.00057418
v  epsilon                0.068501          271.16          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9843e-05       0.0099178      0.00092393       0.0017422
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017894           5.277         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71346         0.85281


 TIME FOR THE TIME STEP             9793:        0.83703E+02

===============================================================


 INSTANT    0.979400000E-02   TIME STEP NUMBER            9794
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.193319812E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.104870222E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.186719960E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.488258223E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.304827236E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81182E-03   0.45982E-02 0.20080E+01 
c  Velocity[X]                                      0.14093E-03 
c  Velocity[Y]                                      0.13105E-03 
c  Velocity[Z]                                      0.43263E-02 
c  Pressure     0.36711E-04     131   0.93429E-02   0.25895E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.50466E-08   0.16309E-08 0.10077E+00 
c  r22          0.10849E-01      13   0.52232E-08   0.18101E-08 0.10241E+00 
c  r33          0.21854E-01      15   0.55384E-08   0.12401E-07 0.12828E+00 
c  r12          0.93828E-03      18   0.64312E-08   0.29461E-09 0.60915E+00 
c  r13          0.46663E-02      18   0.65592E-08   0.14728E-08 0.20062E+00 
c  r23          0.39963E-02      18   0.71239E-08   0.12585E-08 0.19978E+00 
c  epsilon      0.10972E+02      11   0.32496E-08   0.96006E-02 0.16357E+00 
c  TempC        0.25715E+06      16   0.15167E-04   0.84392E-02 0.43297E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61369       0.0052512       0.0015066
v  Velocity[Y]             -0.5737         0.54429       0.0030763      0.00087282
v  Velocity[Z]              1.5657          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4366          4.3406          4.3632
v  Pressure                -36.513          360.02          87.667          169.86
v  r11                   0.0010573         0.08185        0.013066        0.018282
v  r22                   0.0011077        0.082608        0.013346        0.018642
v  r33                   0.0016311         0.17428        0.027233        0.037198
v  r12                   -0.010664        0.013614     -0.00023362     -0.00030921
v  r13                   -0.045557        0.052781       9.226e-05       0.0010132
v  r23                   -0.046664        0.051159      2.9797e-05      0.00057418
v  epsilon                0.068502          271.17          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9844e-05       0.0099178      0.00092393       0.0017422
v  CourantNb               0.44259             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2774         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71346         0.85282


 TIME FOR THE TIME STEP             9794:        0.81037E+02

===============================================================


 INSTANT    0.979500000E-02   TIME STEP NUMBER            9795
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.953332183E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155262937E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.275068879E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.292310714E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.155320692E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81068E-03   0.45646E-02 0.20042E+01 
c  Velocity[X]                                      0.14147E-03 
c  Velocity[Y]                                      0.13058E-03 
c  Velocity[Z]                                      0.42925E-02 
c  Pressure     0.36977E-04     133   0.94105E-02   0.26084E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.48455E-08   0.17347E-08 0.10326E+00 
c  r22          0.10849E-01      13   0.46884E-08   0.18317E-08 0.10309E+00 
c  r33          0.21854E-01      15   0.56254E-08   0.12847E-07 0.13056E+00 
c  r12          0.93828E-03      18   0.55359E-08   0.30418E-09 0.61727E+00 
c  r13          0.46663E-02      18   0.70594E-08   0.14729E-08 0.20075E+00 
c  r23          0.39963E-02      19   0.64193E-08   0.13264E-08 0.20484E+00 
c  epsilon      0.10972E+02      11   0.33183E-08   0.10303E-01 0.17243E+00 
c  TempC        0.25715E+06      16   0.15070E-04   0.85066E-02 0.43503E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392          0.6137       0.0052512       0.0015066
v  Velocity[Y]            -0.57372         0.54437       0.0030764      0.00087286
v  Velocity[Z]              1.5657          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4366          4.3406          4.3632
v  Pressure                -36.441          360.11          87.706          169.93
v  r11                   0.0010573        0.081846        0.013066        0.018282
v  r22                   0.0011077        0.082608        0.013346        0.018642
v  r33                   0.0016312         0.17431        0.027233        0.037198
v  r12                   -0.010662        0.013618     -0.00023362     -0.00030921
v  r13                   -0.045556         0.05278      9.2262e-05       0.0010132
v  r23                   -0.046665        0.051181      2.9798e-05      0.00057418
v  epsilon                0.068502          271.18          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9847e-05       0.0099177      0.00092393       0.0017422
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2768         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71346         0.85282


 TIME FOR THE TIME STEP             9795:        0.83902E+02

===============================================================


 INSTANT    0.979600000E-02   TIME STEP NUMBER            9796
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.121208933E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.205949300E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110320436E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.742351196E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242394265E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81273E-03   0.45658E-02 0.19998E+01 
c  Velocity[X]                                      0.14065E-03 
c  Velocity[Y]                                      0.13018E-03 
c  Velocity[Z]                                      0.42949E-02 
c  Pressure     0.36329E-04     131   0.92529E-02   0.25627E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.50580E-08   0.16563E-08 0.10125E+00 
c  r22          0.10849E-01      13   0.50392E-08   0.18207E-08 0.10225E+00 
c  r33          0.21854E-01      15   0.59992E-08   0.12484E-07 0.12824E+00 
c  r12          0.93828E-03      18   0.62311E-08   0.30452E-09 0.61256E+00 
c  r13          0.46663E-02      19   0.57446E-08   0.14800E-08 0.20001E+00 
c  r23          0.39963E-02      19   0.55934E-08   0.12820E-08 0.20042E+00 
c  epsilon      0.10972E+02      11   0.34043E-08   0.99991E-02 0.16779E+00 
c  TempC        0.25715E+06      16   0.15153E-04   0.84878E-02 0.43513E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61371       0.0052513       0.0015067
v  Velocity[Y]            -0.57369         0.54443       0.0030764      0.00087287
v  Velocity[Z]              1.5658          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4366          4.3406          4.3632
v  Pressure                -36.451          360.02          87.646          169.84
v  r11                   0.0010573        0.081843        0.013066        0.018282
v  r22                   0.0011078        0.082609        0.013346        0.018642
v  r33                   0.0016312         0.17428        0.027233        0.037198
v  r12                   -0.010661        0.013615     -0.00023362     -0.00030921
v  r13                   -0.045559        0.052782      9.2264e-05       0.0010132
v  r23                   -0.046665        0.051168        2.98e-05      0.00057418
v  epsilon                0.068503          271.19          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9849e-05       0.0099177      0.00092393       0.0017422
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2767         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767         0.71347         0.85282


 TIME FOR THE TIME STEP             9796:        0.81341E+02

===============================================================


 INSTANT    0.979700000E-02   TIME STEP NUMBER            9797
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.131682860E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.623892408E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934901E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.306100668E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.222385383E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106003196E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81127E-03   0.45419E-02 0.19951E+01 
c  Velocity[X]                                      0.13920E-03 
c  Velocity[Y]                                      0.13118E-03 
c  Velocity[Z]                                      0.42716E-02 
c  Pressure     0.36280E-04     132   0.92393E-02   0.25592E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.50901E-08   0.16499E-08 0.10105E+00 
c  r22          0.10849E-01      13   0.48778E-08   0.18509E-08 0.10270E+00 
c  r33          0.21854E-01      15   0.56187E-08   0.12684E-07 0.12879E+00 
c  r12          0.93828E-03      18   0.57860E-08   0.30190E-09 0.61242E+00 
c  r13          0.46663E-02      19   0.57015E-08   0.15080E-08 0.20107E+00 
c  r23          0.39963E-02      19   0.61200E-08   0.12866E-08 0.20079E+00 
c  epsilon      0.10972E+02      11   0.33775E-08   0.99844E-02 0.16589E+00 
c  TempC        0.25715E+06      16   0.15127E-04   0.84339E-02 0.43370E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61368       0.0052513       0.0015066
v  Velocity[Y]            -0.57363         0.54451       0.0030765      0.00087286
v  Velocity[Z]              1.5656          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4367          4.3406          4.3632
v  Pressure                -36.432          360.08          87.688           169.9
v  r11                   0.0010574        0.081857        0.013066        0.018282
v  r22                   0.0011078        0.082606        0.013346        0.018642
v  r33                   0.0016312         0.17426        0.027233        0.037198
v  r12                   -0.010665        0.013619     -0.00023362     -0.00030921
v  r13                   -0.045558        0.052783      9.2267e-05       0.0010132
v  r23                   -0.046665        0.051155      2.9801e-05      0.00057419
v  epsilon                0.068503          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9854e-05       0.0099176      0.00092394       0.0017422
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2774         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71346         0.85281


 TIME FOR THE TIME STEP             9797:        0.82752E+02

===============================================================


 INSTANT    0.979800000E-02   TIME STEP NUMBER            9798
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.559863940E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.708695055E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.700025160E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100493482E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.655409400E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81091E-03   0.45678E-02 0.20017E+01 
c  Velocity[X]                                      0.14040E-03 
c  Velocity[Y]                                      0.13182E-03 
c  Velocity[Z]                                      0.42956E-02 
c  Pressure     0.36293E-04     132   0.92460E-02   0.25601E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.56077E-08   0.15866E-08 0.99365E-01 
c  r22          0.10849E-01      13   0.50834E-08   0.18011E-08 0.10158E+00 
c  r33          0.21854E-01      15   0.58696E-08   0.12209E-07 0.12709E+00 
c  r12          0.93828E-03      18   0.59292E-08   0.29600E-09 0.60727E+00 
c  r13          0.46663E-02      19   0.69971E-08   0.15011E-08 0.20077E+00 
c  r23          0.39963E-02      19   0.64776E-08   0.12470E-08 0.19794E+00 
c  epsilon      0.10972E+02      10   0.54832E-08   0.94489E-02 0.16244E+00 
c  TempC        0.25715E+06      16   0.15105E-04   0.84137E-02 0.43243E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61368       0.0052513       0.0015066
v  Velocity[Y]            -0.57361         0.54429       0.0030763      0.00087282
v  Velocity[Z]              1.5655          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4367          4.3406          4.3632
v  Pressure                -36.458          360.02          87.665          169.85
v  r11                   0.0010574        0.081859        0.013066        0.018282
v  r22                   0.0011078        0.082608        0.013346        0.018642
v  r33                   0.0016312         0.17427        0.027233        0.037198
v  r12                   -0.010663        0.013622     -0.00023362     -0.00030921
v  r13                   -0.045556        0.052783       9.227e-05       0.0010132
v  r23                   -0.046665        0.051147      2.9802e-05      0.00057419
v  epsilon                0.068504          271.16          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.986e-05       0.0099175      0.00092394       0.0017422
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2783         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71347         0.85282


 TIME FOR THE TIME STEP             9798:        0.83413E+02

===============================================================


 INSTANT    0.979900000E-02   TIME STEP NUMBER            9799
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249479722E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.467263080E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.413912989E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.113200618E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.544150360E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81230E-03   0.45580E-02 0.20003E+01 
c  Velocity[X]                                      0.13995E-03 
c  Velocity[Y]                                      0.13021E-03 
c  Velocity[Z]                                      0.42878E-02 
c  Pressure     0.36800E-04     134   0.93644E-02   0.25959E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.54521E-08   0.16488E-08 0.10092E+00 
c  r22          0.10849E-01      13   0.51925E-08   0.17904E-08 0.10155E+00 
c  r33          0.21854E-01      15   0.54043E-08   0.12301E-07 0.12760E+00 
c  r12          0.93828E-03      18   0.65836E-08   0.30470E-09 0.61226E+00 
c  r13          0.46663E-02      19   0.65367E-08   0.14577E-08 0.19907E+00 
c  r23          0.39963E-02      19   0.71195E-08   0.12711E-08 0.19925E+00 
c  epsilon      0.10972E+02      11   0.33625E-08   0.94534E-02 0.16312E+00 
c  TempC        0.25715E+06      16   0.15116E-04   0.84843E-02 0.43428E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61371       0.0052512       0.0015066
v  Velocity[Y]            -0.57371         0.54435       0.0030764      0.00087283
v  Velocity[Z]              1.5657          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4367          4.3406          4.3632
v  Pressure                -36.427          360.09           87.68           169.9
v  r11                   0.0010574        0.081859        0.013066        0.018282
v  r22                   0.0011078         0.08261        0.013346        0.018642
v  r33                   0.0016312          0.1743        0.027233        0.037198
v  r12                   -0.010661        0.013618     -0.00023362     -0.00030921
v  r13                   -0.045559        0.052782      9.2272e-05       0.0010132
v  r23                   -0.046665        0.051174      2.9803e-05      0.00057419
v  epsilon                0.068505          271.18          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9868e-05       0.0099175      0.00092394       0.0017422
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2787         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71347         0.85282


 TIME FOR THE TIME STEP             9799:        0.84379E+02

===============================================================


 INSTANT    0.980000000E-02   TIME STEP NUMBER            9800
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.331345319E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.629681887E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.821635217E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.198239282E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145034958E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81115E-03   0.45586E-02 0.19996E+01 
c  Velocity[X]                                      0.14029E-03 
c  Velocity[Y]                                      0.12966E-03 
c  Velocity[Z]                                      0.42887E-02 
c  Pressure     0.36488E-04     132   0.92901E-02   0.25739E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.52211E-08   0.16308E-08 0.10030E+00 
c  r22          0.10849E-01      13   0.51553E-08   0.18226E-08 0.10255E+00 
c  r33          0.21854E-01      14   0.65487E-08   0.12420E-07 0.12823E+00 
c  r12          0.93828E-03      18   0.60986E-08   0.29723E-09 0.60701E+00 
c  r13          0.46663E-02      19   0.58161E-08   0.14898E-08 0.20041E+00 
c  r23          0.39963E-02      19   0.60745E-08   0.12815E-08 0.19966E+00 
c  epsilon      0.10972E+02      11   0.34250E-08   0.96618E-02 0.16485E+00 
c  TempC        0.25715E+06      16   0.15136E-04   0.84452E-02 0.43374E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63396         0.61369       0.0052512       0.0015066
v  Velocity[Y]            -0.57389         0.54448       0.0030764      0.00087282
v  Velocity[Z]              1.5659          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5797          5.4367          4.3406          4.3632
v  Pressure                -36.498          360.03          87.671          169.86
v  r11                   0.0010574        0.081856        0.013066        0.018282
v  r22                   0.0011078        0.082612        0.013346        0.018642
v  r33                   0.0016313         0.17428        0.027233        0.037198
v  r12                   -0.010659         0.01362     -0.00023363     -0.00030921
v  r13                   -0.045557        0.052784      9.2274e-05       0.0010132
v  r23                   -0.046666        0.051166      2.9804e-05      0.00057419
v  epsilon                0.068505          271.18          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9873e-05       0.0099175      0.00092394       0.0017422
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2789         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71347         0.85282


 TIME FOR THE TIME STEP             9800:        0.83304E+02

===============================================================


 INSTANT    0.980100000E-02   TIME STEP NUMBER            9801
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.725321724E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.189439389E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.304246626E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.794364040E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.987731274E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81130E-03   0.45863E-02 0.20055E+01 
c  Velocity[X]                                      0.14064E-03 
c  Velocity[Y]                                      0.13065E-03 
c  Velocity[Z]                                      0.43150E-02 
c  Pressure     0.36589E-04     132   0.93166E-02   0.25811E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.51592E-08   0.16344E-08 0.10064E+00 
c  r22          0.10849E-01      13   0.49725E-08   0.18533E-08 0.10285E+00 
c  r33          0.21854E-01      14   0.68726E-08   0.12538E-07 0.12870E+00 
c  r12          0.93828E-03      18   0.56524E-08   0.30475E-09 0.61218E+00 
c  r13          0.46663E-02      19   0.53396E-08   0.15045E-08 0.20124E+00 
c  r23          0.39963E-02      19   0.58238E-08   0.12739E-08 0.19991E+00 
c  epsilon      0.10972E+02      11   0.34068E-08   0.96585E-02 0.16364E+00 
c  TempC        0.25715E+06      16   0.15133E-04   0.84174E-02 0.43358E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61371       0.0052513       0.0015066
v  Velocity[Y]            -0.57389         0.54426       0.0030764      0.00087286
v  Velocity[Z]              1.5659          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5797          5.4367          4.3406          4.3632
v  Pressure                -36.442          360.04          87.651          169.86
v  r11                   0.0010574        0.081855        0.013066        0.018282
v  r22                   0.0011078        0.082613        0.013346        0.018642
v  r33                   0.0016313         0.17426        0.027233        0.037199
v  r12                   -0.010658        0.013622     -0.00023363     -0.00030922
v  r13                   -0.045558        0.052784      9.2276e-05       0.0010132
v  r23                   -0.046665         0.05116      2.9806e-05      0.00057419
v  epsilon                0.068506          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9879e-05       0.0099176      0.00092394       0.0017422
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2781         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71347         0.85282


 TIME FOR THE TIME STEP             9801:        0.80936E+02

===============================================================


 INSTANT    0.980200000E-02   TIME STEP NUMBER            9802
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127181308E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.650259393E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.233104470E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208680371E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.481935303E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81216E-03   0.45362E-02 0.19963E+01 
c  Velocity[X]                                      0.13952E-03 
c  Velocity[Y]                                      0.13052E-03 
c  Velocity[Z]                                      0.42662E-02 
c  Pressure     0.36446E-04     133   0.92754E-02   0.25709E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.49741E-08   0.16580E-08 0.10093E+00 
c  r22          0.10849E-01      13   0.48119E-08   0.18537E-08 0.10270E+00 
c  r33          0.21854E-01      15   0.52009E-08   0.12812E-07 0.12918E+00 
c  r12          0.93828E-03      18   0.59809E-08   0.29697E-09 0.60673E+00 
c  r13          0.46663E-02      19   0.52896E-08   0.15086E-08 0.20086E+00 
c  r23          0.39963E-02      19   0.54601E-08   0.12977E-08 0.20181E+00 
c  epsilon      0.10972E+02      11   0.34517E-08   0.10617E-01 0.17434E+00 
c  TempC        0.25715E+06      16   0.15137E-04   0.84614E-02 0.43364E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61371       0.0052513       0.0015066
v  Velocity[Y]            -0.57395         0.54435       0.0030764      0.00087285
v  Velocity[Z]               1.566          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5798          5.4366          4.3406          4.3632
v  Pressure                 -36.47          360.11          87.709          169.92
v  r11                   0.0010574        0.081862        0.013066        0.018282
v  r22                   0.0011079        0.082615        0.013346        0.018642
v  r33                   0.0016313         0.17427        0.027233        0.037199
v  r12                   -0.010657        0.013618     -0.00023363     -0.00030922
v  r13                    -0.04556        0.052787      9.2278e-05       0.0010132
v  r23                   -0.046665        0.051155      2.9806e-05      0.00057419
v  epsilon                0.068507          271.16          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9882e-05       0.0099177      0.00092394       0.0017422
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2779         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71347         0.85282


 TIME FOR THE TIME STEP             9802:        0.83241E+02

===============================================================


 INSTANT    0.980300000E-02   TIME STEP NUMBER            9803
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.832082857E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.347022539E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141450499E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184380763E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.299655450E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81135E-03   0.45585E-02 0.20006E+01 
c  Velocity[X]                                      0.14029E-03 
c  Velocity[Y]                                      0.13093E-03 
c  Velocity[Z]                                      0.42873E-02 
c  Pressure     0.36645E-04     132   0.93381E-02   0.25850E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.51056E-08   0.16450E-08 0.10063E+00 
c  r22          0.10849E-01      13   0.48861E-08   0.18433E-08 0.10271E+00 
c  r33          0.21854E-01      15   0.67965E-08   0.12590E-07 0.12814E+00 
c  r12          0.93828E-03      18   0.54167E-08   0.30067E-09 0.60841E+00 
c  r13          0.46663E-02      19   0.55507E-08   0.15140E-08 0.20111E+00 
c  r23          0.39963E-02      19   0.62953E-08   0.12751E-08 0.19909E+00 
c  epsilon      0.10972E+02      11   0.34881E-08   0.99078E-02 0.16521E+00 
c  TempC        0.25715E+06      16   0.15132E-04   0.85248E-02 0.43589E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61369       0.0052513       0.0015066
v  Velocity[Y]             -0.5738         0.54454       0.0030764      0.00087284
v  Velocity[Z]              1.5657          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4366          4.3406          4.3632
v  Pressure                -36.445          360.13          87.732          169.94
v  r11                   0.0010574        0.081869        0.013066        0.018282
v  r22                   0.0011079        0.082613        0.013346        0.018642
v  r33                   0.0016313          0.1743        0.027233        0.037199
v  r12                   -0.010663        0.013621     -0.00023363     -0.00030922
v  r13                   -0.045557        0.052788       9.228e-05       0.0010132
v  r23                   -0.046665        0.051187      2.9807e-05      0.00057419
v  epsilon                0.068507          271.19          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9884e-05       0.0099179      0.00092395       0.0017422
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2785         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71347         0.85282


 TIME FOR THE TIME STEP             9803:        0.81328E+02

===============================================================


 INSTANT    0.980400000E-02   TIME STEP NUMBER            9804
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.274365060E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173228252E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.218408982E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191106559E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226960750E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81164E-03   0.45631E-02 0.20002E+01 
c  Velocity[X]                                      0.14052E-03 
c  Velocity[Y]                                      0.13089E-03 
c  Velocity[Z]                                      0.42917E-02 
c  Pressure     0.36276E-04     132   0.92363E-02   0.25590E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.50200E-08   0.16308E-08 0.10022E+00 
c  r22          0.10849E-01      13   0.48293E-08   0.18272E-08 0.10217E+00 
c  r33          0.21854E-01      15   0.65189E-08   0.12435E-07 0.12750E+00 
c  r12          0.93828E-03      18   0.48989E-08   0.29534E-09 0.60757E+00 
c  r13          0.46663E-02      18   0.63379E-08   0.14831E-08 0.20018E+00 
c  r23          0.39963E-02      19   0.59475E-08   0.12660E-08 0.19861E+00 
c  epsilon      0.10972E+02      11   0.34165E-08   0.98597E-02 0.16362E+00 
c  TempC        0.25715E+06      16   0.15155E-04   0.84689E-02 0.43397E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391          0.6137       0.0052513       0.0015066
v  Velocity[Y]            -0.57389         0.54422       0.0030764      0.00087287
v  Velocity[Z]              1.5657          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4366          4.3406          4.3632
v  Pressure                -36.497          360.03          87.652          169.85
v  r11                   0.0010575         0.08187        0.013066        0.018282
v  r22                   0.0011079        0.082615        0.013346        0.018642
v  r33                   0.0016313         0.17428        0.027233        0.037199
v  r12                   -0.010662        0.013618     -0.00023363     -0.00030922
v  r13                   -0.045556        0.052789      9.2283e-05       0.0010132
v  r23                   -0.046664        0.051178      2.9808e-05      0.00057419
v  epsilon                0.068508           271.2          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9884e-05        0.009918      0.00092395       0.0017422
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2786         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71347         0.85282


 TIME FOR THE TIME STEP             9804:        0.78544E+02

===============================================================


 INSTANT    0.980500000E-02   TIME STEP NUMBER            9805
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242588431E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.122906849E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106985884E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199310258E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.579637918E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81146E-03   0.45651E-02 0.19994E+01 
c  Velocity[X]                                      0.13953E-03 
c  Velocity[Y]                                      0.13054E-03 
c  Velocity[Z]                                      0.42951E-02 
c  Pressure     0.36551E-04     131   0.93026E-02   0.25784E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.55452E-08   0.16611E-08 0.10071E+00 
c  r22          0.10849E-01      13   0.47220E-08   0.18461E-08 0.10244E+00 
c  r33          0.21854E-01      15   0.52663E-08   0.12732E-07 0.12858E+00 
c  r12          0.93828E-03      18   0.50235E-08   0.30458E-09 0.61077E+00 
c  r13          0.46663E-02      18   0.64038E-08   0.15192E-08 0.20142E+00 
c  r23          0.39963E-02      18   0.68213E-08   0.13079E-08 0.20042E+00 
c  epsilon      0.10972E+02      11   0.33143E-08   0.10206E-01 0.16771E+00 
c  TempC        0.25715E+06      16   0.15083E-04   0.83904E-02 0.43217E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63371         0.61372       0.0052513       0.0015066
v  Velocity[Y]            -0.57372         0.54424       0.0030765      0.00087289
v  Velocity[Z]              1.5657          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4366          4.3406          4.3632
v  Pressure                -36.449          360.06          87.661          169.88
v  r11                   0.0010575        0.081862        0.013066        0.018282
v  r22                   0.0011079        0.082618        0.013346        0.018642
v  r33                   0.0016314         0.17425        0.027233        0.037199
v  r12                   -0.010661        0.013615     -0.00023363     -0.00030922
v  r13                    -0.04556         0.05279      9.2285e-05       0.0010132
v  r23                   -0.046663        0.051159      2.9809e-05      0.00057419
v  epsilon                0.068508          271.15          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9883e-05        0.009918      0.00092395       0.0017422
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2786         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71347         0.85282


 TIME FOR THE TIME STEP             9805:        0.76349E+02

===============================================================


 INSTANT    0.980600000E-02   TIME STEP NUMBER            9806
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178174412E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.211803156E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.222498219E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.217928459E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.211220847E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81128E-03   0.45482E-02 0.19975E+01 
c  Velocity[X]                                      0.14002E-03 
c  Velocity[Y]                                      0.13033E-03 
c  Velocity[Z]                                      0.42779E-02 
c  Pressure     0.36228E-04     131   0.92204E-02   0.25555E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.65250E-08   0.16565E-08 0.10042E+00 
c  r22          0.10849E-01      13   0.52736E-08   0.18233E-08 0.10213E+00 
c  r33          0.21854E-01      14   0.69435E-08   0.12565E-07 0.12794E+00 
c  r12          0.93828E-03      18   0.53964E-08   0.29821E-09 0.61007E+00 
c  r13          0.46663E-02      18   0.67939E-08   0.15059E-08 0.20080E+00 
c  r23          0.39963E-02      18   0.70344E-08   0.12970E-08 0.20021E+00 
c  epsilon      0.10972E+02      11   0.33033E-08   0.99822E-02 0.16701E+00 
c  TempC        0.25715E+06      16   0.15127E-04   0.84507E-02 0.43361E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63377          0.6137       0.0052514       0.0015066
v  Velocity[Y]             -0.5737         0.54432       0.0030764      0.00087284
v  Velocity[Z]              1.5655          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4366          4.3406          4.3632
v  Pressure                -36.499             360          87.656          169.83
v  r11                   0.0010575        0.081854        0.013066        0.018282
v  r22                   0.0011079        0.082621        0.013346        0.018642
v  r33                   0.0016314         0.17427        0.027234        0.037199
v  r12                   -0.010659        0.013617     -0.00023363     -0.00030922
v  r13                   -0.045557        0.052791      9.2288e-05       0.0010133
v  r23                   -0.046662        0.051152       2.981e-05      0.00057419
v  epsilon                0.068509          271.16          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9882e-05        0.009918      0.00092395       0.0017422
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2789         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71347         0.85282


 TIME FOR THE TIME STEP             9806:        0.78354E+02

===============================================================


 INSTANT    0.980700000E-02   TIME STEP NUMBER            9807
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.316191838E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.402857289E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.226541073E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.943107995E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.253129776E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81192E-03   0.45548E-02 0.20013E+01 
c  Velocity[X]                                      0.14152E-03 
c  Velocity[Y]                                      0.13100E-03 
c  Velocity[Z]                                      0.42823E-02 
c  Pressure     0.36591E-04     132   0.93144E-02   0.25811E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.58653E-08   0.16308E-08 0.10060E+00 
c  r22          0.10849E-01      13   0.56349E-08   0.17888E-08 0.10173E+00 
c  r33          0.21854E-01      15   0.56929E-08   0.12290E-07 0.12773E+00 
c  r12          0.93829E-03      18   0.59936E-08   0.29007E-09 0.60731E+00 
c  r13          0.46663E-02      19   0.58056E-08   0.14613E-08 0.19913E+00 
c  r23          0.39963E-02      19   0.54880E-08   0.12692E-08 0.19934E+00 
c  epsilon      0.10972E+02      11   0.32402E-08   0.93674E-02 0.16147E+00 
c  TempC        0.25715E+06      16   0.15116E-04   0.85036E-02 0.43519E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61372       0.0052512       0.0015066
v  Velocity[Y]            -0.57353         0.54445       0.0030764      0.00087288
v  Velocity[Z]              1.5656          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4366          4.3406          4.3632
v  Pressure                -36.432          360.12          87.705          169.93
v  r11                   0.0010575        0.081864        0.013066        0.018282
v  r22                   0.0011079        0.082623        0.013346        0.018642
v  r33                   0.0016314          0.1743        0.027234        0.037199
v  r12                   -0.010656        0.013617     -0.00023363     -0.00030922
v  r13                   -0.045557         0.05279       9.229e-05       0.0010133
v  r23                   -0.046661        0.051179      2.9812e-05      0.00057419
v  epsilon                 0.06851          271.19          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9881e-05       0.0099179      0.00092395       0.0017422
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2793         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8793         0.71347         0.85282


 TIME FOR THE TIME STEP             9807:        0.79306E+02

===============================================================


 INSTANT    0.980800000E-02   TIME STEP NUMBER            9808
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.233007356E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.134203871E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.104274628E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.767031380E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.142597367E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81189E-03   0.45454E-02 0.19949E+01 
c  Velocity[X]                                      0.13968E-03 
c  Velocity[Y]                                      0.12976E-03 
c  Velocity[Z]                                      0.42760E-02 
c  Pressure     0.36428E-04     133   0.92738E-02   0.25697E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.55627E-08   0.16781E-08 0.10188E+00 
c  r22          0.10849E-01      13   0.53833E-08   0.18246E-08 0.10216E+00 
c  r33          0.21854E-01      15   0.53933E-08   0.12703E-07 0.12920E+00 
c  r12          0.93829E-03      18   0.59614E-08   0.29980E-09 0.61264E+00 
c  r13          0.46663E-02      18   0.70543E-08   0.14939E-08 0.20068E+00 
c  r23          0.39963E-02      19   0.51434E-08   0.13136E-08 0.20302E+00 
c  epsilon      0.10972E+02      11   0.32859E-08   0.10399E-01 0.17366E+00 
c  TempC        0.25715E+06      16   0.15124E-04   0.83973E-02 0.43298E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61371       0.0052513       0.0015066
v  Velocity[Y]            -0.57363         0.54424       0.0030764      0.00087286
v  Velocity[Z]              1.5657          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4366          4.3406          4.3632
v  Pressure                -36.469          360.03          87.648          169.85
v  r11                   0.0010575         0.08187        0.013066        0.018282
v  r22                    0.001108        0.082624        0.013346        0.018642
v  r33                   0.0016314         0.17428        0.027234        0.037199
v  r12                   -0.010655        0.013611     -0.00023363     -0.00030922
v  r13                   -0.045559        0.052792      9.2292e-05       0.0010133
v  r23                    -0.04666        0.051175      2.9812e-05      0.00057419
v  epsilon                 0.06851           271.2          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9876e-05        0.009918      0.00092395       0.0017422
v  CourantNb               0.44256             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2787         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71347         0.85282


 TIME FOR THE TIME STEP             9808:        0.76220E+02

===============================================================


 INSTANT    0.980900000E-02   TIME STEP NUMBER            9809
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.297586953E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.147218612E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.157964992E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.967514328E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.463078503E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81169E-03   0.45625E-02 0.19992E+01 
c  Velocity[X]                                      0.13952E-03 
c  Velocity[Y]                                      0.13064E-03 
c  Velocity[Z]                                      0.42923E-02 
c  Pressure     0.36740E-04     133   0.93517E-02   0.25917E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.52359E-08   0.16296E-08 0.10023E+00 
c  r22          0.10849E-01      13   0.51946E-08   0.18387E-08 0.10269E+00 
c  r33          0.21854E-01      15   0.58982E-08   0.12549E-07 0.12837E+00 
c  r12          0.93829E-03      18   0.56943E-08   0.29542E-09 0.60750E+00 
c  r13          0.46663E-02      19   0.69437E-08   0.15051E-08 0.20128E+00 
c  r23          0.39963E-02      19   0.52915E-08   0.12873E-08 0.19977E+00 
c  epsilon      0.10972E+02      11   0.33534E-08   0.98941E-02 0.16627E+00 
c  TempC        0.25715E+06      16   0.15123E-04   0.84220E-02 0.43272E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381          0.6137       0.0052513       0.0015066
v  Velocity[Y]            -0.57361         0.54432       0.0030764      0.00087287
v  Velocity[Z]              1.5656          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4366          4.3406          4.3632
v  Pressure                -36.473          360.04          87.653          169.86
v  r11                   0.0010575        0.081872        0.013066        0.018282
v  r22                    0.001108        0.082624        0.013346        0.018642
v  r33                   0.0016315         0.17426        0.027234        0.037199
v  r12                   -0.010659        0.013609     -0.00023363     -0.00030922
v  r13                   -0.045559        0.052793      9.2294e-05       0.0010133
v  r23                    -0.04666        0.051172      2.9812e-05      0.00057419
v  epsilon                0.068511          271.15          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9874e-05       0.0099179      0.00092396       0.0017422
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2788         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71347         0.85282


 TIME FOR THE TIME STEP             9809:        0.76169E+02

===============================================================


 INSTANT    0.981000000E-02   TIME STEP NUMBER            9810
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.417603589E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.210659245E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.345572063E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.333185228E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.196039487E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81171E-03   0.45740E-02 0.20029E+01 
c  Velocity[X]                                      0.14029E-03 
c  Velocity[Y]                                      0.13149E-03 
c  Velocity[Z]                                      0.43022E-02 
c  Pressure     0.36649E-04     132   0.93266E-02   0.25853E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.48983E-08   0.16923E-08 0.10119E+00 
c  r22          0.10849E-01      13   0.50994E-08   0.18780E-08 0.10319E+00 
c  r33          0.21854E-01      15   0.53932E-08   0.13033E-07 0.12980E+00 
c  r12          0.93829E-03      18   0.49975E-08   0.30700E-09 0.61341E+00 
c  r13          0.46663E-02      18   0.60244E-08   0.15318E-08 0.20200E+00 
c  r23          0.39963E-02      18   0.70290E-08   0.13337E-08 0.20294E+00 
c  epsilon      0.10972E+02      11   0.32922E-08   0.10389E-01 0.16831E+00 
c  TempC        0.25715E+06      16   0.15125E-04   0.84721E-02 0.43427E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61373       0.0052513       0.0015066
v  Velocity[Y]            -0.57373         0.54448       0.0030765       0.0008729
v  Velocity[Z]              1.5658          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4366          4.3406          4.3632
v  Pressure                -36.452          360.04          87.669          169.87
v  r11                   0.0010576        0.081878        0.013066        0.018282
v  r22                    0.001108        0.082621        0.013346        0.018642
v  r33                   0.0016315         0.17428        0.027234        0.037199
v  r12                   -0.010662        0.013609     -0.00023363     -0.00030922
v  r13                   -0.045557        0.052796      9.2296e-05       0.0010133
v  r23                   -0.046659        0.051195      2.9813e-05      0.00057419
v  epsilon                0.068512          271.16          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.987e-05       0.0099179      0.00092396       0.0017422
v  CourantNb               0.44256             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2782         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71347         0.85282


 TIME FOR THE TIME STEP             9810:        0.77138E+02

===============================================================


 INSTANT    0.981100000E-02   TIME STEP NUMBER            9811
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203585120E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.266591068E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.125455019E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.167871806E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154292370E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81168E-03   0.45480E-02 0.19999E+01 
c  Velocity[X]                                      0.13950E-03 
c  Velocity[Y]                                      0.12997E-03 
c  Velocity[Z]                                      0.42786E-02 
c  Pressure     0.36634E-04     133   0.93282E-02   0.25841E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.52319E-08   0.16336E-08 0.10037E+00 
c  r22          0.10849E-01      13   0.55056E-08   0.18041E-08 0.10180E+00 
c  r33          0.21854E-01      15   0.51731E-08   0.12430E-07 0.12775E+00 
c  r12          0.93829E-03      17   0.66842E-08   0.29225E-09 0.60485E+00 
c  r13          0.46663E-02      18   0.62627E-08   0.14812E-08 0.19973E+00 
c  r23          0.39964E-02      18   0.63356E-08   0.12786E-08 0.19922E+00 
c  epsilon      0.10972E+02      11   0.32516E-08   0.97858E-02 0.16622E+00 
c  TempC        0.25715E+06      16   0.15098E-04   0.84422E-02 0.43372E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61371       0.0052513       0.0015066
v  Velocity[Y]            -0.57381         0.54429       0.0030765      0.00087291
v  Velocity[Z]              1.5657          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4366          4.3406          4.3632
v  Pressure                 -36.41          360.08          87.673          169.89
v  r11                   0.0010576        0.081884        0.013066        0.018282
v  r22                    0.001108        0.082621        0.013346        0.018642
v  r33                   0.0016315          0.1743        0.027234        0.037199
v  r12                   -0.010661        0.013611     -0.00023363     -0.00030922
v  r13                    -0.04556        0.052796      9.2299e-05       0.0010133
v  r23                    -0.04666        0.051176      2.9814e-05      0.00057419
v  epsilon                0.068512          271.19          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9869e-05       0.0099179      0.00092396       0.0017422
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2773         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71347         0.85282


 TIME FOR THE TIME STEP             9811:        0.76257E+02

===============================================================


 INSTANT    0.981200000E-02   TIME STEP NUMBER            9812
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.245178870E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.560645301E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199218582E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.135905124E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.107037648E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81191E-03   0.45464E-02 0.19975E+01 
c  Velocity[X]                                      0.13964E-03 
c  Velocity[Y]                                      0.13065E-03 
c  Velocity[Z]                                      0.42761E-02 
c  Pressure     0.36497E-04     133   0.92972E-02   0.25746E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.55839E-08   0.16388E-08 0.10048E+00 
c  r22          0.10849E-01      13   0.55524E-08   0.18234E-08 0.10232E+00 
c  r33          0.21854E-01      15   0.58107E-08   0.12538E-07 0.12839E+00 
c  r12          0.93829E-03      18   0.50260E-08   0.29700E-09 0.60845E+00 
c  r13          0.46663E-02      18   0.68212E-08   0.14757E-08 0.20006E+00 
c  r23          0.39964E-02      18   0.63633E-08   0.12758E-08 0.20005E+00 
c  epsilon      0.10972E+02      11   0.33055E-08   0.98178E-02 0.16579E+00 
c  TempC        0.25715E+06      16   0.15137E-04   0.84371E-02 0.43366E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394          0.6137       0.0052513       0.0015066
v  Velocity[Y]            -0.57381         0.54423       0.0030765      0.00087289
v  Velocity[Z]              1.5658          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4366          4.3406          4.3632
v  Pressure                -36.507          360.04          87.661          169.86
v  r11                   0.0010576        0.081888        0.013066        0.018282
v  r22                    0.001108        0.082622        0.013346        0.018642
v  r33                   0.0016315         0.17428        0.027234        0.037199
v  r12                    -0.01066        0.013604     -0.00023363     -0.00030922
v  r13                   -0.045557        0.052795      9.2301e-05       0.0010133
v  r23                    -0.04666        0.051167      2.9815e-05      0.00057419
v  epsilon                0.068513          271.19          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9868e-05       0.0099178      0.00092396       0.0017422
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2777         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71346         0.85281


 TIME FOR THE TIME STEP             9812:        0.77207E+02

===============================================================


 INSTANT    0.981300000E-02   TIME STEP NUMBER            9813
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.112991721E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.165876573E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.513785107E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.437260377E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.143993197E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81156E-03   0.45608E-02 0.19999E+01 
c  Velocity[X]                                      0.14024E-03 
c  Velocity[Y]                                      0.13033E-03 
c  Velocity[Z]                                      0.42902E-02 
c  Pressure     0.36643E-04     132   0.93215E-02   0.25849E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.59934E-08   0.16571E-08 0.10101E+00 
c  r22          0.10849E-01      13   0.57141E-08   0.18355E-08 0.10246E+00 
c  r33          0.21854E-01      15   0.59032E-08   0.12611E-07 0.12860E+00 
c  r12          0.93829E-03      18   0.49398E-08   0.29674E-09 0.60979E+00 
c  r13          0.46663E-02      19   0.52758E-08   0.14919E-08 0.20086E+00 
c  r23          0.39964E-02      18   0.69291E-08   0.12832E-08 0.20061E+00 
c  epsilon      0.10972E+02      11   0.32873E-08   0.97959E-02 0.16395E+00 
c  TempC        0.25715E+06      16   0.15114E-04   0.85003E-02 0.43512E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61372       0.0052514       0.0015067
v  Velocity[Y]            -0.57386         0.54432       0.0030765      0.00087291
v  Velocity[Z]              1.5654          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4366          4.3406          4.3632
v  Pressure                -36.454          360.06          87.653          169.87
v  r11                   0.0010576         0.08189        0.013066        0.018282
v  r22                    0.001108        0.082622        0.013346        0.018642
v  r33                   0.0016315         0.17427        0.027234        0.037199
v  r12                   -0.010662        0.013604     -0.00023363     -0.00030922
v  r13                   -0.045557        0.052794      9.2303e-05       0.0010133
v  r23                   -0.046661        0.051198      2.9816e-05       0.0005742
v  epsilon                0.068513          271.15          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9867e-05       0.0099176      0.00092396       0.0017422
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2778         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71346         0.85281


 TIME FOR THE TIME STEP             9813:        0.78467E+02

===============================================================


 INSTANT    0.981400000E-02   TIME STEP NUMBER            9814
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.660811341E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.163944667E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.373420177E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.198080992E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.202742291E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81200E-03   0.45740E-02 0.20029E+01 
c  Velocity[X]                                      0.14060E-03 
c  Velocity[Y]                                      0.13066E-03 
c  Velocity[Z]                                      0.43027E-02 
c  Pressure     0.36669E-04     132   0.93412E-02   0.25866E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.63793E-08   0.16940E-08 0.10170E+00 
c  r22          0.10849E-01      13   0.58737E-08   0.18433E-08 0.10315E+00 
c  r33          0.21854E-01      15   0.68652E-08   0.12815E-07 0.12989E+00 
c  r12          0.93829E-03      17   0.64840E-08   0.29946E-09 0.61167E+00 
c  r13          0.46663E-02      19   0.62887E-08   0.14914E-08 0.20156E+00 
c  r23          0.39964E-02      18   0.70210E-08   0.13342E-08 0.20380E+00 
c  epsilon      0.10972E+02      11   0.33016E-08   0.10310E-01 0.17293E+00 
c  TempC        0.25715E+06      16   0.15138E-04   0.83846E-02 0.43159E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162017


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61372       0.0052514       0.0015067
v  Velocity[Y]            -0.57398         0.54443       0.0030765      0.00087288
v  Velocity[Z]              1.5657          5.4366          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4366          4.3406          4.3632
v  Pressure                -36.503          359.99          87.626          169.82
v  r11                   0.0010576        0.081887        0.013066        0.018282
v  r22                    0.001108        0.082622        0.013346        0.018642
v  r33                   0.0016316         0.17427        0.027234        0.037199
v  r12                    -0.01066        0.013605     -0.00023363     -0.00030922
v  r13                   -0.045559        0.052796      9.2305e-05       0.0010133
v  r23                   -0.046662        0.051183      2.9817e-05       0.0005742
v  epsilon                0.068514          271.16          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9868e-05       0.0099177      0.00092396       0.0017422
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2774         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71347         0.85282


 TIME FOR THE TIME STEP             9814:        0.76496E+02

===============================================================


 INSTANT    0.981500000E-02   TIME STEP NUMBER            9815
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.523148067E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226205595E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934895E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.142970411E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.448903952E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.146001828E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81172E-03   0.45499E-02 0.19983E+01 
c  Velocity[X]                                      0.13924E-03 
c  Velocity[Y]                                      0.13117E-03 
c  Velocity[Z]                                      0.42795E-02 
c  Pressure     0.36283E-04     131   0.92419E-02   0.25594E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.61422E-08   0.16453E-08 0.10009E+00 
c  r22          0.10849E-01      13   0.57490E-08   0.18537E-08 0.10275E+00 
c  r33          0.21854E-01      15   0.71594E-08   0.12643E-07 0.12833E+00 
c  r12          0.93829E-03      18   0.49983E-08   0.30373E-09 0.61255E+00 
c  r13          0.46663E-02      19   0.59117E-08   0.15170E-08 0.20170E+00 
c  r23          0.39964E-02      19   0.52785E-08   0.12968E-08 0.20005E+00 
c  epsilon      0.10972E+02      11   0.33044E-08   0.99454E-02 0.16540E+00 
c  TempC        0.25715E+06      16   0.15089E-04   0.84196E-02 0.43250E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162021


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393         0.61372       0.0052514       0.0015067
v  Velocity[Y]             -0.5738         0.54423       0.0030766      0.00087294
v  Velocity[Z]              1.5657          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4367          4.3406          4.3632
v  Pressure                -36.467          360.13          87.734          169.95
v  r11                   0.0010577        0.081883        0.013066        0.018282
v  r22                    0.001108        0.082623        0.013346        0.018642
v  r33                   0.0016316          0.1743        0.027234        0.037199
v  r12                    -0.01066        0.013598     -0.00023363     -0.00030922
v  r13                   -0.045557        0.052796      9.2308e-05       0.0010133
v  r23                   -0.046663        0.051172      2.9819e-05       0.0005742
v  epsilon                0.068515          271.16          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9869e-05       0.0099178      0.00092396       0.0017422
v  CourantNb               0.44259             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2776         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71347         0.85282


 TIME FOR THE TIME STEP             9815:        0.76969E+02

===============================================================


 INSTANT    0.981600000E-02   TIME STEP NUMBER            9816
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.998618119E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.385610184E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.159369960E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.351624237E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.102563809E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81196E-03   0.45576E-02 0.19994E+01 
c  Velocity[X]                                      0.14031E-03 
c  Velocity[Y]                                      0.12990E-03 
c  Velocity[Z]                                      0.42874E-02 
c  Pressure     0.36573E-04     133   0.93111E-02   0.25800E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.59743E-08   0.16446E-08 0.10008E+00 
c  r22          0.10849E-01      13   0.54517E-08   0.18585E-08 0.10240E+00 
c  r33          0.21854E-01      15   0.62914E-08   0.12705E-07 0.12810E+00 
c  r12          0.93829E-03      17   0.69520E-08   0.29886E-09 0.60799E+00 
c  r13          0.46663E-02      19   0.54016E-08   0.15394E-08 0.20140E+00 
c  r23          0.39964E-02      19   0.62074E-08   0.12913E-08 0.19964E+00 
c  epsilon      0.10972E+02      11   0.32632E-08   0.10156E-01 0.16648E+00 
c  TempC        0.25715E+06      16   0.15137E-04   0.84422E-02 0.43383E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61376       0.0052515       0.0015067
v  Velocity[Y]             -0.5739         0.54421       0.0030766      0.00087296
v  Velocity[Z]              1.5657          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4367          4.3406          4.3632
v  Pressure                 -36.47          360.03          87.666          169.86
v  r11                   0.0010577        0.081885        0.013066        0.018282
v  r22                   0.0011081        0.082622        0.013346        0.018642
v  r33                   0.0016316         0.17429        0.027234        0.037199
v  r12                   -0.010659        0.013599     -0.00023363     -0.00030922
v  r13                   -0.045556        0.052796       9.231e-05       0.0010133
v  r23                   -0.046664        0.051192       2.982e-05       0.0005742
v  epsilon                0.068515          271.17          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9868e-05       0.0099178      0.00092397       0.0017422
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2775         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71347         0.85282


 TIME FOR THE TIME STEP             9816:        0.75465E+02

===============================================================


 INSTANT    0.981700000E-02   TIME STEP NUMBER            9817
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162118818E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21878E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.164497050E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21878E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.221172612E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935017E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21878E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.402352333E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21878E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.909742758E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21878E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81167E-03   0.45532E-02 0.19980E+01 
c  Velocity[X]                                      0.13902E-03 
c  Velocity[Y]                                      0.12910E-03 
c  Velocity[Z]                                      0.42851E-02 
c  Pressure     0.36647E-04     131   0.93303E-02   0.25850E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.55140E-08   0.16486E-08 0.10047E+00 
c  r22          0.10849E-01      13   0.53417E-08   0.18169E-08 0.10209E+00 
c  r33          0.21854E-01      15   0.60238E-08   0.12538E-07 0.12812E+00 
c  r12          0.93829E-03      17   0.69173E-08   0.30266E-09 0.61208E+00 
c  r13          0.46663E-02      19   0.61242E-08   0.15036E-08 0.20030E+00 
c  r23          0.39964E-02      20   0.64790E-08   0.12875E-08 0.19994E+00 
c  epsilon      0.10972E+02      11   0.35146E-08   0.97389E-02 0.16449E+00 
c  TempC        0.25715E+06      16   0.15095E-04   0.84004E-02 0.43313E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61376       0.0052515       0.0015067
v  Velocity[Y]            -0.57391         0.54428       0.0030766      0.00087294
v  Velocity[Z]              1.5657          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4367          4.3406          4.3632
v  Pressure                -36.472          360.01          87.625          169.83
v  r11                   0.0010577        0.081887        0.013066        0.018282
v  r22                   0.0011081        0.082619        0.013346        0.018642
v  r33                   0.0016316         0.17425        0.027234        0.037199
v  r12                   -0.010659          0.0136     -0.00023364     -0.00030922
v  r13                    -0.04556        0.052797      9.2313e-05       0.0010133
v  r23                   -0.046666        0.051187       2.982e-05       0.0005742
v  epsilon                0.068516          271.13          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9868e-05       0.0099178      0.00092397       0.0017422
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2772         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71347         0.85282


 TIME FOR THE TIME STEP             9817:        0.76894E+02

===============================================================


 INSTANT    0.981800000E-02   TIME STEP NUMBER            9818
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239031743E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.297830842E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237684288E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.265682004E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.323959782E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81183E-03   0.45501E-02 0.19989E+01 
c  Velocity[X]                                      0.14031E-03 
c  Velocity[Y]                                      0.13060E-03 
c  Velocity[Z]                                      0.42791E-02 
c  Pressure     0.36648E-04     131   0.93252E-02   0.25851E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.57535E-08   0.16730E-08 0.10091E+00 
c  r22          0.10849E-01      13   0.56284E-08   0.18146E-08 0.10217E+00 
c  r33          0.21854E-01      15   0.50383E-08   0.12650E-07 0.12868E+00 
c  r12          0.93829E-03      18   0.52320E-08   0.29404E-09 0.60766E+00 
c  r13          0.46663E-02      19   0.57730E-08   0.14662E-08 0.19954E+00 
c  r23          0.39964E-02      19   0.66498E-08   0.13033E-08 0.20112E+00 
c  epsilon      0.10972E+02      11   0.32923E-08   0.98959E-02 0.16611E+00 
c  TempC        0.25715E+06      16   0.15142E-04   0.85119E-02 0.43541E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61374       0.0052515       0.0015067
v  Velocity[Y]             -0.5739         0.54434       0.0030766      0.00087293
v  Velocity[Z]              1.5658          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4367          4.3406          4.3632
v  Pressure                -36.485          359.96          87.629          169.81
v  r11                   0.0010577        0.081885        0.013066        0.018282
v  r22                   0.0011081        0.082621        0.013346        0.018642
v  r33                   0.0016316         0.17427        0.027234        0.037199
v  r12                   -0.010666        0.013602     -0.00023364     -0.00030922
v  r13                   -0.045556        0.052798      9.2315e-05       0.0010133
v  r23                   -0.046668        0.051172      2.9822e-05       0.0005742
v  epsilon                0.068517          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.987e-05       0.0099179      0.00092397       0.0017422
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2778         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71347         0.85282


 TIME FOR THE TIME STEP             9818:        0.75821E+02

===============================================================


 INSTANT    0.981900000E-02   TIME STEP NUMBER            9819
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.651079586E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.143893639E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.978276926E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.342328314E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.206089441E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40344E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81154E-03   0.45762E-02 0.20046E+01 
c  Velocity[X]                                      0.14070E-03 
c  Velocity[Y]                                      0.13089E-03 
c  Velocity[Z]                                      0.43046E-02 
c  Pressure     0.36771E-04     131   0.93665E-02   0.25939E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.56171E-08   0.16636E-08 0.10058E+00 
c  r22          0.10849E-01      13   0.54576E-08   0.18590E-08 0.10262E+00 
c  r33          0.21854E-01      15   0.53985E-08   0.12721E-07 0.12858E+00 
c  r12          0.93829E-03      18   0.51935E-08   0.30195E-09 0.61190E+00 
c  r13          0.46663E-02      19   0.59191E-08   0.14957E-08 0.20008E+00 
c  r23          0.39964E-02      19   0.54623E-08   0.12924E-08 0.20031E+00 
c  epsilon      0.10972E+02      11   0.32579E-08   0.10007E-01 0.16648E+00 
c  TempC        0.25715E+06      16   0.15114E-04   0.85054E-02 0.43473E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61375       0.0052514       0.0015066
v  Velocity[Y]            -0.57378         0.54445       0.0030767      0.00087297
v  Velocity[Z]              1.5657          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4367          4.3406          4.3632
v  Pressure                -36.424          360.06          87.661          169.88
v  r11                   0.0010577        0.081882        0.013066        0.018282
v  r22                   0.0011081        0.082624        0.013346        0.018642
v  r33                   0.0016316          0.1743        0.027234        0.037199
v  r12                   -0.010665        0.013599     -0.00023364     -0.00030922
v  r13                   -0.045556        0.052797      9.2318e-05       0.0010133
v  r23                   -0.046671        0.051196      2.9824e-05       0.0005742
v  epsilon                0.068517          271.19          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9871e-05       0.0099182      0.00092397       0.0017422
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2784         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71347         0.85282


 TIME FOR THE TIME STEP             9819:        0.78715E+02

===============================================================


 INSTANT    0.982000000E-02   TIME STEP NUMBER            9820
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.159988407E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.182497401E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.975034781E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.327772046E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.975768721E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81224E-03   0.45499E-02 0.19969E+01 
c  Velocity[X]                                      0.14015E-03 
c  Velocity[Y]                                      0.13022E-03 
c  Velocity[Z]                                      0.42795E-02 
c  Pressure     0.36309E-04     132   0.92443E-02   0.25612E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.58393E-08   0.17002E-08 0.10176E+00 
c  r22          0.10849E-01      13   0.52781E-08   0.18590E-08 0.10282E+00 
c  r33          0.21854E-01      15   0.52530E-08   0.12955E-07 0.13001E+00 
c  r12          0.93829E-03      18   0.55671E-08   0.30402E-09 0.61313E+00 
c  r13          0.46663E-02      19   0.56140E-08   0.15212E-08 0.20150E+00 
c  r23          0.39964E-02      19   0.57316E-08   0.13364E-08 0.20408E+00 
c  epsilon      0.10972E+02      11   0.32272E-08   0.10453E-01 0.17311E+00 
c  TempC        0.25715E+06      16   0.15116E-04   0.83798E-02 0.43219E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61376       0.0052514       0.0015066
v  Velocity[Y]            -0.57377         0.54428       0.0030765       0.0008729
v  Velocity[Z]              1.5655          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4367          4.3406          4.3632
v  Pressure                -36.487          360.09          87.701          169.91
v  r11                   0.0010578        0.081882        0.013066        0.018282
v  r22                   0.0011081        0.082626        0.013346        0.018642
v  r33                   0.0016317         0.17428        0.027234        0.037199
v  r12                   -0.010659        0.013599     -0.00023364     -0.00030922
v  r13                   -0.045559        0.052798      9.2319e-05       0.0010133
v  r23                   -0.046673         0.05118      2.9824e-05       0.0005742
v  epsilon                0.068518          271.18          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9873e-05       0.0099182      0.00092397       0.0017422
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2789         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71347         0.85282


 TIME FOR THE TIME STEP             9820:        0.77684E+02

===============================================================


 INSTANT    0.982100000E-02   TIME STEP NUMBER            9821
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.114006344E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.274409428E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.333752099E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117624560E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.361283816E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40345E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81172E-03   0.45526E-02 0.19958E+01 
c  Velocity[X]                                      0.13953E-03 
c  Velocity[Y]                                      0.13033E-03 
c  Velocity[Z]                                      0.42828E-02 
c  Pressure     0.36654E-04     131   0.93326E-02   0.25856E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.53670E-08   0.16517E-08 0.10079E+00 
c  r22          0.10849E-01      13   0.50765E-08   0.18630E-08 0.10305E+00 
c  r33          0.21854E-01      15   0.54953E-08   0.12656E-07 0.12881E+00 
c  r12          0.93830E-03      18   0.57351E-08   0.30491E-09 0.61148E+00 
c  r13          0.46663E-02      19   0.59128E-08   0.14953E-08 0.20031E+00 
c  r23          0.39964E-02      19   0.60817E-08   0.12907E-08 0.20110E+00 
c  epsilon      0.10972E+02      11   0.32725E-08   0.99002E-02 0.16489E+00 
c  TempC        0.25715E+06      16   0.15133E-04   0.84040E-02 0.43260E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338         0.61376       0.0052515       0.0015066
v  Velocity[Y]            -0.57377         0.54423       0.0030766      0.00087292
v  Velocity[Z]              1.5656          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4367          4.3406          4.3632
v  Pressure                 -36.44          360.05          87.672          169.88
v  r11                   0.0010578        0.081882        0.013066        0.018282
v  r22                   0.0011081        0.082628        0.013346        0.018642
v  r33                   0.0016317         0.17425        0.027234        0.037199
v  r12                   -0.010656        0.013593     -0.00023364     -0.00030922
v  r13                   -0.045558        0.052798      9.2321e-05       0.0010133
v  r23                   -0.046675         0.05116      2.9825e-05       0.0005742
v  epsilon                0.068518          271.13          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9878e-05       0.0099183      0.00092397       0.0017422
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2782         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71347         0.85282


 TIME FOR THE TIME STEP             9821:        0.77389E+02

===============================================================


 INSTANT    0.982200000E-02   TIME STEP NUMBER            9822
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.372906360E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.448771595E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221805901E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.513713930E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.259031215E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21879E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81121E-03   0.45925E-02 0.20077E+01 
c  Velocity[X]                                      0.14068E-03 
c  Velocity[Y]                                      0.13099E-03 
c  Velocity[Z]                                      0.43208E-02 
c  Pressure     0.36908E-04     133   0.93973E-02   0.26034E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.54138E-08   0.16424E-08 0.10055E+00 
c  r22          0.10849E-01      13   0.52600E-08   0.18419E-08 0.10313E+00 
c  r33          0.21854E-01      15   0.52474E-08   0.12517E-07 0.12847E+00 
c  r12          0.93830E-03      18   0.61954E-08   0.29657E-09 0.60824E+00 
c  r13          0.46663E-02      19   0.61712E-08   0.15002E-08 0.20137E+00 
c  r23          0.39964E-02      19   0.60870E-08   0.12909E-08 0.20056E+00 
c  epsilon      0.10972E+02      11   0.32460E-08   0.97729E-02 0.16398E+00 
c  TempC        0.25715E+06      16   0.15122E-04   0.84807E-02 0.43452E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61377       0.0052515       0.0015067
v  Velocity[Y]            -0.57381         0.54433       0.0030766      0.00087289
v  Velocity[Z]              1.5655          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4367          4.3406          4.3632
v  Pressure                -36.466          360.01          87.649          169.84
v  r11                   0.0010578        0.081882        0.013066        0.018282
v  r22                   0.0011081        0.082629        0.013346        0.018642
v  r33                   0.0016317         0.17427        0.027234        0.037199
v  r12                   -0.010657        0.013594     -0.00023364     -0.00030922
v  r13                   -0.045556        0.052796      9.2325e-05       0.0010133
v  r23                   -0.046677        0.051142      2.9826e-05       0.0005742
v  epsilon                0.068519          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9883e-05       0.0099181      0.00092398       0.0017422
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2774         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71347         0.85282


 TIME FOR THE TIME STEP             9822:        0.79646E+02

===============================================================


 INSTANT    0.982300000E-02   TIME STEP NUMBER            9823
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.599813123E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.327480869E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.873534601E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141737483E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.732443773E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81173E-03   0.45596E-02 0.19973E+01 
c  Velocity[X]                                      0.13857E-03 
c  Velocity[Y]                                      0.12968E-03 
c  Velocity[Z]                                      0.42913E-02 
c  Pressure     0.36280E-04     132   0.92378E-02   0.25592E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.54351E-08   0.16709E-08 0.10126E+00 
c  r22          0.10849E-01      13   0.51499E-08   0.18675E-08 0.10336E+00 
c  r33          0.21854E-01      15   0.52973E-08   0.12830E-07 0.12960E+00 
c  r12          0.93830E-03      18   0.56824E-08   0.30287E-09 0.61602E+00 
c  r13          0.46663E-02      19   0.53615E-08   0.15316E-08 0.20278E+00 
c  r23          0.39964E-02      19   0.56600E-08   0.13056E-08 0.20182E+00 
c  epsilon      0.10972E+02      11   0.33425E-08   0.10150E-01 0.16796E+00 
c  TempC        0.25715E+06      16   0.15088E-04   0.84856E-02 0.43451E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338         0.61378       0.0052515       0.0015067
v  Velocity[Y]            -0.57381          0.5444       0.0030765      0.00087287
v  Velocity[Z]              1.5654          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4367          4.3406          4.3632
v  Pressure                 -36.45          360.07          87.679          169.89
v  r11                   0.0010578        0.081874        0.013066        0.018282
v  r22                   0.0011081        0.082629        0.013346        0.018642
v  r33                   0.0016317         0.17429        0.027234        0.037199
v  r12                   -0.010657        0.013597     -0.00023364     -0.00030922
v  r13                   -0.045559        0.052794      9.2327e-05       0.0010133
v  r23                   -0.046679        0.051175      2.9827e-05      0.00057421
v  epsilon                0.068519          271.18          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.989e-05       0.0099179      0.00092398       0.0017422
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2778         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71347         0.85281


 TIME FOR THE TIME STEP             9823:        0.78624E+02

===============================================================


 INSTANT    0.982400000E-02   TIME STEP NUMBER            9824
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.501286165E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.797369740E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136236466E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.836297795E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172763769E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40346E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81260E-03   0.45235E-02 0.19934E+01 
c  Velocity[X]                                      0.13986E-03 
c  Velocity[Y]                                      0.12987E-03 
c  Velocity[Z]                                      0.42538E-02 
c  Pressure     0.36610E-04     132   0.93205E-02   0.25826E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.56849E-08   0.16261E-08 0.10005E+00 
c  r22          0.10849E-01      13   0.51209E-08   0.18355E-08 0.10239E+00 
c  r33          0.21854E-01      15   0.52653E-08   0.12488E-07 0.12793E+00 
c  r12          0.93830E-03      18   0.55592E-08   0.29578E-09 0.60718E+00 
c  r13          0.46663E-02      18   0.72267E-08   0.14840E-08 0.19986E+00 
c  r23          0.39964E-02      19   0.58015E-08   0.12684E-08 0.19922E+00 
c  epsilon      0.10972E+02      11   0.33315E-08   0.98891E-02 0.16536E+00 
c  TempC        0.25715E+06      16   0.15145E-04   0.84782E-02 0.43433E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61375       0.0052515       0.0015067
v  Velocity[Y]            -0.57375         0.54449       0.0030766      0.00087292
v  Velocity[Z]              1.5654          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4367          4.3406          4.3632
v  Pressure                -36.426          360.06          87.678          169.88
v  r11                   0.0010578         0.08187        0.013066        0.018282
v  r22                   0.0011081        0.082628        0.013346        0.018642
v  r33                   0.0016317         0.17428        0.027234        0.037199
v  r12                   -0.010657        0.013602     -0.00023364     -0.00030922
v  r13                   -0.045556        0.052796      9.2329e-05       0.0010133
v  r23                   -0.046681        0.051169      2.9828e-05      0.00057421
v  epsilon                 0.06852          271.17          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9894e-05       0.0099176      0.00092398       0.0017422
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2784         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71346         0.85281


 TIME FOR THE TIME STEP             9824:        0.78447E+02

===============================================================


 INSTANT    0.982500000E-02   TIME STEP NUMBER            9825
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.823441742E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.645598921E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.271620788E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.835018957E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.456875229E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81091E-03   0.46135E-02 0.20122E+01 
c  Velocity[X]                                      0.14076E-03 
c  Velocity[Y]                                      0.13116E-03 
c  Velocity[Z]                                      0.43416E-02 
c  Pressure     0.36908E-04     132   0.93966E-02   0.26035E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.50446E-08   0.16606E-08 0.10070E+00 
c  r22          0.10849E-01      13   0.48469E-08   0.18539E-08 0.10253E+00 
c  r33          0.21854E-01      15   0.55949E-08   0.12701E-07 0.12840E+00 
c  r12          0.93830E-03      17   0.66867E-08   0.29829E-09 0.60689E+00 
c  r13          0.46663E-02      18   0.67899E-08   0.15023E-08 0.20006E+00 
c  r23          0.39964E-02      19   0.59076E-08   0.12927E-08 0.19976E+00 
c  epsilon      0.10972E+02      11   0.33419E-08   0.10200E-01 0.16692E+00 
c  TempC        0.25715E+06      16   0.15089E-04   0.84424E-02 0.43372E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63372         0.61376       0.0052515       0.0015067
v  Velocity[Y]            -0.57365          0.5443       0.0030766      0.00087293
v  Velocity[Z]              1.5652          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4367          4.3406          4.3632
v  Pressure                  -36.4          360.08           87.68           169.9
v  r11                   0.0010579        0.081865        0.013066        0.018282
v  r22                   0.0011082        0.082627        0.013346        0.018642
v  r33                   0.0016318         0.17425        0.027234        0.037199
v  r12                   -0.010657        0.013599     -0.00023364     -0.00030922
v  r13                   -0.045557        0.052794      9.2332e-05       0.0010133
v  r23                   -0.046682        0.051163       2.983e-05      0.00057421
v  epsilon                0.068521          271.12          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9897e-05       0.0099176      0.00092398       0.0017422
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2787         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71347         0.85282


 TIME FOR THE TIME STEP             9825:        0.77517E+02

===============================================================


 INSTANT    0.982600000E-02   TIME STEP NUMBER            9826
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.104664962E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.607997052E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.255582983E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.270313454E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.180430120E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81278E-03   0.45831E-02 0.20027E+01 
c  Velocity[X]                                      0.13997E-03 
c  Velocity[Y]                                      0.13130E-03 
c  Velocity[Z]                                      0.43118E-02 
c  Pressure     0.36574E-04     133   0.93214E-02   0.25799E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.54001E-08   0.16359E-08 0.10067E+00 
c  r22          0.10849E-01      13   0.49779E-08   0.18452E-08 0.10298E+00 
c  r33          0.21854E-01      15   0.59881E-08   0.12503E-07 0.12874E+00 
c  r12          0.93830E-03      18   0.49837E-08   0.30806E-09 0.61470E+00 
c  r13          0.46663E-02      19   0.67387E-08   0.14896E-08 0.20112E+00 
c  r23          0.39964E-02      19   0.59671E-08   0.12950E-08 0.20193E+00 
c  epsilon      0.10972E+02      11   0.32823E-08   0.97533E-02 0.16805E+00 
c  TempC        0.25715E+06      16   0.15128E-04   0.83902E-02 0.43227E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61377       0.0052515       0.0015067
v  Velocity[Y]             -0.5738          0.5444       0.0030766      0.00087291
v  Velocity[Z]              1.5654          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4367          4.3406          4.3632
v  Pressure                -36.463          360.02          87.662          169.85
v  r11                   0.0010579        0.081861        0.013066        0.018282
v  r22                   0.0011082        0.082626        0.013346        0.018642
v  r33                   0.0016318         0.17427        0.027234        0.037199
v  r12                   -0.010661        0.013602     -0.00023364     -0.00030922
v  r13                    -0.04556        0.052796      9.2335e-05       0.0010133
v  r23                   -0.046684        0.051189      2.9831e-05      0.00057421
v  epsilon                0.068521          271.13          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9899e-05       0.0099176      0.00092398       0.0017422
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2787         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71347         0.85282


 TIME FOR THE TIME STEP             9826:        0.78315E+02

===============================================================


 INSTANT    0.982700000E-02   TIME STEP NUMBER            9827
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171525023E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.985718813E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934911E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.393088794E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.352748442E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.778573072E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81178E-03   0.45788E-02 0.20026E+01 
c  Velocity[X]                                      0.13904E-03 
c  Velocity[Y]                                      0.13013E-03 
c  Velocity[Z]                                      0.43096E-02 
c  Pressure     0.36545E-04     133   0.93110E-02   0.25778E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.52285E-08   0.16264E-08 0.99961E-01 
c  r22          0.10849E-01      13   0.51802E-08   0.18476E-08 0.10294E+00 
c  r33          0.21854E-01      15   0.67810E-08   0.12536E-07 0.12839E+00 
c  r12          0.93830E-03      18   0.60171E-08   0.29534E-09 0.60621E+00 
c  r13          0.46663E-02      19   0.66985E-08   0.14919E-08 0.20067E+00 
c  r23          0.39964E-02      19   0.54438E-08   0.12688E-08 0.19928E+00 
c  epsilon      0.10972E+02      11   0.32818E-08   0.96615E-02 0.16362E+00 
c  TempC        0.25715E+06      16   0.15112E-04   0.84577E-02 0.43403E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61376       0.0052515       0.0015066
v  Velocity[Y]            -0.57366          0.5441       0.0030766       0.0008729
v  Velocity[Z]              1.5654          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4367          4.3406          4.3632
v  Pressure                -36.414          360.09          87.701          169.92
v  r11                   0.0010579        0.081861        0.013066        0.018282
v  r22                   0.0011082        0.082621        0.013346        0.018642
v  r33                   0.0016318          0.1743        0.027234        0.037199
v  r12                    -0.01066        0.013606     -0.00023364     -0.00030922
v  r13                   -0.045557        0.052794      9.2337e-05       0.0010133
v  r23                   -0.046686        0.051192      2.9833e-05      0.00057421
v  epsilon                0.068522          271.16          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc               5.99e-05       0.0099177      0.00092398       0.0017422
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2782         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71347         0.85282


 TIME FOR THE TIME STEP             9827:        0.79916E+02

===============================================================


 INSTANT    0.982800000E-02   TIME STEP NUMBER            9828
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.453398773E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69794E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138450471E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69794E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.423439038E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69794E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.358977543E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69794E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.424270237E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69794E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81112E-03   0.45493E-02 0.20000E+01 
c  Velocity[X]                                      0.14045E-03 
c  Velocity[Y]                                      0.13113E-03 
c  Velocity[Z]                                      0.42777E-02 
c  Pressure     0.36463E-04     132   0.92874E-02   0.25722E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.55130E-08   0.16354E-08 0.10006E+00 
c  r22          0.10849E-01      13   0.45016E-08   0.18403E-08 0.10213E+00 
c  r33          0.21854E-01      15   0.56313E-08   0.12536E-07 0.12773E+00 
c  r12          0.93830E-03      18   0.49736E-08   0.29738E-09 0.60650E+00 
c  r13          0.46663E-02      19   0.61524E-08   0.15029E-08 0.20053E+00 
c  r23          0.39964E-02      19   0.57116E-08   0.12831E-08 0.19901E+00 
c  epsilon      0.10972E+02      11   0.33112E-08   0.99228E-02 0.16494E+00 
c  TempC        0.25715E+06      16   0.15117E-04   0.85045E-02 0.43522E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61375       0.0052515       0.0015066
v  Velocity[Y]            -0.57356         0.54419       0.0030765      0.00087284
v  Velocity[Z]              1.5653          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4367          4.3406          4.3632
v  Pressure                -36.442          360.02          87.653          169.85
v  r11                   0.0010579        0.081862        0.013066        0.018282
v  r22                   0.0011082        0.082622        0.013346        0.018642
v  r33                   0.0016318          0.1743        0.027234        0.037199
v  r12                   -0.010666        0.013603     -0.00023364     -0.00030922
v  r13                   -0.045556        0.052794      9.2339e-05       0.0010133
v  r23                   -0.046687        0.051178      2.9834e-05      0.00057421
v  epsilon                0.068523          271.16          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9898e-05       0.0099177      0.00092398       0.0017422
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2785         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71347         0.85282


 TIME FOR THE TIME STEP             9828:        0.77791E+02

===============================================================


 INSTANT    0.982900000E-02   TIME STEP NUMBER            9829
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173841832E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69794E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.174652385E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69794E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.886612940E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69794E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.231762987E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69794E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.365989390E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69794E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81268E-03   0.45727E-02 0.20006E+01 
c  Velocity[X]                                      0.13965E-03 
c  Velocity[Y]                                      0.12977E-03 
c  Velocity[Z]                                      0.43033E-02 
c  Pressure     0.36867E-04     132   0.93849E-02   0.26006E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.54328E-08   0.16117E-08 0.99489E-01 
c  r22          0.10849E-01      13   0.47559E-08   0.18398E-08 0.10209E+00 
c  r33          0.21854E-01      15   0.65624E-08   0.12466E-07 0.12760E+00 
c  r12          0.93830E-03      18   0.49940E-08   0.29338E-09 0.60525E+00 
c  r13          0.46663E-02      19   0.58102E-08   0.14963E-08 0.20032E+00 
c  r23          0.39964E-02      19   0.62767E-08   0.12557E-08 0.19745E+00 
c  epsilon      0.10972E+02      11   0.35112E-08   0.99108E-02 0.16598E+00 
c  TempC        0.25715E+06      16   0.15135E-04   0.83871E-02 0.43208E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61378       0.0052516       0.0015067
v  Velocity[Y]            -0.57376          0.5443       0.0030766      0.00087285
v  Velocity[Z]              1.5654          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4367          4.3406          4.3632
v  Pressure                -36.476          360.11          87.704          169.92
v  r11                   0.0010579        0.081865        0.013066        0.018282
v  r22                   0.0011082        0.082624        0.013346        0.018642
v  r33                   0.0016318         0.17427        0.027234        0.037199
v  r12                   -0.010665        0.013599     -0.00023364     -0.00030922
v  r13                   -0.045559        0.052796      9.2342e-05       0.0010133
v  r23                   -0.046689        0.051204      2.9836e-05      0.00057421
v  epsilon                0.068523          271.13          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9894e-05       0.0099177      0.00092399       0.0017422
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2786         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71347         0.85282


 TIME FOR THE TIME STEP             9829:        0.78378E+02

===============================================================


 INSTANT    0.983000000E-02   TIME STEP NUMBER            9830
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166709516E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.254760428E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117471687E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.597030430E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.504537150E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81196E-03   0.45622E-02 0.19985E+01 
c  Velocity[X]                                      0.13993E-03 
c  Velocity[Y]                                      0.13014E-03 
c  Velocity[Z]                                      0.42921E-02 
c  Pressure     0.36313E-04     133   0.92504E-02   0.25615E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.63404E-08   0.16913E-08 0.10121E+00 
c  r22          0.10849E-01      13   0.47206E-08   0.18752E-08 0.10304E+00 
c  r33          0.21854E-01      15   0.58479E-08   0.12944E-07 0.12960E+00 
c  r12          0.93830E-03      18   0.49887E-08   0.30724E-09 0.61360E+00 
c  r13          0.46663E-02      19   0.57228E-08   0.15370E-08 0.20222E+00 
c  r23          0.39964E-02      19   0.62003E-08   0.13196E-08 0.20232E+00 
c  epsilon      0.10972E+02      11   0.35077E-08   0.10261E-01 0.16845E+00 
c  TempC        0.25715E+06      16   0.15095E-04   0.83903E-02 0.43174E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61372       0.0052516       0.0015067
v  Velocity[Y]            -0.57367         0.54449       0.0030766      0.00087284
v  Velocity[Z]              1.5652          5.4367          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4367          4.3406          4.3632
v  Pressure                 -36.45          360.04          87.671          169.86
v  r11                    0.001058        0.081873        0.013066        0.018282
v  r22                   0.0011082        0.082626        0.013346        0.018642
v  r33                   0.0016319         0.17428        0.027234        0.037199
v  r12                   -0.010663        0.013601     -0.00023364     -0.00030922
v  r13                   -0.045556        0.052798      9.2344e-05       0.0010133
v  r23                    -0.04669        0.051192      2.9837e-05      0.00057421
v  epsilon                0.068524          271.13          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.989e-05       0.0099178      0.00092399       0.0017422
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2786         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71347         0.85282


 TIME FOR THE TIME STEP             9830:        0.78039E+02

===============================================================


 INSTANT    0.983100000E-02   TIME STEP NUMBER            9831
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.352163660E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.467209455E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.237222588E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.630324243E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.334532517E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81149E-03   0.45841E-02 0.20054E+01 
c  Velocity[X]                                      0.14037E-03 
c  Velocity[Y]                                      0.13098E-03 
c  Velocity[Z]                                      0.43127E-02 
c  Pressure     0.36725E-04     132   0.93547E-02   0.25905E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.62750E-08   0.17316E-08 0.10273E+00 
c  r22          0.10849E-01      12   0.65798E-08   0.18764E-08 0.10313E+00 
c  r33          0.21854E-01      15   0.55571E-08   0.13000E-07 0.13014E+00 
c  r12          0.93830E-03      18   0.56332E-08   0.31066E-09 0.61827E+00 
c  r13          0.46664E-02      19   0.56184E-08   0.15129E-08 0.20156E+00 
c  r23          0.39964E-02      19   0.63810E-08   0.13340E-08 0.20424E+00 
c  epsilon      0.10972E+02      11   0.34564E-08   0.10145E-01 0.16822E+00 
c  TempC        0.25715E+06      16   0.15100E-04   0.84712E-02 0.43443E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63372         0.61375       0.0052515       0.0015066
v  Velocity[Y]            -0.57363         0.54427       0.0030766      0.00087286
v  Velocity[Z]              1.5652          5.4367          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4367          4.3406          4.3632
v  Pressure                 -36.43          360.06          87.667          169.87
v  r11                    0.001058        0.081876        0.013066        0.018282
v  r22                   0.0011082        0.082628        0.013346        0.018642
v  r33                   0.0016319         0.17431        0.027234        0.037199
v  r12                   -0.010662        0.013603     -0.00023364     -0.00030922
v  r13                   -0.045556        0.052798      9.2347e-05       0.0010133
v  r23                   -0.046691        0.051171      2.9839e-05      0.00057422
v  epsilon                0.068524          271.16          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9887e-05       0.0099177      0.00092399       0.0017423
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2784         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71347         0.85282


 TIME FOR THE TIME STEP             9831:        0.76689E+02

===============================================================


 INSTANT    0.983200000E-02   TIME STEP NUMBER            9832
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.510849076E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.957462198E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.722469388E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.411673124E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.240121118E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81226E-03   0.45052E-02 0.19909E+01 
c  Velocity[X]                                      0.14001E-03 
c  Velocity[Y]                                      0.12972E-03 
c  Velocity[Z]                                      0.42354E-02 
c  Pressure     0.36679E-04     133   0.93388E-02   0.25873E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.56487E-08   0.16747E-08 0.10117E+00 
c  r22          0.10849E-01      12   0.65318E-08   0.18400E-08 0.10242E+00 
c  r33          0.21854E-01      14   0.67830E-08   0.12679E-07 0.12877E+00 
c  r12          0.93830E-03      18   0.54039E-08   0.30342E-09 0.61012E+00 
c  r13          0.46664E-02      19   0.54182E-08   0.14942E-08 0.20055E+00 
c  r23          0.39964E-02      19   0.54506E-08   0.13032E-08 0.20165E+00 
c  epsilon      0.10972E+02      11   0.33396E-08   0.10233E-01 0.17154E+00 
c  TempC        0.25715E+06      16   0.15139E-04   0.84506E-02 0.43436E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61374       0.0052516       0.0015067
v  Velocity[Y]            -0.57373         0.54434       0.0030766      0.00087284
v  Velocity[Z]              1.5652          5.4367          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4367          4.3406          4.3632
v  Pressure                -36.486          360.05          87.677          169.87
v  r11                    0.001058         0.08188        0.013066        0.018282
v  r22                   0.0011083        0.082629        0.013346        0.018642
v  r33                   0.0016319         0.17428        0.027234        0.037199
v  r12                   -0.010662        0.013599     -0.00023364     -0.00030922
v  r13                   -0.045559        0.052797      9.2349e-05       0.0010133
v  r23                   -0.046692        0.051193       2.984e-05      0.00057422
v  epsilon                0.068525          271.17          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9884e-05       0.0099176      0.00092399       0.0017423
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2781         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71347         0.85282


 TIME FOR THE TIME STEP             9832:        0.80020E+02

===============================================================


 INSTANT    0.983300000E-02   TIME STEP NUMBER            9833
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.695439972E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.405733704E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.305176170E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227920093E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.250574923E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81167E-03   0.45934E-02 0.20060E+01 
c  Velocity[X]                                      0.13961E-03 
c  Velocity[Y]                                      0.13092E-03 
c  Velocity[Z]                                      0.43228E-02 
c  Pressure     0.36848E-04     133   0.93800E-02   0.25993E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.52984E-08   0.16568E-08 0.10048E+00 
c  r22          0.10849E-01      12   0.65061E-08   0.18409E-08 0.10239E+00 
c  r33          0.21854E-01      15   0.51390E-08   0.12644E-07 0.12841E+00 
c  r12          0.93830E-03      18   0.50258E-08   0.30529E-09 0.61104E+00 
c  r13          0.46664E-02      18   0.69850E-08   0.14913E-08 0.19992E+00 
c  r23          0.39964E-02      19   0.63821E-08   0.12898E-08 0.19979E+00 
c  epsilon      0.10972E+02      11   0.33827E-08   0.96706E-02 0.16349E+00 
c  TempC        0.25715E+06      16   0.15132E-04   0.84516E-02 0.43398E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61369       0.0052516       0.0015066
v  Velocity[Y]             -0.5737          0.5445       0.0030765       0.0008728
v  Velocity[Z]              1.5653          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4367          4.3406          4.3632
v  Pressure                 -36.43           360.1          87.708          169.92
v  r11                    0.001058        0.081886        0.013066        0.018282
v  r22                   0.0011083        0.082629        0.013346        0.018642
v  r33                   0.0016319         0.17426        0.027234        0.037199
v  r12                    -0.01066        0.013606     -0.00023364     -0.00030922
v  r13                   -0.045558        0.052798      9.2351e-05       0.0010133
v  r23                   -0.046693        0.051192       2.984e-05      0.00057422
v  epsilon                0.068526          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9881e-05       0.0099176      0.00092399       0.0017423
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2775         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71347         0.85282


 TIME FOR THE TIME STEP             9833:        0.79851E+02

===============================================================


 INSTANT    0.983400000E-02   TIME STEP NUMBER            9834
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.196939352E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.156588255E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.255115875E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229993504E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.107977521E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81162E-03   0.45888E-02 0.20082E+01 
c  Velocity[X]                                      0.14031E-03 
c  Velocity[Y]                                      0.13072E-03 
c  Velocity[Z]                                      0.43177E-02 
c  Pressure     0.36576E-04     132   0.93139E-02   0.25800E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.52110E-08   0.16272E-08 0.99816E-01 
c  r22          0.10849E-01      13   0.47231E-08   0.18159E-08 0.10179E+00 
c  r33          0.21854E-01      15   0.66966E-08   0.12433E-07 0.12729E+00 
c  r12          0.93830E-03      18   0.50798E-08   0.30203E-09 0.61096E+00 
c  r13          0.46664E-02      19   0.59114E-08   0.14869E-08 0.20003E+00 
c  r23          0.39964E-02      19   0.59641E-08   0.12700E-08 0.19858E+00 
c  epsilon      0.10972E+02      11   0.35070E-08   0.97610E-02 0.16363E+00 
c  TempC        0.25715E+06      16   0.15116E-04   0.84897E-02 0.43423E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61373       0.0052516       0.0015067
v  Velocity[Y]            -0.57378         0.54413       0.0030765      0.00087281
v  Velocity[Z]              1.5653          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4367          4.3406          4.3632
v  Pressure                -36.476             360          87.648          169.84
v  r11                    0.001058        0.081887        0.013066        0.018282
v  r22                   0.0011083         0.08263        0.013346        0.018642
v  r33                   0.0016319         0.17428        0.027234        0.037199
v  r12                   -0.010665        0.013606     -0.00023364     -0.00030923
v  r13                   -0.045557        0.052802      9.2353e-05       0.0010133
v  r23                   -0.046695        0.051177      2.9842e-05      0.00057422
v  epsilon                0.068526          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9878e-05       0.0099176      0.00092399       0.0017423
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2771         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71347         0.85282


 TIME FOR THE TIME STEP             9834:        0.79498E+02

===============================================================


 INSTANT    0.983500000E-02   TIME STEP NUMBER            9835
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.115805324E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.771548232E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.231321686E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.454489469E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.175604535E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81218E-03   0.45444E-02 0.19964E+01 
c  Velocity[X]                                      0.13873E-03 
c  Velocity[Y]                                      0.12969E-03 
c  Velocity[Z]                                      0.42760E-02 
c  Pressure     0.36515E-04     134   0.92968E-02   0.25758E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.52686E-08   0.16265E-08 0.99511E-01 
c  r22          0.10849E-01      13   0.49458E-08   0.18254E-08 0.10209E+00 
c  r33          0.21854E-01      15   0.63671E-08   0.12421E-07 0.12732E+00 
c  r12          0.93830E-03      18   0.55045E-08   0.29345E-09 0.60371E+00 
c  r13          0.46664E-02      19   0.64364E-08   0.14881E-08 0.19995E+00 
c  r23          0.39964E-02      19   0.58170E-08   0.12708E-08 0.19812E+00 
c  epsilon      0.10972E+02      11   0.34290E-08   0.99010E-02 0.16466E+00 
c  TempC        0.25715E+06      16   0.15091E-04   0.84041E-02 0.43205E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61374       0.0052517       0.0015067
v  Velocity[Y]            -0.57367         0.54415       0.0030766      0.00087286
v  Velocity[Z]              1.5653          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4367          4.3406          4.3632
v  Pressure                -36.455          360.11          87.685          169.91
v  r11                    0.001058        0.081888        0.013066        0.018282
v  r22                   0.0011083        0.082627        0.013346        0.018642
v  r33                    0.001632          0.1743        0.027234        0.037199
v  r12                   -0.010664        0.013604     -0.00023364     -0.00030923
v  r13                   -0.045559        0.052802      9.2356e-05       0.0010133
v  r23                   -0.046696        0.051199      2.9844e-05      0.00057422
v  epsilon                0.068527          271.16          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9876e-05       0.0099176        0.000924       0.0017423
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017895           5.278         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71347         0.85282


 TIME FOR THE TIME STEP             9835:        0.78168E+02

===============================================================


 INSTANT    0.983600000E-02   TIME STEP NUMBER            9836
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.137088364E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.243850709E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934903E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160637335E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.211867358E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.109538642E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81201E-03   0.45707E-02 0.20026E+01 
c  Velocity[X]                                      0.14028E-03 
c  Velocity[Y]                                      0.13062E-03 
c  Velocity[Z]                                      0.42998E-02 
c  Pressure     0.36640E-04     131   0.93300E-02   0.25846E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.48517E-08   0.16298E-08 0.99943E-01 
c  r22          0.10849E-01      13   0.47296E-08   0.18049E-08 0.10183E+00 
c  r33          0.21854E-01      15   0.54427E-08   0.12423E-07 0.12761E+00 
c  r12          0.93830E-03      18   0.52592E-08   0.29914E-09 0.61074E+00 
c  r13          0.46664E-02      19   0.64431E-08   0.14833E-08 0.20004E+00 
c  r23          0.39964E-02      19   0.58704E-08   0.12919E-08 0.19981E+00 
c  epsilon      0.10972E+02      11   0.34929E-08   0.96833E-02 0.16452E+00 
c  TempC        0.25715E+06      16   0.15143E-04   0.84494E-02 0.43442E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61371       0.0052516       0.0015067
v  Velocity[Y]            -0.57354         0.54434       0.0030766      0.00087284
v  Velocity[Z]              1.5655          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4367          4.3406          4.3632
v  Pressure                -36.458          360.01          87.678          169.85
v  r11                   0.0010581        0.081886        0.013066        0.018282
v  r22                   0.0011083        0.082628        0.013346        0.018642
v  r33                    0.001632         0.17428        0.027234        0.037199
v  r12                   -0.010661        0.013605     -0.00023364     -0.00030923
v  r13                   -0.045557        0.052802      9.2359e-05       0.0010133
v  r23                   -0.046696        0.051186      2.9845e-05      0.00057422
v  epsilon                0.068528          271.15          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9873e-05       0.0099176        0.000924       0.0017423
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2783         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71347         0.85282


 TIME FOR THE TIME STEP             9836:        0.79787E+02

===============================================================


 INSTANT    0.983700000E-02   TIME STEP NUMBER            9837
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.882105804E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.387656622E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.347209111E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935014E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.682311805E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.363968276E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81207E-03   0.45522E-02 0.19985E+01 
c  Velocity[X]                                      0.14009E-03 
c  Velocity[Y]                                      0.13007E-03 
c  Velocity[Z]                                      0.42821E-02 
c  Pressure     0.36499E-04     131   0.92906E-02   0.25747E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.49980E-08   0.16544E-08 0.10069E+00 
c  r22          0.10849E-01      13   0.50960E-08   0.18061E-08 0.10155E+00 
c  r33          0.21854E-01      15   0.59188E-08   0.12458E-07 0.12771E+00 
c  r12          0.93830E-03      18   0.61275E-08   0.29972E-09 0.61359E+00 
c  r13          0.46664E-02      19   0.65456E-08   0.14751E-08 0.19941E+00 
c  r23          0.39964E-02      19   0.51398E-08   0.12913E-08 0.20039E+00 
c  epsilon      0.10972E+02      11   0.34742E-08   0.96134E-02 0.16349E+00 
c  TempC        0.25715E+06      16   0.15104E-04   0.84344E-02 0.43365E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364         0.61374       0.0052517       0.0015067
v  Velocity[Y]            -0.57369         0.54448       0.0030766      0.00087287
v  Velocity[Z]              1.5655          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4367          4.3406          4.3632
v  Pressure                -36.425          360.09          87.682           169.9
v  r11                   0.0010581        0.081883        0.013066        0.018282
v  r22                   0.0011083        0.082629        0.013346        0.018642
v  r33                    0.001632         0.17425        0.027234        0.037199
v  r12                    -0.01066        0.013603     -0.00023365     -0.00030923
v  r13                   -0.045558          0.0528       9.236e-05       0.0010133
v  r23                   -0.046697        0.051179      2.9845e-05      0.00057422
v  epsilon                0.068528          271.11          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.987e-05       0.0099178        0.000924       0.0017423
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2787         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71347         0.85282


 TIME FOR THE TIME STEP             9837:        0.79881E+02

===============================================================


 INSTANT    0.983800000E-02   TIME STEP NUMBER            9838
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.650107936E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.299836699E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.391163610E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237650857E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.217465177E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81103E-03   0.45494E-02 0.19963E+01 
c  Velocity[X]                                      0.13920E-03 
c  Velocity[Y]                                      0.12989E-03 
c  Velocity[Z]                                      0.42803E-02 
c  Pressure     0.36799E-04     133   0.93701E-02   0.25958E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.56099E-08   0.16801E-08 0.10120E+00 
c  r22          0.10849E-01      13   0.53144E-08   0.18449E-08 0.10214E+00 
c  r33          0.21854E-01      15   0.68783E-08   0.12790E-07 0.12885E+00 
c  r12          0.93830E-03      18   0.67440E-08   0.30729E-09 0.61206E+00 
c  r13          0.46664E-02      19   0.74742E-08   0.15173E-08 0.20143E+00 
c  r23          0.39964E-02      19   0.56708E-08   0.13027E-08 0.20172E+00 
c  epsilon      0.10972E+02      11   0.33359E-08   0.10317E-01 0.17222E+00 
c  TempC        0.25715E+06      16   0.15124E-04   0.84265E-02 0.43292E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61372       0.0052517       0.0015068
v  Velocity[Y]            -0.57378         0.54427       0.0030766      0.00087283
v  Velocity[Z]              1.5655          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4367          4.3406          4.3632
v  Pressure                -36.452          360.06          87.683          169.88
v  r11                   0.0010581        0.081888        0.013066        0.018282
v  r22                   0.0011083         0.08263        0.013346        0.018642
v  r33                    0.001632         0.17427        0.027234        0.037199
v  r12                   -0.010667        0.013602     -0.00023365     -0.00030923
v  r13                    -0.04556        0.052802      9.2362e-05       0.0010133
v  r23                   -0.046697        0.051196      2.9846e-05      0.00057422
v  epsilon                0.068529          271.12          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.987e-05       0.0099178        0.000924       0.0017423
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2791         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71347         0.85282


 TIME FOR THE TIME STEP             9838:        0.79053E+02

===============================================================


 INSTANT    0.983900000E-02   TIME STEP NUMBER            9839
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.325582400E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.259238296E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.303095713E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.304142939E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.671515248E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81257E-03   0.45486E-02 0.19981E+01 
c  Velocity[X]                                      0.13932E-03 
c  Velocity[Y]                                      0.13027E-03 
c  Velocity[Z]                                      0.42791E-02 
c  Pressure     0.36598E-04     132   0.93145E-02   0.25816E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.51294E-08   0.16613E-08 0.10083E+00 
c  r22          0.10849E-01      13   0.53287E-08   0.18364E-08 0.10176E+00 
c  r33          0.21854E-01      15   0.73325E-08   0.12616E-07 0.12789E+00 
c  r12          0.93831E-03      18   0.56903E-08   0.30102E-09 0.61214E+00 
c  r13          0.46664E-02      19   0.70240E-08   0.15047E-08 0.20078E+00 
c  r23          0.39964E-02      19   0.59749E-08   0.12936E-08 0.20066E+00 
c  epsilon      0.10972E+02      11   0.34390E-08   0.99838E-02 0.16566E+00 
c  TempC        0.25715E+06      16   0.15114E-04   0.85517E-02 0.43595E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375          0.6137       0.0052516       0.0015067
v  Velocity[Y]            -0.57385         0.54438       0.0030766      0.00087288
v  Velocity[Z]              1.5655          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4367          4.3406          4.3632
v  Pressure                -36.407          360.05          87.678          169.88
v  r11                   0.0010581        0.081887        0.013066        0.018282
v  r22                   0.0011084        0.082632        0.013346        0.018642
v  r33                    0.001632          0.1743        0.027234        0.037199
v  r12                   -0.010666        0.013604     -0.00023365     -0.00030923
v  r13                   -0.045558        0.052801      9.2364e-05       0.0010133
v  r23                   -0.046698        0.051186      2.9846e-05      0.00057422
v  epsilon                0.068529          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9869e-05       0.0099182        0.000924       0.0017423
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2791         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71347         0.85283


 TIME FOR THE TIME STEP             9839:        0.79305E+02

===============================================================


 INSTANT    0.984000000E-02   TIME STEP NUMBER            9840
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.330807448E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.799264815E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.337066011E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.462418052E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.189436402E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81159E-03   0.45660E-02 0.20016E+01 
c  Velocity[X]                                      0.14073E-03 
c  Velocity[Y]                                      0.13075E-03 
c  Velocity[Z]                                      0.42945E-02 
c  Pressure     0.36550E-04     132   0.93070E-02   0.25782E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.54275E-08   0.16655E-08 0.10038E+00 
c  r22          0.10849E-01      13   0.51670E-08   0.18773E-08 0.10251E+00 
c  r33          0.21854E-01      16   0.59906E-08   0.12835E-07 0.12830E+00 
c  r12          0.93831E-03      18   0.57187E-08   0.30262E-09 0.60984E+00 
c  r13          0.46664E-02      20   0.69234E-08   0.15372E-08 0.20191E+00 
c  r23          0.39964E-02      19   0.55699E-08   0.13059E-08 0.20122E+00 
c  epsilon      0.10972E+02      11   0.35643E-08   0.10272E-01 0.16723E+00 
c  TempC        0.25715E+06      16   0.15119E-04   0.84679E-02 0.43441E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61373       0.0052516       0.0015067
v  Velocity[Y]            -0.57386         0.54454       0.0030766       0.0008729
v  Velocity[Z]              1.5656          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4367          4.3406          4.3632
v  Pressure                -36.432          360.06          87.675          169.88
v  r11                   0.0010581        0.081888        0.013066        0.018282
v  r22                   0.0011084        0.082632        0.013346        0.018642
v  r33                   0.0016321          0.1743        0.027234        0.037199
v  r12                   -0.010666        0.013608     -0.00023365     -0.00030923
v  r13                   -0.045556        0.052802      9.2366e-05       0.0010133
v  r23                   -0.046698        0.051164      2.9848e-05      0.00057422
v  epsilon                 0.06853          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9868e-05       0.0099181        0.000924       0.0017423
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2788         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71347         0.85282


 TIME FOR THE TIME STEP             9840:        0.79571E+02

===============================================================


 INSTANT    0.984100000E-02   TIME STEP NUMBER            9841
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.437685593E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283008082E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.194562470E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105576823E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108644764E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81226E-03   0.45701E-02 0.20026E+01 
c  Velocity[X]                                      0.13994E-03 
c  Velocity[Y]                                      0.13015E-03 
c  Velocity[Z]                                      0.43000E-02 
c  Pressure     0.36474E-04     131   0.92794E-02   0.25728E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.53866E-08   0.16291E-08 0.99926E-01 
c  r22          0.10849E-01      13   0.49413E-08   0.18124E-08 0.10164E+00 
c  r33          0.21854E-01      15   0.52510E-08   0.12443E-07 0.12756E+00 
c  r12          0.93831E-03      18   0.54236E-08   0.29880E-09 0.60788E+00 
c  r13          0.46664E-02      19   0.61155E-08   0.15004E-08 0.20069E+00 
c  r23          0.39964E-02      19   0.57222E-08   0.12872E-08 0.19963E+00 
c  epsilon      0.10972E+02      11   0.32735E-08   0.96174E-02 0.16360E+00 
c  TempC        0.25715E+06      16   0.15116E-04   0.83491E-02 0.43173E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61375       0.0052517       0.0015067
v  Velocity[Y]            -0.57383         0.54424       0.0030767      0.00087289
v  Velocity[Z]              1.5658          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4367          4.3406          4.3632
v  Pressure                -36.419          360.09          87.685           169.9
v  r11                   0.0010581        0.081886        0.013066        0.018283
v  r22                   0.0011084        0.082634        0.013346        0.018642
v  r33                   0.0016321         0.17426        0.027235        0.037199
v  r12                   -0.010664        0.013601     -0.00023365     -0.00030923
v  r13                   -0.045561        0.052802      9.2368e-05       0.0010133
v  r23                   -0.046699        0.051183      2.9849e-05      0.00057422
v  epsilon                0.068531           271.1          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9866e-05        0.009918        0.000924       0.0017423
v  CourantNb               0.44216             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2786         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71347         0.85281


 TIME FOR THE TIME STEP             9841:        0.78684E+02

===============================================================


 INSTANT    0.984200000E-02   TIME STEP NUMBER            9842
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.472692840E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108925958E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.901414913E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.989478739E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.556852199E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81112E-03   0.45733E-02 0.20032E+01 
c  Velocity[X]                                      0.14061E-03 
c  Velocity[Y]                                      0.13043E-03 
c  Velocity[Z]                                      0.43023E-02 
c  Pressure     0.36774E-04     132   0.93648E-02   0.25941E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.51157E-08   0.16383E-08 0.10016E+00 
c  r22          0.10849E-01      13   0.52138E-08   0.18323E-08 0.10223E+00 
c  r33          0.21854E-01      15   0.57727E-08   0.12490E-07 0.12797E+00 
c  r12          0.93831E-03      18   0.60231E-08   0.29633E-09 0.60700E+00 
c  r13          0.46664E-02      19   0.60154E-08   0.14729E-08 0.20020E+00 
c  r23          0.39964E-02      19   0.63745E-08   0.12709E-08 0.19977E+00 
c  epsilon      0.10972E+02      11   0.34352E-08   0.96234E-02 0.16418E+00 
c  TempC        0.25715E+06      16   0.15134E-04   0.84395E-02 0.43347E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61372       0.0052517       0.0015067
v  Velocity[Y]            -0.57374         0.54426       0.0030766      0.00087289
v  Velocity[Z]              1.5658          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4367          4.3406          4.3632
v  Pressure                -36.437          360.05           87.69          169.89
v  r11                   0.0010582        0.081884        0.013066        0.018283
v  r22                   0.0011084         0.08263        0.013346        0.018643
v  r33                   0.0016321         0.17428        0.027235        0.037199
v  r12                   -0.010665        0.013601     -0.00023365     -0.00030923
v  r13                   -0.045558        0.052804      9.2371e-05       0.0010133
v  r23                     -0.0467        0.051169      2.9849e-05      0.00057422
v  epsilon                0.068531           271.1          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9866e-05       0.0099181      0.00092401       0.0017423
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2786         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71347         0.85282


 TIME FOR THE TIME STEP             9842:        0.78511E+02

===============================================================


 INSTANT    0.984300000E-02   TIME STEP NUMBER            9843
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.440574747E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.258152252E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.965797603E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.375750331E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.265182768E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81178E-03   0.45651E-02 0.20011E+01 
c  Velocity[X]                                      0.14084E-03 
c  Velocity[Y]                                      0.13069E-03 
c  Velocity[Z]                                      0.42936E-02 
c  Pressure     0.36258E-04     132   0.92256E-02   0.25576E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.50756E-08   0.16602E-08 0.10042E+00 
c  r22          0.10849E-01      13   0.49951E-08   0.18491E-08 0.10192E+00 
c  r33          0.21854E-01      15   0.61214E-08   0.12585E-07 0.12776E+00 
c  r12          0.93831E-03      18   0.66553E-08   0.29648E-09 0.60507E+00 
c  r13          0.46664E-02      19   0.71822E-08   0.14875E-08 0.19994E+00 
c  r23          0.39964E-02      20   0.59830E-08   0.12671E-08 0.19880E+00 
c  epsilon      0.10972E+02      11   0.34408E-08   0.99411E-02 0.16580E+00 
c  TempC        0.25715E+06      16   0.15101E-04   0.85199E-02 0.43523E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61373       0.0052517       0.0015067
v  Velocity[Y]            -0.57382         0.54439       0.0030766      0.00087292
v  Velocity[Z]              1.5655          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4367          4.3406          4.3632
v  Pressure                -36.406          360.03          87.652          169.86
v  r11                   0.0010582        0.081872        0.013066        0.018283
v  r22                   0.0011084         0.08263        0.013346        0.018643
v  r33                   0.0016321         0.17431        0.027235        0.037199
v  r12                   -0.010662        0.013607     -0.00023365     -0.00030923
v  r13                   -0.045557        0.052803      9.2372e-05       0.0010133
v  r23                     -0.0467        0.051155      2.9851e-05      0.00057422
v  epsilon                0.068532          271.15          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9869e-05        0.009918      0.00092401       0.0017423
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2786         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71347         0.85282


 TIME FOR THE TIME STEP             9843:        0.79870E+02

===============================================================


 INSTANT    0.984400000E-02   TIME STEP NUMBER            9844
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.192495736E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.265848189E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934909E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.299755404E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.487843635E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.207411693E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81205E-03   0.45315E-02 0.19932E+01 
c  Velocity[X]                                      0.13910E-03 
c  Velocity[Y]                                      0.12987E-03 
c  Velocity[Z]                                      0.42625E-02 
c  Pressure     0.36777E-04     132   0.93656E-02   0.25942E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.51669E-08   0.16443E-08 0.10010E+00 
c  r22          0.10849E-01      13   0.53153E-08   0.18224E-08 0.10179E+00 
c  r33          0.21854E-01      15   0.60433E-08   0.12502E-07 0.12739E+00 
c  r12          0.93831E-03      18   0.71211E-08   0.29837E-09 0.60598E+00 
c  r13          0.46664E-02      20   0.62757E-08   0.14825E-08 0.20010E+00 
c  r23          0.39964E-02      20   0.66207E-08   0.12949E-08 0.20001E+00 
c  epsilon      0.10972E+02      11   0.33401E-08   0.98476E-02 0.16478E+00 
c  TempC        0.25715E+06      16   0.15162E-04   0.84410E-02 0.43369E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61371       0.0052517       0.0015067
v  Velocity[Y]            -0.57379         0.54452       0.0030767      0.00087294
v  Velocity[Z]              1.5657          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4367          4.3406          4.3632
v  Pressure                -36.447          360.04          87.665          169.86
v  r11                   0.0010582         0.08186        0.013066        0.018283
v  r22                   0.0011084        0.082632        0.013346        0.018643
v  r33                   0.0016321         0.17429        0.027235        0.037199
v  r12                   -0.010659        0.013611     -0.00023365     -0.00030923
v  r13                    -0.04556        0.052802      9.2374e-05       0.0010133
v  r23                   -0.046701        0.051181      2.9852e-05      0.00057422
v  epsilon                0.068532          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9869e-05       0.0099179      0.00092401       0.0017423
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2786         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71347         0.85282


 TIME FOR THE TIME STEP             9844:        0.78749E+02

===============================================================


 INSTANT    0.984500000E-02   TIME STEP NUMBER            9845
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125182684E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.388380436E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.244104367E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.672507689E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.306304210E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81127E-03   0.45478E-02 0.19981E+01 
c  Velocity[X]                                      0.13895E-03 
c  Velocity[Y]                                      0.13002E-03 
c  Velocity[Z]                                      0.42788E-02 
c  Pressure     0.36773E-04     131   0.93537E-02   0.25940E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.54026E-08   0.16529E-08 0.10024E+00 
c  r22          0.10849E-01      13   0.52461E-08   0.18428E-08 0.10203E+00 
c  r33          0.21854E-01      15   0.73779E-08   0.12700E-07 0.12814E+00 
c  r12          0.93831E-03      19   0.55123E-08   0.30271E-09 0.60830E+00 
c  r13          0.46664E-02      20   0.64989E-08   0.14911E-08 0.19984E+00 
c  r23          0.39964E-02      20   0.64631E-08   0.12995E-08 0.20108E+00 
c  epsilon      0.10972E+02      11   0.36382E-08   0.10324E-01 0.17184E+00 
c  TempC        0.25715E+06      16   0.15107E-04   0.83969E-02 0.43242E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338          0.6137       0.0052518       0.0015067
v  Velocity[Y]             -0.5739         0.54419       0.0030768      0.00087296
v  Velocity[Z]              1.5655          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4367          4.3406          4.3632
v  Pressure                -36.421          360.12          87.712          169.93
v  r11                   0.0010582        0.081856        0.013066        0.018283
v  r22                   0.0011084        0.082633        0.013346        0.018643
v  r33                   0.0016321         0.17426        0.027235        0.037199
v  r12                   -0.010664        0.013607     -0.00023365     -0.00030923
v  r13                   -0.045559          0.0528      9.2377e-05       0.0010133
v  r23                   -0.046702        0.051179      2.9853e-05      0.00057423
v  epsilon                0.068533          271.11          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9871e-05       0.0099179      0.00092401       0.0017423
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017895           5.278         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71347         0.85282


 TIME FOR THE TIME STEP             9845:        0.80325E+02

===============================================================


 INSTANT    0.984600000E-02   TIME STEP NUMBER            9846
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.194562527E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.342635332E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.534027736E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.289816993E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169356092E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81177E-03   0.45828E-02 0.20067E+01 
c  Velocity[X]                                      0.14113E-03 
c  Velocity[Y]                                      0.13069E-03 
c  Velocity[Z]                                      0.43110E-02 
c  Pressure     0.36423E-04     132   0.92816E-02   0.25693E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.55235E-08   0.16282E-08 0.10015E+00 
c  r22          0.10849E-01      13   0.55530E-08   0.18348E-08 0.10204E+00 
c  r33          0.21854E-01      15   0.69553E-08   0.12489E-07 0.12744E+00 
c  r12          0.93831E-03      18   0.71006E-08   0.29421E-09 0.60550E+00 
c  r13          0.46664E-02      19   0.68478E-08   0.15015E-08 0.20018E+00 
c  r23          0.39964E-02      20   0.65147E-08   0.12704E-08 0.19903E+00 
c  epsilon      0.10972E+02      11   0.34801E-08   0.97091E-02 0.16423E+00 
c  TempC        0.25715E+06      16   0.15135E-04   0.84717E-02 0.43423E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61373       0.0052518       0.0015067
v  Velocity[Y]            -0.57379         0.54424       0.0030767      0.00087299
v  Velocity[Z]              1.5657          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4367          4.3406          4.3632
v  Pressure                 -36.46          360.03          87.677          169.87
v  r11                   0.0010582        0.081848        0.013066        0.018283
v  r22                   0.0011085        0.082634        0.013346        0.018643
v  r33                   0.0016322         0.17428        0.027235        0.037199
v  r12                   -0.010671        0.013607     -0.00023365     -0.00030923
v  r13                   -0.045557        0.052801      9.2378e-05       0.0010133
v  r23                   -0.046702        0.051169      2.9854e-05      0.00057423
v  epsilon                0.068534           271.1          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9875e-05       0.0099179      0.00092401       0.0017423
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2771         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71347         0.85282


 TIME FOR THE TIME STEP             9846:        0.77142E+02

===============================================================


 INSTANT    0.984700000E-02   TIME STEP NUMBER            9847
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181185263E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227176054E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.307523009E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.556978969E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249555671E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      40   0.81168E-03   0.45450E-02 0.19969E+01 
c  Velocity[X]                                      0.13931E-03 
c  Velocity[Y]                                      0.13001E-03 
c  Velocity[Z]                                      0.42757E-02 
c  Pressure     0.36487E-04     132   0.92884E-02   0.25737E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.49258E-08   0.16186E-08 0.99964E-01 
c  r22          0.10849E-01      13   0.50605E-08   0.18028E-08 0.10190E+00 
c  r33          0.21854E-01      15   0.70236E-08   0.12265E-07 0.12695E+00 
c  r12          0.93831E-03      18   0.61622E-08   0.29697E-09 0.60898E+00 
c  r13          0.46664E-02      19   0.62648E-08   0.14624E-08 0.19906E+00 
c  r23          0.39964E-02      20   0.60728E-08   0.12462E-08 0.19782E+00 
c  epsilon      0.10972E+02      11   0.34827E-08   0.93496E-02 0.16155E+00 
c  TempC        0.25715E+06      16   0.15080E-04   0.84475E-02 0.43357E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61374       0.0052518       0.0015067
v  Velocity[Y]            -0.57392         0.54434       0.0030768        0.000873
v  Velocity[Z]              1.5657          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4367          4.3406          4.3632
v  Pressure                -36.401          360.05          87.663          169.87
v  r11                   0.0010582        0.081838        0.013066        0.018283
v  r22                   0.0011085        0.082633        0.013347        0.018643
v  r33                   0.0016322          0.1743        0.027235        0.037199
v  r12                   -0.010672        0.013603     -0.00023365     -0.00030923
v  r13                   -0.045559        0.052798      9.2381e-05       0.0010133
v  r23                   -0.046703         0.05116      2.9854e-05      0.00057423
v  epsilon                0.068534          271.15          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9881e-05        0.009918      0.00092401       0.0017423
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2774         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71347         0.85282


 TIME FOR THE TIME STEP             9847:        0.77575E+02

===============================================================


 INSTANT    0.984800000E-02   TIME STEP NUMBER            9848
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.202073642E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.124753479E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.426955420E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.721960132E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.749929424E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81187E-03   0.45493E-02 0.19965E+01 
c  Velocity[X]                                      0.13974E-03 
c  Velocity[Y]                                      0.13005E-03 
c  Velocity[Z]                                      0.42795E-02 
c  Pressure     0.36795E-04     134   0.93700E-02   0.25956E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.48927E-08   0.16652E-08 0.10066E+00 
c  r22          0.10849E-01      13   0.50791E-08   0.18391E-08 0.10228E+00 
c  r33          0.21854E-01      15   0.62375E-08   0.12691E-07 0.12806E+00 
c  r12          0.93831E-03      18   0.66772E-08   0.29989E-09 0.60572E+00 
c  r13          0.46664E-02      19   0.66284E-08   0.15198E-08 0.20145E+00 
c  r23          0.39964E-02      20   0.62823E-08   0.13120E-08 0.20084E+00 
c  epsilon      0.10972E+02      11   0.33913E-08   0.10185E-01 0.16768E+00 
c  TempC        0.25715E+06      16   0.15154E-04   0.84665E-02 0.43451E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364         0.61371       0.0052517       0.0015067
v  Velocity[Y]            -0.57393         0.54449       0.0030767      0.00087297
v  Velocity[Z]              1.5655          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4367          4.3406          4.3632
v  Pressure                -36.464          360.06          87.686          169.89
v  r11                   0.0010582        0.081835        0.013066        0.018283
v  r22                   0.0011085        0.082632        0.013347        0.018643
v  r33                   0.0016322         0.17429        0.027235        0.037199
v  r12                   -0.010671        0.013602     -0.00023365     -0.00030923
v  r13                   -0.045556        0.052798      9.2382e-05       0.0010133
v  r23                   -0.046703        0.051189      2.9855e-05      0.00057423
v  epsilon                0.068535          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9884e-05       0.0099179      0.00092402       0.0017423
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2766         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71347         0.85282


 TIME FOR THE TIME STEP             9848:        0.76349E+02

===============================================================


 INSTANT    0.984900000E-02   TIME STEP NUMBER            9849
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.189520065E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158304527E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.126687193E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150893372E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.353436239E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81219E-03   0.45604E-02 0.20001E+01 
c  Velocity[X]                                      0.14002E-03 
c  Velocity[Y]                                      0.13037E-03 
c  Velocity[Z]                                      0.42900E-02 
c  Pressure     0.36289E-04     131   0.92392E-02   0.25598E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.49524E-08   0.16357E-08 0.10017E+00 
c  r22          0.10849E-01      13   0.50462E-08   0.18187E-08 0.10195E+00 
c  r33          0.21854E-01      15   0.66263E-08   0.12353E-07 0.12716E+00 
c  r12          0.93831E-03      18   0.68829E-08   0.29850E-09 0.60781E+00 
c  r13          0.46664E-02      19   0.65636E-08   0.14801E-08 0.19973E+00 
c  r23          0.39964E-02      19   0.64888E-08   0.12717E-08 0.19869E+00 
c  epsilon      0.10972E+02      11   0.33754E-08   0.96438E-02 0.16360E+00 
c  TempC        0.25715E+06      16   0.15138E-04   0.84527E-02 0.43352E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364         0.61374       0.0052517       0.0015067
v  Velocity[Y]            -0.57398          0.5443       0.0030768      0.00087303
v  Velocity[Z]              1.5656          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4367          4.3406          4.3632
v  Pressure                -36.414          360.08          87.668          169.89
v  r11                   0.0010583        0.081835        0.013066        0.018283
v  r22                   0.0011085        0.082628        0.013347        0.018643
v  r33                   0.0016322         0.17427        0.027235        0.037199
v  r12                    -0.01067        0.013603     -0.00023365     -0.00030923
v  r13                   -0.045557          0.0528      9.2384e-05       0.0010133
v  r23                   -0.046703        0.051189      2.9856e-05      0.00057423
v  epsilon                0.068535          271.11          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9888e-05       0.0099178      0.00092402       0.0017423
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2765         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765         0.71347         0.85282


 TIME FOR THE TIME STEP             9849:        0.76616E+02

===============================================================


 INSTANT    0.985000000E-02   TIME STEP NUMBER            9850
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145563699E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.109194804E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.629288049E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178425755E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.147194493E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81189E-03   0.45508E-02 0.19974E+01 
c  Velocity[X]                                      0.13926E-03 
c  Velocity[Y]                                      0.12984E-03 
c  Velocity[Z]                                      0.42817E-02 
c  Pressure     0.36807E-04     132   0.93732E-02   0.25963E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.47462E-08   0.16453E-08 0.10018E+00 
c  r22          0.10849E-01      13   0.48103E-08   0.18178E-08 0.10199E+00 
c  r33          0.21854E-01      16   0.60481E-08   0.12496E-07 0.12775E+00 
c  r12          0.93831E-03      18   0.60834E-08   0.30051E-09 0.60780E+00 
c  r13          0.46664E-02      20   0.60680E-08   0.14591E-08 0.19887E+00 
c  r23          0.39964E-02      19   0.62589E-08   0.12777E-08 0.19952E+00 
c  epsilon      0.10972E+02      11   0.35491E-08   0.96870E-02 0.16271E+00 
c  TempC        0.25715E+06      16   0.15130E-04   0.84335E-02 0.43319E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61374       0.0052518       0.0015067
v  Velocity[Y]            -0.57385         0.54438       0.0030768      0.00087306
v  Velocity[Z]              1.5655          5.4367          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4367          4.3406          4.3632
v  Pressure                -36.403          360.04          87.674          169.87
v  r11                   0.0010583        0.081834        0.013066        0.018283
v  r22                   0.0011085        0.082628        0.013347        0.018643
v  r33                   0.0016322         0.17427        0.027235        0.037199
v  r12                   -0.010669        0.013599     -0.00023365     -0.00030923
v  r13                    -0.04556        0.052801      9.2387e-05       0.0010133
v  r23                   -0.046703        0.051177      2.9857e-05      0.00057423
v  epsilon                0.068536          271.12          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9891e-05       0.0099177      0.00092402       0.0017423
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2773         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71347         0.85282


 TIME FOR THE TIME STEP             9850:        0.78418E+02

===============================================================


 INSTANT    0.985100000E-02   TIME STEP NUMBER            9851
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.371221400E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.134664618E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.284468884E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.139338047E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.442194574E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81142E-03   0.45575E-02 0.20018E+01 
c  Velocity[X]                                      0.13944E-03 
c  Velocity[Y]                                      0.12963E-03 
c  Velocity[Z]                                      0.42884E-02 
c  Pressure     0.36593E-04     132   0.93195E-02   0.25813E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.49565E-08   0.16640E-08 0.10102E+00 
c  r22          0.10849E-01      13   0.52714E-08   0.18513E-08 0.10260E+00 
c  r33          0.21854E-01      15   0.58320E-08   0.12716E-07 0.12881E+00 
c  r12          0.93831E-03      18   0.60940E-08   0.30619E-09 0.61194E+00 
c  r13          0.46664E-02      19   0.63940E-08   0.15098E-08 0.20094E+00 
c  r23          0.39964E-02      19   0.58973E-08   0.13021E-08 0.20128E+00 
c  epsilon      0.10972E+02      11   0.34285E-08   0.10145E-01 0.16852E+00 
c  TempC        0.25715E+06      16   0.15106E-04   0.84228E-02 0.43324E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379         0.61374       0.0052517       0.0015066
v  Velocity[Y]            -0.57389         0.54449       0.0030769      0.00087307
v  Velocity[Z]              1.5656          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4368          4.3406          4.3632
v  Pressure                -36.382          360.07          87.678          169.88
v  r11                   0.0010583        0.081833        0.013066        0.018283
v  r22                   0.0011085         0.08263        0.013347        0.018643
v  r33                   0.0016322          0.1743        0.027235        0.037199
v  r12                    -0.01067        0.013605     -0.00023365     -0.00030923
v  r13                   -0.045558          0.0528      9.2389e-05       0.0010133
v  r23                   -0.046704         0.05117      2.9857e-05      0.00057423
v  epsilon                0.068536          271.13          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9895e-05       0.0099175      0.00092402       0.0017423
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2778         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71347         0.85282


 TIME FOR THE TIME STEP             9851:        0.78597E+02

===============================================================


 INSTANT    0.985200000E-02   TIME STEP NUMBER            9852
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100799417E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.288668641E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.916711367E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.302520405E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153765712E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81170E-03   0.45641E-02 0.19981E+01 
c  Velocity[X]                                      0.14059E-03 
c  Velocity[Y]                                      0.13000E-03 
c  Velocity[Z]                                      0.42935E-02 
c  Pressure     0.36510E-04     132   0.92892E-02   0.25754E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.52050E-08   0.16371E-08 0.10028E+00 
c  r22          0.10849E-01      13   0.56729E-08   0.18480E-08 0.10216E+00 
c  r33          0.21854E-01      15   0.57136E-08   0.12597E-07 0.12789E+00 
c  r12          0.93831E-03      18   0.64389E-08   0.30101E-09 0.60947E+00 
c  r13          0.46664E-02      19   0.71610E-08   0.15232E-08 0.20124E+00 
c  r23          0.39964E-02      19   0.67739E-08   0.12759E-08 0.19889E+00 
c  epsilon      0.10972E+02      11   0.34820E-08   0.99050E-02 0.16587E+00 
c  TempC        0.25715E+06      16   0.15138E-04   0.84496E-02 0.43380E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63377         0.61376       0.0052518       0.0015067
v  Velocity[Y]            -0.57379         0.54414       0.0030768      0.00087306
v  Velocity[Z]              1.5658          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4368          4.3406          4.3632
v  Pressure                -36.462          360.05          87.672          169.87
v  r11                   0.0010583        0.081836        0.013067        0.018283
v  r22                   0.0011085        0.082631        0.013347        0.018643
v  r33                   0.0016322         0.17429        0.027235        0.037199
v  r12                   -0.010669        0.013606     -0.00023365     -0.00030923
v  r13                   -0.045556        0.052799      9.2391e-05       0.0010133
v  r23                   -0.046704         0.05119      2.9858e-05      0.00057423
v  epsilon                0.068537          271.15          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9899e-05       0.0099174      0.00092402       0.0017423
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2784         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71347         0.85282


 TIME FOR THE TIME STEP             9852:        0.77983E+02

===============================================================


 INSTANT    0.985300000E-02   TIME STEP NUMBER            9853
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.243739521E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.107821139E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.336349452E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190632188E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.381890943E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81217E-03   0.45370E-02 0.19938E+01 
c  Velocity[X]                                      0.13873E-03 
c  Velocity[Y]                                      0.12990E-03 
c  Velocity[Z]                                      0.42684E-02 
c  Pressure     0.36464E-04     133   0.92826E-02   0.25721E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.52497E-08   0.16308E-08 0.10001E+00 
c  r22          0.10849E-01      13   0.56907E-08   0.18152E-08 0.10149E+00 
c  r33          0.21854E-01      15   0.54695E-08   0.12437E-07 0.12711E+00 
c  r12          0.93831E-03      18   0.57604E-08   0.29433E-09 0.60386E+00 
c  r13          0.46664E-02      19   0.58416E-08   0.14821E-08 0.19953E+00 
c  r23          0.39964E-02      19   0.56007E-08   0.12648E-08 0.19783E+00 
c  epsilon      0.10972E+02      11   0.33759E-08   0.98030E-02 0.16453E+00 
c  TempC        0.25715E+06      16   0.15103E-04   0.84492E-02 0.43386E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63377         0.61375       0.0052518       0.0015067
v  Velocity[Y]            -0.57393         0.54412       0.0030769      0.00087308
v  Velocity[Z]              1.5657          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4368          4.3406          4.3632
v  Pressure                -36.444          360.02          87.638          169.85
v  r11                   0.0010583        0.081845        0.013067        0.018283
v  r22                   0.0011085         0.08263        0.013347        0.018643
v  r33                   0.0016322         0.17425        0.027235        0.037199
v  r12                    -0.01067        0.013609     -0.00023365     -0.00030923
v  r13                    -0.04556        0.052798      9.2393e-05       0.0010133
v  r23                   -0.046704        0.051191      2.9859e-05      0.00057423
v  epsilon                0.068537          271.12          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9902e-05       0.0099175      0.00092402       0.0017423
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2786         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71347         0.85283


 TIME FOR THE TIME STEP             9853:        0.77481E+02

===============================================================


 INSTANT    0.985400000E-02   TIME STEP NUMBER            9854
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276661454E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.259132277E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.131666977E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.104056792E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190447128E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81155E-03   0.45615E-02 0.19988E+01 
c  Velocity[X]                                      0.13881E-03 
c  Velocity[Y]                                      0.12992E-03 
c  Velocity[Z]                                      0.42928E-02 
c  Pressure     0.36460E-04     133   0.92861E-02   0.25718E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.51742E-08   0.16636E-08 0.10049E+00 
c  r22          0.10849E-01      13   0.55210E-08   0.18364E-08 0.10203E+00 
c  r33          0.21854E-01      15   0.53846E-08   0.12616E-07 0.12800E+00 
c  r12          0.93831E-03      18   0.58273E-08   0.29808E-09 0.60836E+00 
c  r13          0.46664E-02      19   0.62673E-08   0.14948E-08 0.20029E+00 
c  r23          0.39964E-02      19   0.57838E-08   0.12954E-08 0.20052E+00 
c  epsilon      0.10972E+02      11   0.34427E-08   0.99497E-02 0.16690E+00 
c  TempC        0.25715E+06      16   0.15138E-04   0.84835E-02 0.43407E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61372       0.0052518       0.0015067
v  Velocity[Y]            -0.57374         0.54425       0.0030769      0.00087311
v  Velocity[Z]              1.5656          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4368          4.3406          4.3632
v  Pressure                 -36.42          360.02          87.653          169.85
v  r11                   0.0010583        0.081849        0.013067        0.018283
v  r22                   0.0011085        0.082631        0.013347        0.018643
v  r33                   0.0016323         0.17427        0.027235        0.037199
v  r12                   -0.010676        0.013606     -0.00023365     -0.00030923
v  r13                   -0.045557          0.0528      9.2395e-05       0.0010133
v  r23                   -0.046704        0.051175      2.9861e-05      0.00057423
v  epsilon                0.068538          271.13          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9905e-05       0.0099174      0.00092402       0.0017423
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2785         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71347         0.85282


 TIME FOR THE TIME STEP             9854:        0.79302E+02

===============================================================


 INSTANT    0.985500000E-02   TIME STEP NUMBER            9855
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.816560614E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100374169E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184999312E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.194097741E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.100265449E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81100E-03   0.45686E-02 0.20040E+01 
c  Velocity[X]                                      0.14129E-03 
c  Velocity[Y]                                      0.12989E-03 
c  Velocity[Z]                                      0.42975E-02 
c  Pressure     0.36919E-04     133   0.93993E-02   0.26042E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.51077E-08   0.16368E-08 0.10043E+00 
c  r22          0.10849E-01      13   0.54489E-08   0.18052E-08 0.10180E+00 
c  r33          0.21854E-01      15   0.56453E-08   0.12339E-07 0.12751E+00 
c  r12          0.93832E-03      18   0.54079E-08   0.29908E-09 0.60665E+00 
c  r13          0.46664E-02      19   0.59275E-08   0.14744E-08 0.19976E+00 
c  r23          0.39964E-02      19   0.65232E-08   0.12689E-08 0.19912E+00 
c  epsilon      0.10972E+02      11   0.33017E-08   0.95041E-02 0.16335E+00 
c  TempC        0.25715E+06      16   0.15077E-04   0.85134E-02 0.43522E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63359         0.61373       0.0052518       0.0015066
v  Velocity[Y]            -0.57386          0.5444       0.0030769      0.00087311
v  Velocity[Z]              1.5655          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4368          4.3406          4.3632
v  Pressure                -36.367          360.07           87.67          169.88
v  r11                   0.0010583         0.08185        0.013067        0.018283
v  r22                   0.0011086        0.082631        0.013347        0.018643
v  r33                   0.0016323         0.17431        0.027235        0.037199
v  r12                   -0.010676        0.013607     -0.00023365     -0.00030923
v  r13                   -0.045557          0.0528      9.2396e-05       0.0010133
v  r23                   -0.046704          0.0512      2.9862e-05      0.00057423
v  epsilon                0.068538          271.15          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9904e-05       0.0099175      0.00092403       0.0017423
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2781         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71347         0.85282


 TIME FOR THE TIME STEP             9855:        0.78793E+02

===============================================================


 INSTANT    0.985600000E-02   TIME STEP NUMBER            9856
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.348677317E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.257007282E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.164017375E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.196736840E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.430838941E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81282E-03   0.45119E-02 0.19911E+01 
c  Velocity[X]                                      0.13966E-03 
c  Velocity[Y]                                      0.13057E-03 
c  Velocity[Z]                                      0.42416E-02 
c  Pressure     0.36065E-04     133   0.91848E-02   0.25441E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.51730E-08   0.16802E-08 0.10110E+00 
c  r22          0.10849E-01      13   0.49987E-08   0.18463E-08 0.10234E+00 
c  r33          0.21854E-01      15   0.55723E-08   0.12797E-07 0.12889E+00 
c  r12          0.93832E-03      18   0.53312E-08   0.30317E-09 0.60784E+00 
c  r13          0.46664E-02      19   0.59581E-08   0.15011E-08 0.20101E+00 
c  r23          0.39964E-02      19   0.67934E-08   0.13211E-08 0.20264E+00 
c  epsilon      0.10972E+02      11   0.33367E-08   0.10335E-01 0.17154E+00 
c  TempC        0.25715E+06      16   0.15146E-04   0.83919E-02 0.43296E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63365         0.61371       0.0052518       0.0015067
v  Velocity[Y]             -0.5739          0.5445        0.003077      0.00087318
v  Velocity[Z]              1.5657          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4368          4.3406          4.3632
v  Pressure                -36.423          360.04          87.669          169.87
v  r11                   0.0010584        0.081855        0.013067        0.018283
v  r22                   0.0011086         0.08263        0.013347        0.018643
v  r33                   0.0016323         0.17428        0.027235        0.037199
v  r12                   -0.010676        0.013611     -0.00023365     -0.00030923
v  r13                    -0.04556        0.052799      9.2398e-05       0.0010133
v  r23                   -0.046703        0.051188      2.9862e-05      0.00057423
v  epsilon                0.068539          271.16          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9902e-05       0.0099174      0.00092403       0.0017423
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2776         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71347         0.85282


 TIME FOR THE TIME STEP             9856:        0.80181E+02

===============================================================


 INSTANT    0.985700000E-02   TIME STEP NUMBER            9857
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.240395942E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145555244E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.238509835E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.640404016E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.625286071E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      39   0.81154E-03   0.45615E-02 0.19990E+01 
c  Velocity[X]                                      0.13924E-03 
c  Velocity[Y]                                      0.13042E-03 
c  Velocity[Z]                                      0.42919E-02 
c  Pressure     0.36454E-04     133   0.92778E-02   0.25715E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.53602E-08   0.16419E-08 0.10023E+00 
c  r22          0.10849E-01      13   0.47552E-08   0.18119E-08 0.10197E+00 
c  r33          0.21854E-01      15   0.65403E-08   0.12381E-07 0.12755E+00 
c  r12          0.93832E-03      17   0.70258E-08   0.30165E-09 0.60635E+00 
c  r13          0.46664E-02      19   0.64765E-08   0.14725E-08 0.19960E+00 
c  r23          0.39965E-02      19   0.63963E-08   0.12731E-08 0.19888E+00 
c  epsilon      0.10972E+02      11   0.34213E-08   0.94779E-02 0.16240E+00 
c  TempC        0.25715E+06      16   0.15128E-04   0.83795E-02 0.43262E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63372          0.6137       0.0052518       0.0015067
v  Velocity[Y]            -0.57379          0.5443        0.003077      0.00087317
v  Velocity[Z]              1.5658          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4368          4.3406          4.3632
v  Pressure                -36.418          360.03          87.645          169.85
v  r11                   0.0010584        0.081858        0.013067        0.018283
v  r22                   0.0011086         0.08263        0.013347        0.018643
v  r33                   0.0016323         0.17426        0.027235        0.037199
v  r12                   -0.010671        0.013607     -0.00023366     -0.00030923
v  r13                   -0.045559        0.052798        9.24e-05       0.0010133
v  r23                   -0.046703        0.051173      2.9863e-05      0.00057423
v  epsilon                0.068539          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9899e-05       0.0099174      0.00092403       0.0017423
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2774         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71347         0.85282


 TIME FOR THE TIME STEP             9857:        0.81579E+02

===============================================================


 INSTANT    0.985800000E-02   TIME STEP NUMBER            9858
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.386877321E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242184317E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173124804E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.225624360E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.209729618E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81137E-03   0.45761E-02 0.20018E+01 
c  Velocity[X]                                      0.14002E-03 
c  Velocity[Y]                                      0.13063E-03 
c  Velocity[Z]                                      0.43055E-02 
c  Pressure     0.36745E-04     134   0.93640E-02   0.25920E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.53861E-08   0.16664E-08 0.10116E+00 
c  r22          0.10849E-01      13   0.51602E-08   0.18332E-08 0.10240E+00 
c  r33          0.21854E-01      15   0.60784E-08   0.12622E-07 0.12876E+00 
c  r12          0.93832E-03      18   0.58804E-08   0.30814E-09 0.61258E+00 
c  r13          0.46664E-02      19   0.68783E-08   0.14999E-08 0.20149E+00 
c  r23          0.39965E-02      19   0.62185E-08   0.12950E-08 0.20120E+00 
c  epsilon      0.10972E+02      11   0.33478E-08   0.97852E-02 0.16471E+00 
c  TempC        0.25715E+06      16   0.15111E-04   0.85000E-02 0.43463E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63377         0.61372       0.0052519       0.0015067
v  Velocity[Y]            -0.57376         0.54427        0.003077      0.00087315
v  Velocity[Z]              1.5658          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4368          4.3406          4.3632
v  Pressure                 -36.41          360.06          87.683          169.88
v  r11                   0.0010584        0.081854        0.013067        0.018283
v  r22                   0.0011086         0.08263        0.013347        0.018643
v  r33                   0.0016323         0.17428        0.027235        0.037199
v  r12                   -0.010675        0.013613     -0.00023366     -0.00030923
v  r13                   -0.045556        0.052798      9.2402e-05       0.0010133
v  r23                   -0.046702        0.051161      2.9864e-05      0.00057423
v  epsilon                 0.06854          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9897e-05       0.0099174      0.00092403       0.0017423
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2775         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71347         0.85282


 TIME FOR THE TIME STEP             9858:        0.81500E+02

===============================================================


 INSTANT    0.985900000E-02   TIME STEP NUMBER            9859
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.235207077E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239680582E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.871758756E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.259562583E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.190105199E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81210E-03   0.45551E-02 0.19982E+01 
c  Velocity[X]                                      0.13958E-03 
c  Velocity[Y]                                      0.13030E-03 
c  Velocity[Z]                                      0.42852E-02 
c  Pressure     0.36676E-04     132   0.93391E-02   0.25870E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.55199E-08   0.16689E-08 0.10111E+00 
c  r22          0.10849E-01      13   0.50684E-08   0.18546E-08 0.10281E+00 
c  r33          0.21854E-01      15   0.74802E-08   0.12663E-07 0.12853E+00 
c  r12          0.93832E-03      18   0.69227E-08   0.29825E-09 0.60752E+00 
c  r13          0.46664E-02      21   0.62788E-08   0.15084E-08 0.20181E+00 
c  r23          0.39965E-02      20   0.58941E-08   0.12904E-08 0.20061E+00 
c  epsilon      0.10972E+02      11   0.34965E-08   0.98798E-02 0.16540E+00 
c  TempC        0.25715E+06      16   0.15106E-04   0.84260E-02 0.43287E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375          0.6137       0.0052519       0.0015067
v  Velocity[Y]             -0.5737         0.54433        0.003077      0.00087317
v  Velocity[Z]               1.566          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5797          5.4368          4.3406          4.3632
v  Pressure                -36.349          360.03          87.625          169.84
v  r11                   0.0010584        0.081854        0.013067        0.018283
v  r22                   0.0011086        0.082626        0.013347        0.018643
v  r33                   0.0016323          0.1743        0.027235        0.037199
v  r12                   -0.010673        0.013611     -0.00023366     -0.00030923
v  r13                   -0.045559        0.052799      9.2404e-05       0.0010133
v  r23                   -0.046702        0.051191      2.9865e-05      0.00057423
v  epsilon                 0.06854          271.17          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9894e-05       0.0099174      0.00092403       0.0017423
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2777         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71347         0.85282


 TIME FOR THE TIME STEP             9859:        0.81515E+02

===============================================================


 INSTANT    0.986000000E-02   TIME STEP NUMBER            9860
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.321925225E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.410630287E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934895E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.256109050E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.381856570E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130927027E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81141E-03   0.45609E-02 0.19999E+01 
c  Velocity[X]                                      0.14028E-03 
c  Velocity[Y]                                      0.12993E-03 
c  Velocity[Z]                                      0.42907E-02 
c  Pressure     0.36604E-04     132   0.93151E-02   0.25820E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.60220E-08   0.16443E-08 0.10015E+00 
c  r22          0.10849E-01      13   0.54588E-08   0.18635E-08 0.10296E+00 
c  r33          0.21854E-01      15   0.71998E-08   0.12659E-07 0.12845E+00 
c  r12          0.93832E-03      19   0.60632E-08   0.29855E-09 0.60613E+00 
c  r13          0.46664E-02      20   0.70407E-08   0.15133E-08 0.20193E+00 
c  r23          0.39965E-02      19   0.67536E-08   0.12795E-08 0.19873E+00 
c  epsilon      0.10972E+02      11   0.33922E-08   0.10122E-01 0.16776E+00 
c  TempC        0.25715E+06      16   0.15146E-04   0.84547E-02 0.43394E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61368       0.0052519       0.0015067
v  Velocity[Y]            -0.57376         0.54441       0.0030771      0.00087318
v  Velocity[Z]              1.5657          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4368          4.3406          4.3632
v  Pressure                -36.411             360           87.66          169.84
v  r11                   0.0010584        0.081857        0.013067        0.018283
v  r22                   0.0011086        0.082626        0.013347        0.018643
v  r33                   0.0016323         0.17429        0.027235        0.037199
v  r12                    -0.01067        0.013615     -0.00023366     -0.00030923
v  r13                   -0.045557        0.052799      9.2406e-05       0.0010133
v  r23                   -0.046701        0.051191      2.9866e-05      0.00057424
v  epsilon                0.068541          271.17          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9892e-05       0.0099174      0.00092403       0.0017423
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2784         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71347         0.85282


 TIME FOR THE TIME STEP             9860:        0.79331E+02

===============================================================


 INSTANT    0.986100000E-02   TIME STEP NUMBER            9861
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.185021621E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.201882486E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.529757003E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.250613917E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120678977E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81129E-03   0.45640E-02 0.20015E+01 
c  Velocity[X]                                      0.13970E-03 
c  Velocity[Y]                                      0.13065E-03 
c  Velocity[Z]                                      0.42936E-02 
c  Pressure     0.36685E-04     132   0.93444E-02   0.25879E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.63134E-08   0.16617E-08 0.10086E+00 
c  r22          0.10849E-01      13   0.53054E-08   0.18279E-08 0.10239E+00 
c  r33          0.21854E-01      15   0.62424E-08   0.12494E-07 0.12797E+00 
c  r12          0.93832E-03      19   0.60320E-08   0.29504E-09 0.60425E+00 
c  r13          0.46664E-02      20   0.60973E-08   0.14784E-08 0.20045E+00 
c  r23          0.39965E-02      19   0.53938E-08   0.12733E-08 0.19955E+00 
c  epsilon      0.10972E+02      11   0.34217E-08   0.96789E-02 0.16468E+00 
c  TempC        0.25715E+06      16   0.15098E-04   0.84234E-02 0.43331E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373          0.6137       0.0052518       0.0015067
v  Velocity[Y]            -0.57373         0.54452       0.0030771      0.00087323
v  Velocity[Z]              1.5657          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4369          4.3406          4.3632
v  Pressure                -36.385          360.07           87.68          169.89
v  r11                   0.0010584        0.081862        0.013067        0.018283
v  r22                   0.0011086        0.082627        0.013347        0.018643
v  r33                   0.0016324         0.17427        0.027235        0.037199
v  r12                   -0.010667        0.013611     -0.00023366     -0.00030923
v  r13                   -0.045557        0.052798      9.2408e-05       0.0010133
v  r23                   -0.046701         0.05119      2.9867e-05      0.00057424
v  epsilon                0.068541          271.14          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9891e-05       0.0099175      0.00092404       0.0017423
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2779         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71347         0.85282


 TIME FOR THE TIME STEP             9861:        0.81881E+02

===============================================================


 INSTANT    0.986200000E-02   TIME STEP NUMBER            9862
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.311833628E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.314533559E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.247452252E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.234191719E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.329074822E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81236E-03   0.45644E-02 0.20011E+01 
c  Velocity[X]                                      0.13963E-03 
c  Velocity[Y]                                      0.12976E-03 
c  Velocity[Z]                                      0.42950E-02 
c  Pressure     0.36370E-04     132   0.92622E-02   0.25656E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.63149E-08   0.16776E-08 0.10140E+00 
c  r22          0.10849E-01      13   0.55468E-08   0.18253E-08 0.10238E+00 
c  r33          0.21854E-01      15   0.62729E-08   0.12733E-07 0.12905E+00 
c  r12          0.93832E-03      19   0.54900E-08   0.29875E-09 0.60695E+00 
c  r13          0.46664E-02      20   0.58130E-08   0.14961E-08 0.20096E+00 
c  r23          0.39965E-02      19   0.68018E-08   0.13143E-08 0.20228E+00 
c  epsilon      0.10972E+02      11   0.35023E-08   0.10299E-01 0.17401E+00 
c  TempC        0.25715E+06      16   0.15132E-04   0.84107E-02 0.43269E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63371         0.61371       0.0052519       0.0015067
v  Velocity[Y]            -0.57379          0.5443       0.0030771      0.00087318
v  Velocity[Z]              1.5657          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4369          4.3406          4.3632
v  Pressure                -36.408          360.12          87.735          169.94
v  r11                   0.0010584        0.081865        0.013067        0.018283
v  r22                   0.0011086        0.082628        0.013347        0.018643
v  r33                   0.0016324         0.17429        0.027235        0.037199
v  r12                   -0.010674         0.01361     -0.00023366     -0.00030923
v  r13                   -0.045559        0.052798      9.2411e-05       0.0010133
v  r23                   -0.046701        0.051209      2.9868e-05      0.00057424
v  epsilon                0.068542          271.17          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9892e-05       0.0099177      0.00092404       0.0017423
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2782         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71347         0.85282


 TIME FOR THE TIME STEP             9862:        0.80402E+02

===============================================================


 INSTANT    0.986300000E-02   TIME STEP NUMBER            9863
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.805198218E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.241809232E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.681155579E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.297632010E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.197160069E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81129E-03   0.45834E-02 0.20050E+01 
c  Velocity[X]                                      0.13940E-03 
c  Velocity[Y]                                      0.13171E-03 
c  Velocity[Z]                                      0.43123E-02 
c  Pressure     0.36520E-04     133   0.93000E-02   0.25760E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.59676E-08   0.16558E-08 0.10087E+00 
c  r22          0.10849E-01      13   0.55344E-08   0.18463E-08 0.10285E+00 
c  r33          0.21854E-01      15   0.68575E-08   0.12662E-07 0.12847E+00 
c  r12          0.93832E-03      18   0.70472E-08   0.29960E-09 0.60841E+00 
c  r13          0.46664E-02      20   0.58676E-08   0.15087E-08 0.20153E+00 
c  r23          0.39965E-02      19   0.68699E-08   0.12901E-08 0.19998E+00 
c  epsilon      0.10972E+02      11   0.34375E-08   0.10175E-01 0.16654E+00 
c  TempC        0.25715E+06      16   0.15113E-04   0.85197E-02 0.43560E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61368       0.0052519       0.0015067
v  Velocity[Y]            -0.57372         0.54441       0.0030771      0.00087317
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.397          360.07          87.668          169.88
v  r11                   0.0010584        0.081866        0.013067        0.018283
v  r22                   0.0011086        0.082627        0.013347        0.018643
v  r33                   0.0016324         0.17432        0.027235        0.037199
v  r12                   -0.010674        0.013609     -0.00023366     -0.00030923
v  r13                   -0.045556        0.052796      9.2412e-05       0.0010133
v  r23                   -0.046701        0.051201      2.9868e-05      0.00057424
v  epsilon                0.068542          271.19          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.989e-05       0.0099178      0.00092404       0.0017423
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2775         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71347         0.85282


 TIME FOR THE TIME STEP             9863:        0.80639E+02

===============================================================


 INSTANT    0.986400000E-02   TIME STEP NUMBER            9864
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203421646E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.730934215E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934898E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.203096026E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138898591E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160536494E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81180E-03   0.45741E-02 0.20038E+01 
c  Velocity[X]                                      0.14042E-03 
c  Velocity[Y]                                      0.13066E-03 
c  Velocity[Z]                                      0.43030E-02 
c  Pressure     0.36439E-04     132   0.92848E-02   0.25704E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.56272E-08   0.16273E-08 0.10075E+00 
c  r22          0.10849E-01      13   0.51202E-08   0.18165E-08 0.10270E+00 
c  r33          0.21854E-01      15   0.59344E-08   0.12336E-07 0.12838E+00 
c  r12          0.93832E-03      18   0.66030E-08   0.30267E-09 0.61156E+00 
c  r13          0.46664E-02      19   0.67634E-08   0.14824E-08 0.20102E+00 
c  r23          0.39965E-02      19   0.68560E-08   0.12641E-08 0.20039E+00 
c  epsilon      0.10972E+02      11   0.33487E-08   0.93616E-02 0.16156E+00 
c  TempC        0.25715E+06      16   0.15164E-04   0.84512E-02 0.43370E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338         0.61373       0.0052519       0.0015067
v  Velocity[Y]            -0.57379         0.54411       0.0030771      0.00087318
v  Velocity[Z]              1.5658          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4369          4.3406          4.3632
v  Pressure                -36.471          360.06          87.698          169.89
v  r11                   0.0010584        0.081872        0.013067        0.018283
v  r22                   0.0011086        0.082627        0.013347        0.018643
v  r33                   0.0016324         0.17431        0.027235        0.037199
v  r12                   -0.010671        0.013606     -0.00023366     -0.00030923
v  r13                   -0.045555        0.052795      9.2414e-05       0.0010133
v  r23                   -0.046702        0.051179      2.9869e-05      0.00057424
v  epsilon                0.068543          271.19          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9887e-05       0.0099178      0.00092404       0.0017423
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2777         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71347         0.85282


 TIME FOR THE TIME STEP             9864:        0.83614E+02

===============================================================


 INSTANT    0.986500000E-02   TIME STEP NUMBER            9865
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.979094430E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.275364487E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.112830197E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154624930E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.791347518E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81168E-03   0.45149E-02 0.19911E+01 
c  Velocity[X]                                      0.13938E-03 
c  Velocity[Y]                                      0.12952E-03 
c  Velocity[Z]                                      0.42460E-02 
c  Pressure     0.36542E-04     132   0.93007E-02   0.25776E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.57052E-08   0.16365E-08 0.10056E+00 
c  r22          0.10849E-01      13   0.51775E-08   0.17896E-08 0.10137E+00 
c  r33          0.21854E-01      15   0.59795E-08   0.12413E-07 0.12785E+00 
c  r12          0.93832E-03      18   0.71047E-08   0.29206E-09 0.60374E+00 
c  r13          0.46664E-02      19   0.70768E-08   0.14596E-08 0.19901E+00 
c  r23          0.39965E-02      19   0.62386E-08   0.12739E-08 0.19985E+00 
c  epsilon      0.10972E+02      11   0.33840E-08   0.97432E-02 0.16531E+00 
c  TempC        0.25715E+06      16   0.15087E-04   0.83510E-02 0.43110E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373          0.6137       0.0052519       0.0015067
v  Velocity[Y]            -0.57378         0.54414       0.0030771      0.00087317
v  Velocity[Z]              1.5657          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4369          4.3406          4.3632
v  Pressure                -36.376           360.1          87.688          169.91
v  r11                   0.0010585        0.081866        0.013067        0.018283
v  r22                   0.0011087        0.082626        0.013347        0.018643
v  r33                   0.0016324         0.17428        0.027235        0.037199
v  r12                   -0.010669        0.013609     -0.00023366     -0.00030923
v  r13                    -0.04556        0.052795      9.2416e-05       0.0010133
v  r23                   -0.046703        0.051172       2.987e-05      0.00057424
v  epsilon                0.068543          271.17          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9887e-05       0.0099177      0.00092404       0.0017423
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017896           5.278         0.11438         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71347         0.85281


 TIME FOR THE TIME STEP             9865:        0.78376E+02

===============================================================


 INSTANT    0.986600000E-02   TIME STEP NUMBER            9866
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.240468044E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.506425436E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.126334030E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.407439147E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120267371E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81221E-03   0.45922E-02 0.20059E+01 
c  Velocity[X]                                      0.13969E-03 
c  Velocity[Y]                                      0.13001E-03 
c  Velocity[Z]                                      0.43225E-02 
c  Pressure     0.36994E-04     133   0.94145E-02   0.26096E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.60253E-08   0.16857E-08 0.10151E+00 
c  r22          0.10849E-01      13   0.51409E-08   0.18368E-08 0.10221E+00 
c  r33          0.21854E-01      15   0.56539E-08   0.12728E-07 0.12880E+00 
c  r12          0.93832E-03      18   0.60706E-08   0.29816E-09 0.60604E+00 
c  r13          0.46664E-02      19   0.69912E-08   0.14909E-08 0.19993E+00 
c  r23          0.39965E-02      19   0.65015E-08   0.13104E-08 0.20234E+00 
c  epsilon      0.10972E+02      11   0.33097E-08   0.10048E-01 0.16670E+00 
c  TempC        0.25715E+06      16   0.15130E-04   0.84258E-02 0.43324E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61366       0.0052519       0.0015067
v  Velocity[Y]             -0.5737         0.54429       0.0030771      0.00087314
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.426          359.94           87.63          169.79
v  r11                   0.0010585        0.081866        0.013067        0.018283
v  r22                   0.0011087        0.082626        0.013347        0.018643
v  r33                   0.0016324          0.1743        0.027235        0.037199
v  r12                   -0.010666        0.013605     -0.00023366     -0.00030923
v  r13                   -0.045557        0.052794      9.2419e-05       0.0010133
v  r23                   -0.046704        0.051205      2.9871e-05      0.00057424
v  epsilon                0.068543          271.18          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9886e-05       0.0099175      0.00092404       0.0017423
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2785         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71347         0.85282


 TIME FOR THE TIME STEP             9866:        0.80090E+02

===============================================================


 INSTANT    0.986700000E-02   TIME STEP NUMBER            9867
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.280439665E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.187893247E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.342540592E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.193195029E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294477158E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81104E-03   0.45837E-02 0.20072E+01 
c  Velocity[X]                                      0.14044E-03 
c  Velocity[Y]                                      0.13111E-03 
c  Velocity[Z]                                      0.43122E-02 
c  Pressure     0.36412E-04     132   0.92723E-02   0.25685E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.58477E-08   0.16936E-08 0.10238E+00 
c  r22          0.10849E-01      13   0.47843E-08   0.18656E-08 0.10329E+00 
c  r33          0.21854E-01      15   0.51153E-08   0.12724E-07 0.12980E+00 
c  r12          0.93832E-03      18   0.53477E-08   0.30061E-09 0.61259E+00 
c  r13          0.46664E-02      20   0.58981E-08   0.14893E-08 0.20117E+00 
c  r23          0.39965E-02      18   0.71022E-08   0.12704E-08 0.20201E+00 
c  epsilon      0.10972E+02      11   0.32043E-08   0.98403E-02 0.16469E+00 
c  TempC        0.25715E+06      16   0.15093E-04   0.84896E-02 0.43539E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61372       0.0052519       0.0015067
v  Velocity[Y]            -0.57356         0.54448       0.0030771      0.00087318
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.412           360.1          87.694          169.92
v  r11                   0.0010585        0.081864        0.013067        0.018283
v  r22                   0.0011087        0.082625        0.013347        0.018643
v  r33                   0.0016324         0.17434        0.027235        0.037199
v  r12                   -0.010663        0.013608     -0.00023366     -0.00030923
v  r13                   -0.045556        0.052792       9.242e-05       0.0010133
v  r23                   -0.046705        0.051201      2.9872e-05      0.00057424
v  epsilon                0.068544           271.2          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9884e-05       0.0099177      0.00092404       0.0017423
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2796         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8796         0.71347         0.85282


 TIME FOR THE TIME STEP             9867:        0.81349E+02

===============================================================


 INSTANT    0.986800000E-02   TIME STEP NUMBER            9868
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.617545313E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191412626E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934904E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.103842128E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.983231760E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.893575670E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81274E-03   0.45210E-02 0.19897E+01 
c  Velocity[X]                                      0.13999E-03 
c  Velocity[Y]                                      0.12936E-03 
c  Velocity[Z]                                      0.42517E-02 
c  Pressure     0.36381E-04     131   0.92757E-02   0.25663E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.64953E-08   0.16687E-08 0.10136E+00 
c  r22          0.10849E-01      13   0.47503E-08   0.18286E-08 0.10227E+00 
c  r33          0.21854E-01      15   0.52284E-08   0.12635E-07 0.12887E+00 
c  r12          0.93832E-03      18   0.55003E-08   0.30238E-09 0.60924E+00 
c  r13          0.46664E-02      20   0.58621E-08   0.15114E-08 0.20166E+00 
c  r23          0.39965E-02      19   0.54401E-08   0.12944E-08 0.20209E+00 
c  epsilon      0.10972E+02      11   0.32978E-08   0.10412E-01 0.17183E+00 
c  TempC        0.25715E+06      16   0.15133E-04   0.84529E-02 0.43389E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161988


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61369       0.0052519       0.0015067
v  Velocity[Y]            -0.57368         0.54414       0.0030771      0.00087314
v  Velocity[Z]              1.5657          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4369          4.3406          4.3632
v  Pressure                -36.399          360.11          87.733          169.94
v  r11                   0.0010585        0.081864        0.013067        0.018283
v  r22                   0.0011087        0.082624        0.013347        0.018643
v  r33                   0.0016324         0.17432        0.027235        0.037199
v  r12                   -0.010664        0.013604     -0.00023366     -0.00030923
v  r13                   -0.045558         0.05279      9.2422e-05       0.0010133
v  r23                   -0.046706        0.051196      2.9873e-05      0.00057424
v  epsilon                0.068544          271.21          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9884e-05       0.0099178      0.00092405       0.0017423
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2799         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8799         0.71347         0.85282


 TIME FOR THE TIME STEP             9868:        0.80271E+02

===============================================================


 INSTANT    0.986900000E-02   TIME STEP NUMBER            9869
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.110567165E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.180479030E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.300668944E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.268062046E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129101008E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      40   0.81116E-03   0.45436E-02 0.19952E+01 
c  Velocity[X]                                      0.13947E-03 
c  Velocity[Y]                                      0.12820E-03 
c  Velocity[Z]                                      0.42759E-02 
c  Pressure     0.36629E-04     133   0.93276E-02   0.25839E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.69980E-08   0.16444E-08 0.10085E+00 
c  r22          0.10849E-01      13   0.48512E-08   0.18189E-08 0.10241E+00 
c  r33          0.21854E-01      15   0.62640E-08   0.12479E-07 0.12835E+00 
c  r12          0.93832E-03      18   0.54633E-08   0.29577E-09 0.60575E+00 
c  r13          0.46664E-02      19   0.70403E-08   0.14910E-08 0.20018E+00 
c  r23          0.39965E-02      19   0.64685E-08   0.12801E-08 0.20066E+00 
c  epsilon      0.10972E+02      11   0.35097E-08   0.96163E-02 0.16242E+00 
c  TempC        0.25715E+06      16   0.15125E-04   0.84515E-02 0.43344E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161987


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61367       0.0052519       0.0015067
v  Velocity[Y]             -0.5736         0.54419       0.0030771      0.00087313
v  Velocity[Z]              1.5658          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4369          4.3406          4.3632
v  Pressure                -36.376           360.1          87.705          169.92
v  r11                   0.0010585        0.081865        0.013067        0.018283
v  r22                   0.0011087        0.082618        0.013347        0.018643
v  r33                   0.0016324         0.17429        0.027235        0.037199
v  r12                   -0.010662        0.013604     -0.00023366     -0.00030923
v  r13                   -0.045557        0.052792      9.2424e-05       0.0010133
v  r23                   -0.046706        0.051219      2.9874e-05      0.00057424
v  epsilon                0.068544          271.18          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9883e-05       0.0099177      0.00092405       0.0017423
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2795         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8795         0.71347         0.85282


 TIME FOR THE TIME STEP             9869:        0.80359E+02

===============================================================


 INSTANT    0.987000000E-02   TIME STEP NUMBER            9870
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.413143246E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.646616540E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.176912643E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.231442662E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.231437943E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81134E-03   0.45972E-02 0.20099E+01 
c  Velocity[X]                                      0.14118E-03 
c  Velocity[Y]                                      0.13132E-03 
c  Velocity[Z]                                      0.43247E-02 
c  Pressure     0.36977E-04     132   0.94094E-02   0.26085E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.67020E-08   0.16373E-08 0.10114E+00 
c  r22          0.10849E-01      13   0.52912E-08   0.18235E-08 0.10278E+00 
c  r33          0.21855E-01      15   0.56310E-08   0.12531E-07 0.12909E+00 
c  r12          0.93832E-03      18   0.57947E-08   0.29853E-09 0.60944E+00 
c  r13          0.46664E-02      19   0.69052E-08   0.15015E-08 0.20164E+00 
c  r23          0.39965E-02      19   0.73930E-08   0.12910E-08 0.20217E+00 
c  epsilon      0.10972E+02      11   0.35294E-08   0.98341E-02 0.16582E+00 
c  TempC        0.25715E+06      16   0.15125E-04   0.84268E-02 0.43271E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61371        0.005252       0.0015067
v  Velocity[Y]            -0.57363          0.5443       0.0030771      0.00087314
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.436          360.04          87.681          169.88
v  r11                   0.0010585        0.081862        0.013067        0.018283
v  r22                   0.0011087        0.082617        0.013347        0.018643
v  r33                   0.0016325         0.17431        0.027235        0.037199
v  r12                   -0.010659        0.013602     -0.00023366     -0.00030923
v  r13                   -0.045555        0.052793      9.2427e-05       0.0010133
v  r23                   -0.046707        0.051212      2.9875e-05      0.00057424
v  epsilon                0.068545          271.18          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9886e-05       0.0099173      0.00092405       0.0017423
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2779         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71347         0.85282


 TIME FOR THE TIME STEP             9870:        0.78940E+02

===============================================================


 INSTANT    0.987100000E-02   TIME STEP NUMBER            9871
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.387876055E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184340728E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181239915E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.122444545E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.902309335E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81202E-03   0.45526E-02 0.19997E+01 
c  Velocity[X]                                      0.13879E-03 
c  Velocity[Y]                                      0.13087E-03 
c  Velocity[Z]                                      0.42829E-02 
c  Pressure     0.36592E-04     132   0.93196E-02   0.25813E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.63998E-08   0.16446E-08 0.10093E+00 
c  r22          0.10849E-01      13   0.53724E-08   0.18003E-08 0.10193E+00 
c  r33          0.21855E-01      15   0.54338E-08   0.12395E-07 0.12792E+00 
c  r12          0.93832E-03      18   0.51447E-08   0.29669E-09 0.60704E+00 
c  r13          0.46665E-02      19   0.56593E-08   0.14807E-08 0.19962E+00 
c  r23          0.39965E-02      19   0.64122E-08   0.12701E-08 0.19967E+00 
c  epsilon      0.10972E+02      11   0.34190E-08   0.98612E-02 0.16635E+00 
c  TempC        0.25715E+06      16   0.15104E-04   0.84239E-02 0.43308E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161986


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386          0.6137       0.0052519       0.0015067
v  Velocity[Y]            -0.57345         0.54438       0.0030771      0.00087319
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                 -36.39             360          87.637          169.84
v  r11                   0.0010585        0.081861        0.013067        0.018283
v  r22                   0.0011087        0.082617        0.013347        0.018643
v  r33                   0.0016325         0.17432        0.027235        0.037199
v  r12                   -0.010656        0.013603     -0.00023366     -0.00030923
v  r13                   -0.045558        0.052792      9.2428e-05       0.0010133
v  r23                   -0.046707        0.051193      2.9876e-05      0.00057424
v  epsilon                0.068545          271.21          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9889e-05       0.0099173      0.00092405       0.0017423
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2772         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71347         0.85282


 TIME FOR THE TIME STEP             9871:        0.80755E+02

===============================================================


 INSTANT    0.987200000E-02   TIME STEP NUMBER            9872
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.422183093E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154917778E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.458733272E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.367685408E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.246428244E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81147E-03   0.45412E-02 0.19980E+01 
c  Velocity[X]                                      0.13950E-03 
c  Velocity[Y]                                      0.13045E-03 
c  Velocity[Z]                                      0.42712E-02 
c  Pressure     0.36665E-04     131   0.93335E-02   0.25864E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.57231E-08   0.16359E-08 0.10074E+00 
c  r22          0.10849E-01      13   0.52683E-08   0.18004E-08 0.10195E+00 
c  r33          0.21855E-01      15   0.53274E-08   0.12296E-07 0.12764E+00 
c  r12          0.93832E-03      18   0.52153E-08   0.30171E-09 0.60924E+00 
c  r13          0.46665E-02      19   0.62317E-08   0.14749E-08 0.19960E+00 
c  r23          0.39965E-02      19   0.61056E-08   0.12770E-08 0.19997E+00 
c  epsilon      0.10972E+02      11   0.31760E-08   0.96298E-02 0.16421E+00 
c  TempC        0.25715E+06      16   0.15118E-04   0.84791E-02 0.43499E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161988


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61366        0.005252       0.0015067
v  Velocity[Y]            -0.57352         0.54421       0.0030771      0.00087315
v  Velocity[Z]              1.5659          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5797          5.4369          4.3406          4.3632
v  Pressure                -36.385          360.01          87.654          169.85
v  r11                   0.0010585        0.081856        0.013067        0.018283
v  r22                   0.0011087        0.082618        0.013347        0.018643
v  r33                   0.0016325          0.1743        0.027235        0.037199
v  r12                   -0.010654        0.013603     -0.00023366     -0.00030923
v  r13                   -0.045556        0.052792      9.2429e-05       0.0010133
v  r23                   -0.046707        0.051217      2.9877e-05      0.00057425
v  epsilon                0.068545          271.22          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9887e-05       0.0099175      0.00092405       0.0017423
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2771         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71347         0.85282


 TIME FOR THE TIME STEP             9872:        0.80998E+02

===============================================================


 INSTANT    0.987300000E-02   TIME STEP NUMBER            9873
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.378201121E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.573373698E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.354061322E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140649945E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221068192E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81113E-03   0.45752E-02 0.20030E+01 
c  Velocity[X]                                      0.14071E-03 
c  Velocity[Y]                                      0.13021E-03 
c  Velocity[Z]                                      0.43043E-02 
c  Pressure     0.36576E-04     133   0.93027E-02   0.25801E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.58462E-08   0.16343E-08 0.10067E+00 
c  r22          0.10849E-01      13   0.53472E-08   0.18328E-08 0.10273E+00 
c  r33          0.21855E-01      15   0.63692E-08   0.12356E-07 0.12804E+00 
c  r12          0.93832E-03      18   0.58295E-08   0.30652E-09 0.61514E+00 
c  r13          0.46665E-02      19   0.71521E-08   0.14859E-08 0.20081E+00 
c  r23          0.39965E-02      19   0.60087E-08   0.12710E-08 0.19987E+00 
c  epsilon      0.10972E+02      11   0.31851E-08   0.96298E-02 0.16353E+00 
c  TempC        0.25715E+06      16   0.15112E-04   0.84338E-02 0.43361E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61371        0.005252       0.0015067
v  Velocity[Y]            -0.57352          0.5443       0.0030771      0.00087317
v  Velocity[Z]              1.5658          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4369          4.3406          4.3632
v  Pressure                -36.406          360.09          87.702          169.91
v  r11                   0.0010586        0.081859        0.013067        0.018283
v  r22                   0.0011087        0.082618        0.013347        0.018643
v  r33                   0.0016325         0.17428        0.027235        0.037199
v  r12                   -0.010651        0.013608     -0.00023366     -0.00030923
v  r13                   -0.045556        0.052789      9.2432e-05       0.0010133
v  r23                   -0.046707        0.051211      2.9879e-05      0.00057425
v  epsilon                0.068546          271.17          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9888e-05       0.0099177      0.00092405       0.0017423
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2768         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71347         0.85282


 TIME FOR THE TIME STEP             9873:        0.81635E+02

===============================================================


 INSTANT    0.987400000E-02   TIME STEP NUMBER            9874
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.843636244E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.545306917E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.153786195E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.498633560E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.176442509E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81283E-03   0.45538E-02 0.19976E+01 
c  Velocity[X]                                      0.13937E-03 
c  Velocity[Y]                                      0.12976E-03 
c  Velocity[Z]                                      0.42847E-02 
c  Pressure     0.36646E-04     131   0.93322E-02   0.25850E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.58644E-08   0.16638E-08 0.10115E+00 
c  r22          0.10849E-01      13   0.53438E-08   0.18212E-08 0.10201E+00 
c  r33          0.21855E-01      15   0.63647E-08   0.12613E-07 0.12895E+00 
c  r12          0.93833E-03      18   0.61360E-08   0.29614E-09 0.60765E+00 
c  r13          0.46665E-02      20   0.62190E-08   0.14888E-08 0.20055E+00 
c  r23          0.39965E-02      19   0.65350E-08   0.13024E-08 0.20300E+00 
c  epsilon      0.10972E+02      11   0.33116E-08   0.10236E-01 0.17130E+00 
c  TempC        0.25715E+06      16   0.15153E-04   0.84178E-02 0.43266E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61368       0.0052519       0.0015067
v  Velocity[Y]            -0.57362         0.54446       0.0030772      0.00087315
v  Velocity[Z]              1.5658          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4369          4.3406          4.3632
v  Pressure                -36.406          360.06          87.701           169.9
v  r11                   0.0010586        0.081857        0.013067        0.018283
v  r22                   0.0011087        0.082619        0.013347        0.018643
v  r33                   0.0016325         0.17429        0.027235        0.037199
v  r12                   -0.010647        0.013607     -0.00023366     -0.00030924
v  r13                   -0.045559        0.052792      9.2434e-05       0.0010133
v  r23                   -0.046707        0.051206       2.988e-05      0.00057425
v  epsilon                0.068546           271.2          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9886e-05        0.009918      0.00092406       0.0017423
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2767         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767         0.71347         0.85282


 TIME FOR THE TIME STEP             9874:        0.81139E+02

===============================================================


 INSTANT    0.987500000E-02   TIME STEP NUMBER            9875
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.250287558E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.260571782E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.176142916E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.463947877E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.165642700E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81097E-03   0.45790E-02 0.20043E+01 
c  Velocity[X]                                      0.13964E-03 
c  Velocity[Y]                                      0.13059E-03 
c  Velocity[Z]                                      0.43087E-02 
c  Pressure     0.36906E-04     131   0.94023E-02   0.26033E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.60969E-08   0.16197E-08 0.10032E+00 
c  r22          0.10849E-01      13   0.56375E-08   0.17909E-08 0.10165E+00 
c  r33          0.21855E-01      15   0.63658E-08   0.12293E-07 0.12768E+00 
c  r12          0.93833E-03      18   0.65103E-08   0.29702E-09 0.60786E+00 
c  r13          0.46665E-02      20   0.60019E-08   0.14856E-08 0.19993E+00 
c  r23          0.39965E-02      19   0.67487E-08   0.12650E-08 0.19969E+00 
c  epsilon      0.10972E+02      11   0.34862E-08   0.95742E-02 0.16306E+00 
c  TempC        0.25715E+06      16   0.15108E-04   0.84791E-02 0.43409E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61367       0.0052519       0.0015067
v  Velocity[Y]            -0.57354         0.54417       0.0030772      0.00087318
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.396          360.05          87.671          169.88
v  r11                   0.0010586        0.081857        0.013067        0.018283
v  r22                   0.0011088        0.082619        0.013347        0.018643
v  r33                   0.0016325         0.17432        0.027235        0.037199
v  r12                   -0.010646        0.013609     -0.00023367     -0.00030924
v  r13                   -0.045557         0.05279      9.2436e-05       0.0010134
v  r23                   -0.046707        0.051224       2.988e-05      0.00057425
v  epsilon                0.068546          271.21          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9886e-05        0.009918      0.00092406       0.0017423
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2763         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8763         0.71347         0.85282


 TIME FOR THE TIME STEP             9875:        0.82775E+02

===============================================================


 INSTANT    0.987600000E-02   TIME STEP NUMBER            9876
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.984571597E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.925559880E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.254413291E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.126206803E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168423641E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81162E-03   0.45711E-02 0.20035E+01 
c  Velocity[X]                                      0.14097E-03 
c  Velocity[Y]                                      0.13036E-03 
c  Velocity[Z]                                      0.42998E-02 
c  Pressure     0.36403E-04     133   0.92665E-02   0.25680E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.65773E-08   0.16492E-08 0.10079E+00 
c  r22          0.10849E-01      13   0.57147E-08   0.18318E-08 0.10229E+00 
c  r33          0.21855E-01      15   0.66362E-08   0.12605E-07 0.12826E+00 
c  r12          0.93833E-03      18   0.65361E-08   0.29895E-09 0.60978E+00 
c  r13          0.46665E-02      20   0.59772E-08   0.15000E-08 0.20087E+00 
c  r23          0.39965E-02      19   0.71436E-08   0.13028E-08 0.20133E+00 
c  epsilon      0.10972E+02      11   0.35911E-08   0.10129E-01 0.16561E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.84473E-02 0.43418E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61371        0.005252       0.0015067
v  Velocity[Y]            -0.57361         0.54418       0.0030771      0.00087313
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.447             360          87.644          169.84
v  r11                   0.0010586        0.081863        0.013067        0.018283
v  r22                   0.0011088        0.082615        0.013347        0.018643
v  r33                   0.0016325         0.17431        0.027235        0.037199
v  r12                   -0.010645        0.013603     -0.00023367     -0.00030924
v  r13                   -0.045555         0.05279      9.2438e-05       0.0010134
v  r23                   -0.046706        0.051212      2.9881e-05      0.00057425
v  epsilon                0.068547          271.21          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9882e-05       0.0099176      0.00092406       0.0017423
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2764         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8764         0.71347         0.85282


 TIME FOR THE TIME STEP             9876:        0.80415E+02

===============================================================


 INSTANT    0.987700000E-02   TIME STEP NUMBER            9877
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.416797406E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.208769162E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188553753E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.619913623E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.170164473E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      40   0.81209E-03   0.45401E-02 0.19944E+01 
c  Velocity[X]                                      0.13953E-03 
c  Velocity[Y]                                      0.12942E-03 
c  Velocity[Z]                                      0.42711E-02 
c  Pressure     0.36425E-04     133   0.92707E-02   0.25693E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.69298E-08   0.16259E-08 0.10008E+00 
c  r22          0.10849E-01      13   0.61609E-08   0.18101E-08 0.10182E+00 
c  r33          0.21855E-01      15   0.70398E-08   0.12421E-07 0.12753E+00 
c  r12          0.93833E-03      18   0.67723E-08   0.29590E-09 0.60788E+00 
c  r13          0.46665E-02      20   0.60881E-08   0.14997E-08 0.20063E+00 
c  r23          0.39965E-02      20   0.55909E-08   0.12827E-08 0.19958E+00 
c  epsilon      0.10972E+02      11   0.34916E-08   0.96869E-02 0.16408E+00 
c  TempC        0.25716E+06      16   0.15118E-04   0.83970E-02 0.43275E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61365        0.005252       0.0015067
v  Velocity[Y]            -0.57365         0.54429       0.0030772      0.00087314
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.341          360.07          87.681          169.89
v  r11                   0.0010586        0.081866        0.013067        0.018283
v  r22                   0.0011088        0.082616        0.013347        0.018643
v  r33                   0.0016325         0.17428        0.027235        0.037199
v  r12                   -0.010644        0.013603     -0.00023367     -0.00030924
v  r13                   -0.045559         0.05279      9.2441e-05       0.0010134
v  r23                   -0.046705        0.051191      2.9882e-05      0.00057425
v  epsilon                0.068547          271.18          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9881e-05       0.0099177      0.00092406       0.0017423
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2771         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71347         0.85282


 TIME FOR THE TIME STEP             9877:        0.81232E+02

===============================================================


 INSTANT    0.987800000E-02   TIME STEP NUMBER            9878
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.947673565E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.377781491E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.485767400E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.637661688E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.479812504E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      40   0.81162E-03   0.45566E-02 0.19994E+01 
c  Velocity[X]                                      0.13973E-03 
c  Velocity[Y]                                      0.12988E-03 
c  Velocity[Z]                                      0.42870E-02 
c  Pressure     0.36487E-04     132   0.92926E-02   0.25738E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.64267E-08   0.16464E-08 0.10103E+00 
c  r22          0.10849E-01      13   0.62146E-08   0.18262E-08 0.10277E+00 
c  r33          0.21855E-01      15   0.73538E-08   0.12492E-07 0.12876E+00 
c  r12          0.93833E-03      18   0.64648E-08   0.30047E-09 0.61356E+00 
c  r13          0.46665E-02      20   0.58523E-08   0.14903E-08 0.20144E+00 
c  r23          0.39965E-02      20   0.61878E-08   0.12854E-08 0.20171E+00 
c  epsilon      0.10972E+02      11   0.34611E-08   0.96384E-02 0.16636E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.84169E-02 0.43261E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61371       0.0052519       0.0015067
v  Velocity[Y]            -0.57377         0.54447       0.0030771       0.0008731
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.431          360.05          87.703           169.9
v  r11                   0.0010586        0.081863        0.013067        0.018283
v  r22                   0.0011088        0.082617        0.013347        0.018643
v  r33                   0.0016326          0.1743        0.027236        0.037199
v  r12                   -0.010647        0.013609     -0.00023367     -0.00030924
v  r13                   -0.045556         0.05279      9.2443e-05       0.0010134
v  r23                   -0.046703        0.051211      2.9883e-05      0.00057425
v  epsilon                0.068547          271.19          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9879e-05       0.0099178      0.00092406       0.0017423
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2774         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71347         0.85282


 TIME FOR THE TIME STEP             9878:        0.79429E+02

===============================================================


 INSTANT    0.987900000E-02   TIME STEP NUMBER            9879
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.365129756E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.113128308E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.259835600E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106948828E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.169277980E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21880E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81177E-03   0.45679E-02 0.20023E+01 
c  Velocity[X]                                      0.14003E-03 
c  Velocity[Y]                                      0.13045E-03 
c  Velocity[Z]                                      0.42974E-02 
c  Pressure     0.36999E-04     132   0.94157E-02   0.26099E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.64361E-08   0.16502E-08 0.10078E+00 
c  r22          0.10849E-01      13   0.62993E-08   0.18209E-08 0.10224E+00 
c  r33          0.21855E-01      15   0.73260E-08   0.12512E-07 0.12813E+00 
c  r12          0.93833E-03      18   0.63739E-08   0.29467E-09 0.60747E+00 
c  r13          0.46665E-02      20   0.59678E-08   0.14789E-08 0.20035E+00 
c  r23          0.39965E-02      20   0.62328E-08   0.12876E-08 0.20054E+00 
c  epsilon      0.10972E+02      11   0.34109E-08   0.97546E-02 0.16489E+00 
c  TempC        0.25716E+06      16   0.15086E-04   0.85119E-02 0.43468E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61369        0.005252       0.0015067
v  Velocity[Y]            -0.57381         0.54413       0.0030771      0.00087311
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.416          360.05          87.661          169.87
v  r11                   0.0010586         0.08186        0.013067        0.018283
v  r22                   0.0011088        0.082617        0.013347        0.018643
v  r33                   0.0016326         0.17433        0.027236          0.0372
v  r12                    -0.01065        0.013609     -0.00023367     -0.00030924
v  r13                   -0.045555        0.052789      9.2444e-05       0.0010134
v  r23                   -0.046702        0.051204      2.9883e-05      0.00057425
v  epsilon                0.068548          271.21          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9876e-05       0.0099179      0.00092406       0.0017423
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2783         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71347         0.85282


 TIME FOR THE TIME STEP             9879:        0.79275E+02

===============================================================


 INSTANT    0.988000000E-02   TIME STEP NUMBER            9880
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.364114207E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.382373801E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.437937301E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.699738045E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.252416206E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40347E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81194E-03   0.45302E-02 0.19939E+01 
c  Velocity[X]                                      0.13985E-03 
c  Velocity[Y]                                      0.12942E-03 
c  Velocity[Z]                                      0.42610E-02 
c  Pressure     0.36803E-04     133   0.93695E-02   0.25961E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.62973E-08   0.16902E-08 0.10187E+00 
c  r22          0.10849E-01      13   0.65357E-08   0.18620E-08 0.10269E+00 
c  r33          0.21855E-01      15   0.57229E-08   0.12936E-07 0.12977E+00 
c  r12          0.93833E-03      18   0.66989E-08   0.30295E-09 0.61239E+00 
c  r13          0.46665E-02      19   0.73153E-08   0.15279E-08 0.20145E+00 
c  r23          0.39965E-02      19   0.64717E-08   0.13338E-08 0.20443E+00 
c  epsilon      0.10972E+02      11   0.34707E-08   0.10484E-01 0.17341E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.83940E-02 0.43295E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63377         0.61364        0.005252       0.0015067
v  Velocity[Y]            -0.57387         0.54416       0.0030771       0.0008731
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.425          360.09          87.705          169.91
v  r11                   0.0010586        0.081851        0.013067        0.018283
v  r22                   0.0011088        0.082617        0.013347        0.018643
v  r33                   0.0016326          0.1743        0.027236          0.0372
v  r12                   -0.010653        0.013612     -0.00023367     -0.00030924
v  r13                   -0.045558        0.052789      9.2446e-05       0.0010134
v  r23                   -0.046699        0.051193      2.9884e-05      0.00057425
v  epsilon                0.068548          271.21          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9875e-05        0.009918      0.00092406       0.0017423
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2783         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71347         0.85282


 TIME FOR THE TIME STEP             9880:        0.77520E+02

===============================================================


 INSTANT    0.988100000E-02   TIME STEP NUMBER            9881
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.247843100E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.103618353E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.386230855E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.484804500E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105153605E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81183E-03   0.45894E-02 0.20050E+01 
c  Velocity[X]                                      0.13960E-03 
c  Velocity[Y]                                      0.13048E-03 
c  Velocity[Z]                                      0.43193E-02 
c  Pressure     0.36587E-04     133   0.93120E-02   0.25810E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.58308E-08   0.16491E-08 0.10095E+00 
c  r22          0.10849E-01      13   0.62040E-08   0.18467E-08 0.10270E+00 
c  r33          0.21855E-01      15   0.60962E-08   0.12534E-07 0.12832E+00 
c  r12          0.93833E-03      18   0.66557E-08   0.29749E-09 0.60872E+00 
c  r13          0.46665E-02      19   0.61052E-08   0.14930E-08 0.20021E+00 
c  r23          0.39965E-02      19   0.64325E-08   0.12626E-08 0.19929E+00 
c  epsilon      0.10972E+02      11   0.34249E-08   0.98521E-02 0.16501E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.84172E-02 0.43325E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385          0.6137        0.005252       0.0015067
v  Velocity[Y]            -0.57379         0.54427       0.0030772       0.0008731
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.386          360.04          87.664          169.87
v  r11                   0.0010586        0.081851        0.013067        0.018283
v  r22                   0.0011088        0.082613        0.013347        0.018643
v  r33                   0.0016326         0.17428        0.027236          0.0372
v  r12                   -0.010652        0.013609     -0.00023367     -0.00030924
v  r13                   -0.045557        0.052789      9.2449e-05       0.0010134
v  r23                   -0.046697        0.051182      2.9885e-05      0.00057425
v  epsilon                0.068548          271.18          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9875e-05        0.009918      0.00092407       0.0017423
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2781         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71347         0.85282


 TIME FOR THE TIME STEP             9881:        0.74829E+02

===============================================================


 INSTANT    0.988200000E-02   TIME STEP NUMBER            9882
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181236511E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.105790234E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.321759414E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.323881927E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.215723832E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81204E-03   0.45794E-02 0.20040E+01 
c  Velocity[X]                                      0.14018E-03 
c  Velocity[Y]                                      0.13061E-03 
c  Velocity[Z]                                      0.43086E-02 
c  Pressure     0.36432E-04     133   0.92747E-02   0.25700E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.57408E-08   0.16353E-08 0.10051E+00 
c  r22          0.10849E-01      13   0.61175E-08   0.18222E-08 0.10215E+00 
c  r33          0.21855E-01      14   0.69210E-08   0.12452E-07 0.12800E+00 
c  r12          0.93833E-03      18   0.71370E-08   0.29983E-09 0.60880E+00 
c  r13          0.46665E-02      19   0.54710E-08   0.15080E-08 0.20096E+00 
c  r23          0.39965E-02      19   0.66923E-08   0.12823E-08 0.20077E+00 
c  epsilon      0.10972E+02      11   0.35004E-08   0.96755E-02 0.16378E+00 
c  TempC        0.25716E+06      16   0.15120E-04   0.84717E-02 0.43408E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61367        0.005252       0.0015067
v  Velocity[Y]            -0.57389         0.54443       0.0030772      0.00087309
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.472          360.02          87.663          169.86
v  r11                   0.0010586         0.08185        0.013067        0.018283
v  r22                   0.0011088        0.082614        0.013347        0.018643
v  r33                   0.0016326          0.1743        0.027236          0.0372
v  r12                   -0.010652        0.013612     -0.00023367     -0.00030924
v  r13                   -0.045555        0.052789      9.2451e-05       0.0010134
v  r23                   -0.046695        0.051211      2.9885e-05      0.00057425
v  epsilon                0.068549           271.2          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9876e-05        0.009918      0.00092407       0.0017423
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2775         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71347         0.85282


 TIME FOR THE TIME STEP             9882:        0.78139E+02

===============================================================


 INSTANT    0.988300000E-02   TIME STEP NUMBER            9883
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.519373775E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.108468524E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.938044233E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.488853730E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115743685E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81159E-03   0.45179E-02 0.19906E+01 
c  Velocity[X]                                      0.13887E-03 
c  Velocity[Y]                                      0.13056E-03 
c  Velocity[Z]                                      0.42484E-02 
c  Pressure     0.36305E-04     132   0.92473E-02   0.25609E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.58297E-08   0.16548E-08 0.10097E+00 
c  r22          0.10849E-01      13   0.62097E-08   0.17982E-08 0.10156E+00 
c  r33          0.21855E-01      15   0.52786E-08   0.12457E-07 0.12793E+00 
c  r12          0.93833E-03      18   0.72899E-08   0.30253E-09 0.61274E+00 
c  r13          0.46665E-02      19   0.59654E-08   0.14774E-08 0.19964E+00 
c  r23          0.39965E-02      19   0.67714E-08   0.12921E-08 0.20170E+00 
c  epsilon      0.10972E+02      11   0.33569E-08   0.97024E-02 0.16426E+00 
c  TempC        0.25716E+06      16   0.15088E-04   0.85206E-02 0.43513E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61362        0.005252       0.0015067
v  Velocity[Y]            -0.57374         0.54421       0.0030772      0.00087308
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.412          360.09          87.694          169.91
v  r11                   0.0010586        0.081849        0.013067        0.018283
v  r22                   0.0011089        0.082615        0.013347        0.018643
v  r33                   0.0016326         0.17433        0.027236          0.0372
v  r12                   -0.010653        0.013607     -0.00023367     -0.00030924
v  r13                   -0.045558        0.052788      9.2452e-05       0.0010134
v  r23                   -0.046694        0.051196      2.9886e-05      0.00057425
v  epsilon                0.068549          271.23          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9877e-05        0.009918      0.00092407       0.0017423
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2784         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71347         0.85282


 TIME FOR THE TIME STEP             9883:        0.78248E+02

===============================================================


 INSTANT    0.988400000E-02   TIME STEP NUMBER            9884
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.188883221E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.215631446E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.139637840E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.365269974E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.334852049E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81247E-03   0.45667E-02 0.20006E+01 
c  Velocity[X]                                      0.14036E-03 
c  Velocity[Y]                                      0.13107E-03 
c  Velocity[Z]                                      0.42953E-02 
c  Pressure     0.36743E-04     132   0.93535E-02   0.25920E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.58822E-08   0.16726E-08 0.10149E+00 
c  r22          0.10849E-01      13   0.62104E-08   0.18251E-08 0.10223E+00 
c  r33          0.21855E-01      14   0.70544E-08   0.12570E-07 0.12865E+00 
c  r12          0.93833E-03      18   0.71031E-08   0.30198E-09 0.61211E+00 
c  r13          0.46665E-02      19   0.59037E-08   0.14699E-08 0.19951E+00 
c  r23          0.39965E-02      19   0.64137E-08   0.12984E-08 0.20219E+00 
c  epsilon      0.10972E+02      11   0.32362E-08   0.96399E-02 0.16359E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.84434E-02 0.43333E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63395         0.61363        0.005252       0.0015067
v  Velocity[Y]            -0.57387         0.54428       0.0030772      0.00087309
v  Velocity[Z]              1.5657          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.448          360.03          87.667          169.86
v  r11                   0.0010586        0.081845        0.013067        0.018283
v  r22                   0.0011089        0.082617        0.013347        0.018643
v  r33                   0.0016326         0.17431        0.027236          0.0372
v  r12                   -0.010651        0.013609     -0.00023367     -0.00030924
v  r13                   -0.045556        0.052789      9.2455e-05       0.0010134
v  r23                   -0.046693         0.05119      2.9887e-05      0.00057425
v  epsilon                0.068549          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.988e-05        0.009918      0.00092407       0.0017423
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2786         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71347         0.85282


 TIME FOR THE TIME STEP             9884:        0.78371E+02

===============================================================


 INSTANT    0.988500000E-02   TIME STEP NUMBER            9885
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.843620372E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.699506783E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171357232E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201128909E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.244893844E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81162E-03   0.45898E-02 0.20062E+01 
c  Velocity[X]                                      0.14059E-03 
c  Velocity[Y]                                      0.12976E-03 
c  Velocity[Z]                                      0.43195E-02 
c  Pressure     0.36388E-04     133   0.92540E-02   0.25669E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.58133E-08   0.16187E-08 0.10034E+00 
c  r22          0.10849E-01      13   0.59636E-08   0.17937E-08 0.10151E+00 
c  r33          0.21855E-01      15   0.51926E-08   0.12274E-07 0.12741E+00 
c  r12          0.93833E-03      18   0.69720E-08   0.29395E-09 0.60548E+00 
c  r13          0.46665E-02      19   0.68251E-08   0.14728E-08 0.20003E+00 
c  r23          0.39965E-02      19   0.64571E-08   0.12588E-08 0.19920E+00 
c  epsilon      0.10972E+02      11   0.32782E-08   0.94197E-02 0.16205E+00 
c  TempC        0.25716E+06      16   0.15108E-04   0.83953E-02 0.43259E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61363        0.005252       0.0015067
v  Velocity[Y]            -0.57386         0.54444       0.0030772      0.00087307
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.409          360.04          87.656          169.86
v  r11                   0.0010587        0.081852        0.013067        0.018283
v  r22                   0.0011089        0.082617        0.013347        0.018643
v  r33                   0.0016326          0.1743        0.027236          0.0372
v  r12                    -0.01065        0.013612     -0.00023367     -0.00030924
v  r13                   -0.045556        0.052787      9.2457e-05       0.0010134
v  r23                   -0.046693        0.051191      2.9888e-05      0.00057425
v  epsilon                0.068549           271.2          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9884e-05       0.0099179      0.00092407       0.0017423
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2786         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71347         0.85282


 TIME FOR THE TIME STEP             9885:        0.78355E+02

===============================================================


 INSTANT    0.988600000E-02   TIME STEP NUMBER            9886
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.415619409E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.278565914E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.319948319E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.307685875E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.242540038E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      40   0.81152E-03   0.45366E-02 0.19962E+01 
c  Velocity[X]                                      0.13917E-03 
c  Velocity[Y]                                      0.12980E-03 
c  Velocity[Z]                                      0.42677E-02 
c  Pressure     0.36690E-04     131   0.93452E-02   0.25882E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.60712E-08   0.16893E-08 0.10159E+00 
c  r22          0.10849E-01      13   0.57174E-08   0.18416E-08 0.10235E+00 
c  r33          0.21855E-01      15   0.53844E-08   0.12831E-07 0.12939E+00 
c  r12          0.93833E-03      18   0.65842E-08   0.30154E-09 0.61025E+00 
c  r13          0.46665E-02      19   0.63266E-08   0.15084E-08 0.20140E+00 
c  r23          0.39965E-02      19   0.70193E-08   0.13140E-08 0.20280E+00 
c  epsilon      0.10972E+02      11   0.34097E-08   0.10438E-01 0.17359E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.84006E-02 0.43258E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61358        0.005252       0.0015067
v  Velocity[Y]            -0.57395         0.54414       0.0030771      0.00087304
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.471          360.06          87.694          169.89
v  r11                   0.0010587        0.081863        0.013067        0.018283
v  r22                   0.0011089        0.082617        0.013347        0.018643
v  r33                   0.0016326         0.17431        0.027236          0.0372
v  r12                    -0.01065        0.013609     -0.00023367     -0.00030924
v  r13                   -0.045559        0.052787      9.2459e-05       0.0010134
v  r23                   -0.046693        0.051216      2.9889e-05      0.00057425
v  epsilon                 0.06855          271.21          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9889e-05       0.0099178      0.00092407       0.0017423
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2785         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71347         0.85282


 TIME FOR THE TIME STEP             9886:        0.79554E+02

===============================================================


 INSTANT    0.988700000E-02   TIME STEP NUMBER            9887
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.443344213E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.308574589E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.257766048E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.165730037E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.143535080E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40348E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81239E-03   0.45494E-02 0.19988E+01 
c  Velocity[X]                                      0.13987E-03 
c  Velocity[Y]                                      0.12976E-03 
c  Velocity[Z]                                      0.42798E-02 
c  Pressure     0.36757E-04     133   0.93562E-02   0.25929E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.58098E-08   0.16386E-08 0.99948E-01 
c  r22          0.10849E-01      13   0.57303E-08   0.18309E-08 0.10206E+00 
c  r33          0.21855E-01      15   0.63095E-08   0.12476E-07 0.12762E+00 
c  r12          0.93833E-03      18   0.58021E-08   0.29906E-09 0.60777E+00 
c  r13          0.46665E-02      19   0.56419E-08   0.14821E-08 0.19969E+00 
c  r23          0.39965E-02      19   0.64688E-08   0.12776E-08 0.19889E+00 
c  epsilon      0.10972E+02      11   0.34432E-08   0.98269E-02 0.16598E+00 
c  TempC        0.25716E+06      16   0.15100E-04   0.84840E-02 0.43469E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61364        0.005252       0.0015067
v  Velocity[Y]            -0.57379         0.54415       0.0030771      0.00087308
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.441          360.05          87.674          169.88
v  r11                   0.0010587        0.081868        0.013067        0.018283
v  r22                   0.0011089        0.082613        0.013347        0.018643
v  r33                   0.0016326         0.17435        0.027236          0.0372
v  r12                   -0.010647        0.013612     -0.00023367     -0.00030924
v  r13                   -0.045556        0.052788      9.2461e-05       0.0010134
v  r23                   -0.046694        0.051205      2.9889e-05      0.00057425
v  epsilon                 0.06855          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9895e-05       0.0099177      0.00092407       0.0017423
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2783         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71347         0.85282


 TIME FOR THE TIME STEP             9887:        0.79525E+02

===============================================================


 INSTANT    0.988800000E-02   TIME STEP NUMBER            9888
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184918702E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.183159869E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.912050735E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.162660135E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.288555078E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81162E-03   0.45574E-02 0.20001E+01 
c  Velocity[X]                                      0.13964E-03 
c  Velocity[Y]                                      0.13026E-03 
c  Velocity[Z]                                      0.42875E-02 
c  Pressure     0.36668E-04     132   0.93369E-02   0.25867E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.60265E-08   0.16440E-08 0.10009E+00 
c  r22          0.10849E-01      13   0.58569E-08   0.18377E-08 0.10202E+00 
c  r33          0.21855E-01      15   0.58643E-08   0.12632E-07 0.12807E+00 
c  r12          0.93833E-03      18   0.63653E-08   0.29865E-09 0.60615E+00 
c  r13          0.46665E-02      19   0.59725E-08   0.15168E-08 0.20121E+00 
c  r23          0.39965E-02      20   0.54675E-08   0.12960E-08 0.19960E+00 
c  epsilon      0.10972E+02      11   0.34055E-08   0.10064E-01 0.16595E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.84768E-02 0.43408E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161986


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61362       0.0052521       0.0015067
v  Velocity[Y]            -0.57392         0.54429       0.0030772      0.00087306
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.501             360          87.636          169.82
v  r11                   0.0010587        0.081874        0.013067        0.018283
v  r22                   0.0011089        0.082615        0.013347        0.018643
v  r33                   0.0016327         0.17434        0.027236          0.0372
v  r12                   -0.010646        0.013611     -0.00023367     -0.00030924
v  r13                   -0.045555        0.052788      9.2463e-05       0.0010134
v  r23                   -0.046695        0.051186       2.989e-05      0.00057425
v  epsilon                 0.06855          271.24          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9897e-05       0.0099175      0.00092408       0.0017423
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2779         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71347         0.85282


 TIME FOR THE TIME STEP             9888:        0.81146E+02

===============================================================


 INSTANT    0.988900000E-02   TIME STEP NUMBER            9889
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.199711158E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.224270822E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.253120464E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.422661319E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.134707747E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81273E-03   0.45483E-02 0.19965E+01 
c  Velocity[X]                                      0.13886E-03 
c  Velocity[Y]                                      0.13006E-03 
c  Velocity[Z]                                      0.42794E-02 
c  Pressure     0.36166E-04     133   0.92148E-02   0.25511E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.53860E-08   0.16247E-08 0.99664E-01 
c  r22          0.10849E-01      13   0.55765E-08   0.18208E-08 0.10150E+00 
c  r33          0.21855E-01      14   0.69974E-08   0.12408E-07 0.12704E+00 
c  r12          0.93833E-03      18   0.61574E-08   0.29459E-09 0.60394E+00 
c  r13          0.46665E-02      19   0.57086E-08   0.14792E-08 0.19924E+00 
c  r23          0.39965E-02      19   0.68284E-08   0.12667E-08 0.19777E+00 
c  epsilon      0.10972E+02      11   0.33062E-08   0.98473E-02 0.16568E+00 
c  TempC        0.25716E+06      16   0.15118E-04   0.84234E-02 0.43316E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161983


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379         0.61359        0.005252       0.0015067
v  Velocity[Y]            -0.57383          0.5441       0.0030771      0.00087302
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                 -36.45          360.08          87.657          169.88
v  r11                   0.0010587        0.081873        0.013067        0.018283
v  r22                   0.0011089        0.082616        0.013347        0.018643
v  r33                   0.0016327          0.1743        0.027236          0.0372
v  r12                   -0.010644        0.013612     -0.00023367     -0.00030924
v  r13                   -0.045559        0.052788      9.2464e-05       0.0010134
v  r23                   -0.046696        0.051206      2.9891e-05      0.00057425
v  epsilon                0.068551          271.22          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9899e-05       0.0099175      0.00092408       0.0017423
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2778         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71347         0.85282


 TIME FOR THE TIME STEP             9889:        0.80368E+02

===============================================================


 INSTANT    0.989000000E-02   TIME STEP NUMBER            9890
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.498680930E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182573861E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934890E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.547237182E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.635451338E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934912E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.185802535E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81153E-03   0.45636E-02 0.20015E+01 
c  Velocity[X]                                      0.14062E-03 
c  Velocity[Y]                                      0.13001E-03 
c  Velocity[Z]                                      0.42930E-02 
c  Pressure     0.36591E-04     132   0.93169E-02   0.25812E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.52438E-08   0.16386E-08 0.10015E+00 
c  r22          0.10849E-01      13   0.55056E-08   0.18288E-08 0.10188E+00 
c  r33          0.21855E-01      15   0.66631E-08   0.12475E-07 0.12761E+00 
c  r12          0.93833E-03      18   0.65799E-08   0.29762E-09 0.60436E+00 
c  r13          0.46665E-02      19   0.62714E-08   0.14862E-08 0.19970E+00 
c  r23          0.39965E-02      19   0.62381E-08   0.12850E-08 0.19960E+00 
c  epsilon      0.10972E+02      11   0.33546E-08   0.98353E-02 0.16487E+00 
c  TempC        0.25716E+06      16   0.15121E-04   0.84437E-02 0.43307E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61362       0.0052521       0.0015067
v  Velocity[Y]            -0.57386         0.54419       0.0030771      0.00087307
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.471          360.03            87.7          169.88
v  r11                   0.0010587        0.081881        0.013067        0.018283
v  r22                   0.0011089        0.082617        0.013347        0.018643
v  r33                   0.0016327         0.17431        0.027236          0.0372
v  r12                    -0.01065         0.01361     -0.00023367     -0.00030924
v  r13                   -0.045556        0.052788      9.2466e-05       0.0010134
v  r23                   -0.046697        0.051203      2.9892e-05      0.00057426
v  epsilon                0.068551          271.21          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9901e-05       0.0099174      0.00092408       0.0017423
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2782         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71347         0.85282


 TIME FOR THE TIME STEP             9890:        0.78804E+02

===============================================================


 INSTANT    0.989100000E-02   TIME STEP NUMBER            9891
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.550197868E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130021514E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.367688343E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.187730038E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.349610319E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81197E-03   0.45507E-02 0.20010E+01 
c  Velocity[X]                                      0.14093E-03 
c  Velocity[Y]                                      0.13035E-03 
c  Velocity[Z]                                      0.42794E-02 
c  Pressure     0.36505E-04     132   0.92997E-02   0.25750E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.51650E-08   0.16485E-08 0.10058E+00 
c  r22          0.10849E-01      13   0.56204E-08   0.18404E-08 0.10246E+00 
c  r33          0.21855E-01      15   0.63176E-08   0.12537E-07 0.12829E+00 
c  r12          0.93833E-03      18   0.63303E-08   0.29862E-09 0.60584E+00 
c  r13          0.46665E-02      19   0.72777E-08   0.14987E-08 0.20180E+00 
c  r23          0.39965E-02      19   0.65929E-08   0.12755E-08 0.19972E+00 
c  epsilon      0.10972E+02      11   0.34517E-08   0.97593E-02 0.16449E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.84589E-02 0.43394E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61361       0.0052521       0.0015067
v  Velocity[Y]            -0.57388         0.54438       0.0030771      0.00087304
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.409          360.04          87.656          169.87
v  r11                   0.0010587        0.081888        0.013067        0.018283
v  r22                   0.0011089        0.082618        0.013347        0.018643
v  r33                   0.0016327         0.17434        0.027236          0.0372
v  r12                    -0.01065        0.013612     -0.00023367     -0.00030924
v  r13                   -0.045555        0.052788      9.2468e-05       0.0010134
v  r23                   -0.046699        0.051185      2.9893e-05      0.00057426
v  epsilon                0.068551          271.24          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9902e-05       0.0099174      0.00092408       0.0017423
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017896           5.279         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71347         0.85282


 TIME FOR THE TIME STEP             9891:        0.80056E+02

===============================================================


 INSTANT    0.989200000E-02   TIME STEP NUMBER            9892
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.402530840E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.288612349E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934900E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.231558266E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161505781E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.109827514E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81204E-03   0.45383E-02 0.19956E+01 
c  Velocity[X]                                      0.13885E-03 
c  Velocity[Y]                                      0.12952E-03 
c  Velocity[Z]                                      0.42699E-02 
c  Pressure     0.36298E-04     134   0.92348E-02   0.25605E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.51075E-08   0.16717E-08 0.10164E+00 
c  r22          0.10849E-01      13   0.53615E-08   0.18365E-08 0.10258E+00 
c  r33          0.21855E-01      15   0.53940E-08   0.12661E-07 0.12925E+00 
c  r12          0.93833E-03      18   0.53670E-08   0.30130E-09 0.61014E+00 
c  r13          0.46665E-02      19   0.68458E-08   0.14994E-08 0.20172E+00 
c  r23          0.39965E-02      19   0.68260E-08   0.12946E-08 0.20212E+00 
c  epsilon      0.10972E+02      11   0.34920E-08   0.10180E-01 0.17105E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.83827E-02 0.43249E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61358        0.005252       0.0015067
v  Velocity[Y]            -0.57381          0.5442       0.0030771      0.00087299
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.424          360.08            87.7          169.91
v  r11                   0.0010587        0.081895        0.013067        0.018283
v  r22                   0.0011089        0.082619        0.013347        0.018643
v  r33                   0.0016327         0.17432        0.027236          0.0372
v  r12                    -0.01065        0.013609     -0.00023367     -0.00030924
v  r13                   -0.045557        0.052791       9.247e-05       0.0010134
v  r23                     -0.0467        0.051203      2.9894e-05      0.00057426
v  epsilon                0.068552          271.26          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9901e-05       0.0099176      0.00092408       0.0017423
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2796         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8796         0.71347         0.85282


 TIME FOR THE TIME STEP             9892:        0.78727E+02

===============================================================


 INSTANT    0.989300000E-02   TIME STEP NUMBER            9893
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.347309021E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33841E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.410924132E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33841E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.378293215E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33841E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.554648163E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33841E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.413033037E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33841E+00
   Friction velocity        uk    :  0.11552E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81173E-03   0.45486E-02 0.19977E+01 
c  Velocity[X]                                      0.13974E-03 
c  Velocity[Y]                                      0.13065E-03 
c  Velocity[Z]                                      0.42782E-02 
c  Pressure     0.36558E-04     133   0.93069E-02   0.25788E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.54450E-08   0.16502E-08 0.10066E+00 
c  r22          0.10849E-01      13   0.53680E-08   0.18280E-08 0.10236E+00 
c  r33          0.21855E-01      15   0.56849E-08   0.12549E-07 0.12831E+00 
c  r12          0.93834E-03      18   0.51560E-08   0.30368E-09 0.61191E+00 
c  r13          0.46665E-02      19   0.64684E-08   0.14672E-08 0.19967E+00 
c  r23          0.39965E-02      19   0.66359E-08   0.12929E-08 0.20089E+00 
c  epsilon      0.10972E+02      11   0.33809E-08   0.96639E-02 0.16374E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.84501E-02 0.43399E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393         0.61363        0.005252       0.0015067
v  Velocity[Y]            -0.57387         0.54416       0.0030771        0.000873
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                 -36.42          360.03          87.658          169.86
v  r11                   0.0010587        0.081899        0.013067        0.018283
v  r22                   0.0011089         0.08262        0.013347        0.018643
v  r33                   0.0016327          0.1743        0.027236          0.0372
v  r12                   -0.010647        0.013613     -0.00023367     -0.00030924
v  r13                   -0.045557         0.05279      9.2471e-05       0.0010134
v  r23                   -0.046701        0.051195      2.9894e-05      0.00057426
v  epsilon                0.068552          271.22          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc               5.99e-05       0.0099177      0.00092408       0.0017423
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2799         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8799         0.71347         0.85282


 TIME FOR THE TIME STEP             9893:        0.80878E+02

===============================================================


 INSTANT    0.989400000E-02   TIME STEP NUMBER            9894
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.506754672E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.205268471E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.612998307E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.220900894E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.197200407E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81176E-03   0.45668E-02 0.20015E+01 
c  Velocity[X]                                      0.14029E-03 
c  Velocity[Y]                                      0.13034E-03 
c  Velocity[Z]                                      0.42962E-02 
c  Pressure     0.36630E-04     132   0.93188E-02   0.25839E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.54631E-08   0.16627E-08 0.10116E+00 
c  r22          0.10849E-01      13   0.53166E-08   0.18433E-08 0.10249E+00 
c  r33          0.21855E-01      15   0.60139E-08   0.12640E-07 0.12875E+00 
c  r12          0.93834E-03      18   0.58170E-08   0.30459E-09 0.61345E+00 
c  r13          0.46665E-02      19   0.66579E-08   0.14904E-08 0.20104E+00 
c  r23          0.39965E-02      19   0.66669E-08   0.12911E-08 0.20138E+00 
c  epsilon      0.10972E+02      11   0.36012E-08   0.99497E-02 0.16540E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.84613E-02 0.43361E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63395          0.6136       0.0052521       0.0015067
v  Velocity[Y]            -0.57383         0.54425       0.0030771      0.00087298
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.441          360.12          87.734          169.94
v  r11                   0.0010587        0.081899        0.013067        0.018283
v  r22                   0.0011089         0.08262        0.013347        0.018643
v  r33                   0.0016327         0.17433        0.027236          0.0372
v  r12                   -0.010646        0.013614     -0.00023367     -0.00030924
v  r13                   -0.045555        0.052791      9.2472e-05       0.0010134
v  r23                   -0.046703        0.051179      2.9896e-05      0.00057426
v  epsilon                0.068552          271.23          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9898e-05       0.0099178      0.00092409       0.0017423
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2798         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8798         0.71347         0.85282


 TIME FOR THE TIME STEP             9894:        0.80871E+02

===============================================================


 INSTANT    0.989500000E-02   TIME STEP NUMBER            9895
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.244799149E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.124499356E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.272338622E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.909296367E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.140065683E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81147E-03   0.45310E-02 0.19937E+01 
c  Velocity[X]                                      0.13888E-03 
c  Velocity[Y]                                      0.12950E-03 
c  Velocity[Z]                                      0.42626E-02 
c  Pressure     0.36596E-04     131   0.93237E-02   0.25814E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.54421E-08   0.16812E-08 0.10112E+00 
c  r22          0.10849E-01      13   0.51859E-08   0.18295E-08 0.10209E+00 
c  r33          0.21855E-01      15   0.60315E-08   0.12666E-07 0.12820E+00 
c  r12          0.93834E-03      18   0.52421E-08   0.30516E-09 0.61044E+00 
c  r13          0.46665E-02      19   0.64999E-08   0.14942E-08 0.20056E+00 
c  r23          0.39965E-02      19   0.68651E-08   0.13068E-08 0.20087E+00 
c  epsilon      0.10972E+02      11   0.36200E-08   0.99724E-02 0.16562E+00 
c  TempC        0.25716E+06      16   0.15096E-04   0.84510E-02 0.43336E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61359        0.005252       0.0015067
v  Velocity[Y]            -0.57387         0.54434       0.0030771      0.00087296
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.445          360.04          87.661          169.87
v  r11                   0.0010588        0.081894        0.013067        0.018283
v  r22                    0.001109        0.082619        0.013347        0.018643
v  r33                   0.0016327         0.17435        0.027236          0.0372
v  r12                   -0.010646        0.013616     -0.00023368     -0.00030924
v  r13                   -0.045558        0.052789      9.2474e-05       0.0010134
v  r23                   -0.046704        0.051206      2.9896e-05      0.00057426
v  epsilon                0.068553          271.27          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9895e-05       0.0099181      0.00092409       0.0017423
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2796         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8796         0.71348         0.85282


 TIME FOR THE TIME STEP             9895:        0.80249E+02

===============================================================


 INSTANT    0.989600000E-02   TIME STEP NUMBER            9896
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.291323978E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.668247976E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.137019705E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.157492141E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.147841943E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81191E-03   0.45824E-02 0.20039E+01 
c  Velocity[X]                                      0.13974E-03 
c  Velocity[Y]                                      0.12986E-03 
c  Velocity[Z]                                      0.43128E-02 
c  Pressure     0.36671E-04     132   0.93332E-02   0.25870E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.55744E-08   0.16430E-08 0.10042E+00 
c  r22          0.10849E-01      13   0.51705E-08   0.18142E-08 0.10186E+00 
c  r33          0.21855E-01      15   0.63199E-08   0.12388E-07 0.12780E+00 
c  r12          0.93834E-03      18   0.58731E-08   0.29137E-09 0.60066E+00 
c  r13          0.46665E-02      19   0.58256E-08   0.14710E-08 0.19989E+00 
c  r23          0.39965E-02      19   0.62874E-08   0.12669E-08 0.19886E+00 
c  epsilon      0.10972E+02      11   0.35466E-08   0.96696E-02 0.16278E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.84468E-02 0.43432E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61359        0.005252       0.0015067
v  Velocity[Y]            -0.57378         0.54414       0.0030771      0.00087297
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.496          360.03          87.669          169.86
v  r11                   0.0010588        0.081893        0.013067        0.018283
v  r22                    0.001109        0.082619        0.013347        0.018643
v  r33                   0.0016327         0.17434        0.027236          0.0372
v  r12                   -0.010643        0.013611     -0.00023368     -0.00030924
v  r13                   -0.045555        0.052791      9.2475e-05       0.0010134
v  r23                   -0.046705        0.051194      2.9897e-05      0.00057426
v  epsilon                0.068553          271.26          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9889e-05       0.0099183      0.00092409       0.0017423
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2787         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71347         0.85282


 TIME FOR THE TIME STEP             9896:        0.78905E+02

===============================================================


 INSTANT    0.989700000E-02   TIME STEP NUMBER            9897
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.957698615E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.527776064E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.924405766E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125965184E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.167602727E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81158E-03   0.45667E-02 0.20037E+01 
c  Velocity[X]                                      0.13964E-03 
c  Velocity[Y]                                      0.12970E-03 
c  Velocity[Z]                                      0.42973E-02 
c  Pressure     0.36745E-04     132   0.93551E-02   0.25920E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.57690E-08   0.16560E-08 0.10091E+00 
c  r22          0.10849E-01      13   0.50330E-08   0.18304E-08 0.10248E+00 
c  r33          0.21855E-01      15   0.72295E-08   0.12542E-07 0.12869E+00 
c  r12          0.93834E-03      18   0.56190E-08   0.29693E-09 0.60542E+00 
c  r13          0.46665E-02      20   0.62463E-08   0.15005E-08 0.20211E+00 
c  r23          0.39965E-02      19   0.68233E-08   0.12916E-08 0.20119E+00 
c  epsilon      0.10972E+02      11   0.34437E-08   0.97289E-02 0.16410E+00 
c  TempC        0.25716E+06      16   0.15110E-04   0.84091E-02 0.43300E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379         0.61359       0.0052521       0.0015067
v  Velocity[Y]            -0.57391         0.54413       0.0030771      0.00087298
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.452             360          87.637          169.83
v  r11                   0.0010588        0.081893        0.013067        0.018283
v  r22                    0.001109        0.082615        0.013347        0.018643
v  r33                   0.0016327         0.17432        0.027236          0.0372
v  r12                   -0.010641        0.013613     -0.00023368     -0.00030924
v  r13                   -0.045556        0.052793      9.2477e-05       0.0010134
v  r23                   -0.046706        0.051173      2.9898e-05      0.00057426
v  epsilon                0.068553          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9886e-05       0.0099182      0.00092409       0.0017423
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2782         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71347         0.85282


 TIME FOR THE TIME STEP             9897:        0.81808E+02

===============================================================


 INSTANT    0.989800000E-02   TIME STEP NUMBER            9898
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172516748E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.594170836E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.256863380E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.651669330E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.745229524E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81187E-03   0.45135E-02 0.19912E+01 
c  Velocity[X]                                      0.13924E-03 
c  Velocity[Y]                                      0.12893E-03 
c  Velocity[Z]                                      0.42454E-02 
c  Pressure     0.36702E-04     131   0.93453E-02   0.25891E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.62060E-08   0.16716E-08 0.10140E+00 
c  r22          0.10849E-01      13   0.52092E-08   0.18291E-08 0.10248E+00 
c  r33          0.21855E-01      15   0.58259E-08   0.12636E-07 0.12901E+00 
c  r12          0.93834E-03      18   0.64410E-08   0.30302E-09 0.60993E+00 
c  r13          0.46665E-02      19   0.71325E-08   0.14840E-08 0.20085E+00 
c  r23          0.39965E-02      19   0.70856E-08   0.13188E-08 0.20309E+00 
c  epsilon      0.10972E+02      11   0.33421E-08   0.10107E-01 0.17039E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.84037E-02 0.43240E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61355       0.0052521       0.0015068
v  Velocity[Y]            -0.57396          0.5442       0.0030771      0.00087298
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.469          360.05          87.678          169.88
v  r11                   0.0010588        0.081887        0.013067        0.018283
v  r22                    0.001109        0.082616        0.013347        0.018643
v  r33                   0.0016327         0.17433        0.027236          0.0372
v  r12                   -0.010644        0.013612     -0.00023368     -0.00030924
v  r13                   -0.045558        0.052793      9.2479e-05       0.0010134
v  r23                   -0.046706        0.051158      2.9899e-05      0.00057426
v  epsilon                0.068554          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9882e-05       0.0099182      0.00092409       0.0017423
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2777         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71347         0.85282


 TIME FOR THE TIME STEP             9898:        0.83088E+02

===============================================================


 INSTANT    0.989900000E-02   TIME STEP NUMBER            9899
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182755753E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.534420874E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.653795173E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.275594595E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.170330945E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81209E-03   0.45759E-02 0.20028E+01 
c  Velocity[X]                                      0.13995E-03 
c  Velocity[Y]                                      0.13015E-03 
c  Velocity[Z]                                      0.43058E-02 
c  Pressure     0.36426E-04     132   0.92737E-02   0.25695E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.62171E-08   0.16521E-08 0.10025E+00 
c  r22          0.10849E-01      13   0.52063E-08   0.18300E-08 0.10187E+00 
c  r33          0.21855E-01      15   0.59315E-08   0.12562E-07 0.12753E+00 
c  r12          0.93834E-03      18   0.65436E-08   0.30400E-09 0.60722E+00 
c  r13          0.46665E-02      19   0.64779E-08   0.14899E-08 0.20008E+00 
c  r23          0.39965E-02      19   0.63890E-08   0.12838E-08 0.19919E+00 
c  epsilon      0.10972E+02      11   0.34322E-08   0.10173E-01 0.16690E+00 
c  TempC        0.25716E+06      16   0.15125E-04   0.84799E-02 0.43390E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61359       0.0052521       0.0015068
v  Velocity[Y]            -0.57383         0.54433       0.0030772      0.00087302
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.425             360          87.635          169.84
v  r11                   0.0010588        0.081881        0.013067        0.018283
v  r22                    0.001109        0.082616        0.013347        0.018643
v  r33                   0.0016328         0.17435        0.027236          0.0372
v  r12                   -0.010648        0.013614     -0.00023368     -0.00030924
v  r13                   -0.045555        0.052791       9.248e-05       0.0010134
v  r23                   -0.046707        0.051183        2.99e-05      0.00057426
v  epsilon                0.068554          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9879e-05       0.0099181      0.00092409       0.0017423
v  CourantNb               0.44256             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2779         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71347         0.85282


 TIME FOR THE TIME STEP             9899:        0.81491E+02

===============================================================


 INSTANT    0.990000000E-02   TIME STEP NUMBER            9900
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.108076023E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133538637E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.254463669E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.863547108E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.146589871E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      40   0.81060E-03   0.45645E-02 0.20007E+01 
c  Velocity[X]                                      0.13980E-03 
c  Velocity[Y]                                      0.13017E-03 
c  Velocity[Z]                                      0.42945E-02 
c  Pressure     0.36390E-04     133   0.92634E-02   0.25670E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.60552E-08   0.16509E-08 0.10104E+00 
c  r22          0.10849E-01      13   0.50819E-08   0.18504E-08 0.10284E+00 
c  r33          0.21855E-01      15   0.65308E-08   0.12573E-07 0.12857E+00 
c  r12          0.93834E-03      18   0.70136E-08   0.29798E-09 0.60569E+00 
c  r13          0.46665E-02      19   0.69685E-08   0.15073E-08 0.20114E+00 
c  r23          0.39965E-02      19   0.69412E-08   0.12780E-08 0.20133E+00 
c  epsilon      0.10972E+02      11   0.35410E-08   0.10077E-01 0.16617E+00 
c  TempC        0.25716E+06      16   0.15110E-04   0.84431E-02 0.43379E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61357       0.0052521       0.0015068
v  Velocity[Y]            -0.57391         0.54414       0.0030771      0.00087294
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.428          360.06          87.678          169.89
v  r11                   0.0010588        0.081871        0.013067        0.018283
v  r22                    0.001109        0.082617        0.013347        0.018643
v  r33                   0.0016328         0.17434        0.027236          0.0372
v  r12                    -0.01065         0.01361     -0.00023368     -0.00030924
v  r13                   -0.045554         0.05279      9.2482e-05       0.0010134
v  r23                   -0.046707        0.051169      2.9902e-05      0.00057426
v  epsilon                0.068554          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9876e-05        0.009918      0.00092409       0.0017423
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2779         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71347         0.85282


 TIME FOR THE TIME STEP             9900:        0.82276E+02

===============================================================


 INSTANT    0.990100000E-02   TIME STEP NUMBER            9901
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.482561656E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.100504586E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934906E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.256076575E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.741880399E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.594780961E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81245E-03   0.45318E-02 0.19952E+01 
c  Velocity[X]                                      0.13855E-03 
c  Velocity[Y]                                      0.12999E-03 
c  Velocity[Z]                                      0.42632E-02 
c  Pressure     0.36440E-04     132   0.92747E-02   0.25704E-01 0.00000E+00 
c  r11          0.10582E-01      13   0.63831E-08   0.16441E-08 0.10058E+00 
c  r22          0.10849E-01      13   0.55411E-08   0.18118E-08 0.10197E+00 
c  r33          0.21855E-01      15   0.60636E-08   0.12483E-07 0.12775E+00 
c  r12          0.93834E-03      18   0.64223E-08   0.29801E-09 0.60780E+00 
c  r13          0.46665E-02      19   0.72724E-08   0.14823E-08 0.20002E+00 
c  r23          0.39965E-02      19   0.74155E-08   0.12860E-08 0.20064E+00 
c  epsilon      0.10972E+02      11   0.34480E-08   0.10013E-01 0.16737E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.83820E-02 0.43243E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61355       0.0052522       0.0015068
v  Velocity[Y]            -0.57367         0.54421       0.0030771      0.00087295
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.395           360.1          87.707          169.92
v  r11                   0.0010588        0.081859        0.013067        0.018283
v  r22                    0.001109        0.082617        0.013347        0.018643
v  r33                   0.0016328         0.17431        0.027236          0.0372
v  r12                   -0.010653        0.013611     -0.00023368     -0.00030924
v  r13                   -0.045558        0.052791      9.2484e-05       0.0010134
v  r23                   -0.046707        0.051163      2.9903e-05      0.00057426
v  epsilon                0.068554          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9874e-05        0.009918       0.0009241       0.0017423
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2775         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71347         0.85282


 TIME FOR THE TIME STEP             9901:        0.78804E+02

===============================================================


 INSTANT    0.990200000E-02   TIME STEP NUMBER            9902
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.421648799E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.926402498E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232907740E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.264985869E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.786312170E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81141E-03   0.45618E-02 0.20012E+01 
c  Velocity[X]                                      0.14052E-03 
c  Velocity[Y]                                      0.13016E-03 
c  Velocity[Z]                                      0.42911E-02 
c  Pressure     0.36625E-04     132   0.93248E-02   0.25836E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60043E-08   0.16447E-08 0.10057E+00 
c  r22          0.10849E-01      13   0.53721E-08   0.18305E-08 0.10235E+00 
c  r33          0.21855E-01      15   0.54020E-08   0.12515E-07 0.12810E+00 
c  r12          0.93834E-03      18   0.64476E-08   0.29110E-09 0.60261E+00 
c  r13          0.46665E-02      19   0.66513E-08   0.14909E-08 0.20058E+00 
c  r23          0.39965E-02      20   0.60166E-08   0.12833E-08 0.20077E+00 
c  epsilon      0.10972E+02      11   0.33935E-08   0.10024E-01 0.16693E+00 
c  TempC        0.25716E+06      16   0.15114E-04   0.84202E-02 0.43309E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63405         0.61359       0.0052521       0.0015068
v  Velocity[Y]            -0.57365         0.54438       0.0030771      0.00087295
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.459          360.06          87.703           169.9
v  r11                   0.0010588        0.081865        0.013067        0.018283
v  r22                    0.001109        0.082618        0.013347        0.018643
v  r33                   0.0016328         0.17433        0.027236          0.0372
v  r12                   -0.010657        0.013605     -0.00023368     -0.00030924
v  r13                   -0.045555        0.052793      9.2486e-05       0.0010134
v  r23                   -0.046707        0.051188      2.9904e-05      0.00057426
v  epsilon                0.068555          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9871e-05       0.0099179       0.0009241       0.0017423
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2773         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71347         0.85282


 TIME FOR THE TIME STEP             9902:        0.82443E+02

===============================================================


 INSTANT    0.990300000E-02   TIME STEP NUMBER            9903
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.504816973E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.658757685E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117196773E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.228832225E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.232776331E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81184E-03   0.45661E-02 0.20008E+01 
c  Velocity[X]                                      0.14089E-03 
c  Velocity[Y]                                      0.12994E-03 
c  Velocity[Z]                                      0.42953E-02 
c  Pressure     0.36091E-04     132   0.91955E-02   0.25458E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59393E-08   0.16326E-08 0.10004E+00 
c  r22          0.10849E-01      13   0.51946E-08   0.18142E-08 0.10181E+00 
c  r33          0.21855E-01      14   0.70524E-08   0.12428E-07 0.12769E+00 
c  r12          0.93834E-03      18   0.61436E-08   0.29848E-09 0.60680E+00 
c  r13          0.46665E-02      19   0.72273E-08   0.14875E-08 0.20036E+00 
c  r23          0.39965E-02      20   0.64245E-08   0.12805E-08 0.20041E+00 
c  epsilon      0.10972E+02      11   0.33122E-08   0.99134E-02 0.16513E+00 
c  TempC        0.25716E+06      16   0.15088E-04   0.85859E-02 0.43684E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61355       0.0052521       0.0015067
v  Velocity[Y]            -0.57357         0.54411        0.003077      0.00087293
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.405          360.02          87.649          169.86
v  r11                   0.0010588        0.081871        0.013067        0.018283
v  r22                    0.001109        0.082618        0.013347        0.018643
v  r33                   0.0016328         0.17436        0.027236          0.0372
v  r12                    -0.01066        0.013604     -0.00023368     -0.00030924
v  r13                   -0.045554         0.05279      9.2488e-05       0.0010134
v  r23                   -0.046707        0.051179      2.9905e-05      0.00057426
v  epsilon                0.068555           271.3          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.987e-05       0.0099179       0.0009241       0.0017423
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2779         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71347         0.85282


 TIME FOR THE TIME STEP             9903:        0.81624E+02

===============================================================


 INSTANT    0.990400000E-02   TIME STEP NUMBER            9904
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115475876E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33841E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.181459487E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934908E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33841E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119666472E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33841E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.160632167E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33841E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.789541142E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33841E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81197E-03   0.45091E-02 0.19893E+01 
c  Velocity[X]                                      0.13968E-03 
c  Velocity[Y]                                      0.12956E-03 
c  Velocity[Z]                                      0.42399E-02 
c  Pressure     0.36525E-04     132   0.92956E-02   0.25765E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.61163E-08   0.16734E-08 0.10129E+00 
c  r22          0.10849E-01      13   0.51716E-08   0.18416E-08 0.10206E+00 
c  r33          0.21855E-01      15   0.54211E-08   0.12774E-07 0.12924E+00 
c  r12          0.93834E-03      18   0.59672E-08   0.30274E-09 0.60938E+00 
c  r13          0.46665E-02      19   0.68105E-08   0.15232E-08 0.20163E+00 
c  r23          0.39965E-02      20   0.58919E-08   0.13216E-08 0.20420E+00 
c  epsilon      0.10972E+02      11   0.33639E-08   0.10520E-01 0.17290E+00 
c  TempC        0.25716E+06      16   0.15178E-04   0.84368E-02 0.43345E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63401          0.6136       0.0052521       0.0015067
v  Velocity[Y]            -0.57358         0.54414       0.0030771      0.00087294
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.442          360.06          87.689           169.9
v  r11                   0.0010589        0.081874        0.013067        0.018283
v  r22                    0.001109        0.082618        0.013347        0.018643
v  r33                   0.0016328         0.17434        0.027236          0.0372
v  r12                   -0.010664          0.0136     -0.00023368     -0.00030924
v  r13                   -0.045557        0.052791       9.249e-05       0.0010134
v  r23                   -0.046708        0.051154      2.9905e-05      0.00057426
v  epsilon                0.068555          271.31          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9866e-05       0.0099179       0.0009241       0.0017423
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2779         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71347         0.85282


 TIME FOR THE TIME STEP             9904:        0.80851E+02

===============================================================


 INSTANT    0.990500000E-02   TIME STEP NUMBER            9905
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.236230532E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.322831959E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.274304862E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.998961905E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.454462533E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81102E-03   0.45566E-02 0.19996E+01 
c  Velocity[X]                                      0.13852E-03 
c  Velocity[Y]                                      0.13009E-03 
c  Velocity[Z]                                      0.42880E-02 
c  Pressure     0.35955E-04     136   0.91552E-02   0.25363E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.61766E-08   0.16227E-08 0.99740E-01 
c  r22          0.10849E-01      13   0.51625E-08   0.18375E-08 0.10204E+00 
c  r33          0.21855E-01      15   0.53035E-08   0.12488E-07 0.12752E+00 
c  r12          0.93834E-03      18   0.62746E-08   0.29731E-09 0.60809E+00 
c  r13          0.46665E-02      19   0.73589E-08   0.14912E-08 0.19951E+00 
c  r23          0.39965E-02      20   0.56165E-08   0.12700E-08 0.19884E+00 
c  epsilon      0.10972E+02      11   0.34061E-08   0.98438E-02 0.16402E+00 
c  TempC        0.25716E+06      16   0.15114E-04   0.83742E-02 0.43166E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -0.634         0.61359       0.0052521       0.0015067
v  Velocity[Y]            -0.57359         0.54429       0.0030771      0.00087294
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.482          360.05           87.67          169.88
v  r11                   0.0010589        0.081872        0.013067        0.018283
v  r22                    0.001109        0.082617        0.013347        0.018643
v  r33                   0.0016328          0.1743        0.027236          0.0372
v  r12                   -0.010665        0.013601     -0.00023368     -0.00030924
v  r13                   -0.045555        0.052788      9.2492e-05       0.0010134
v  r23                   -0.046708        0.051173      2.9907e-05      0.00057426
v  epsilon                0.068556          271.27          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9865e-05       0.0099179       0.0009241       0.0017423
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2785         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71347         0.85282


 TIME FOR THE TIME STEP             9905:        0.80001E+02

===============================================================


 INSTANT    0.990600000E-02   TIME STEP NUMBER            9906
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.926889997E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.156880747E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.102368045E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.148898134E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.181118398E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81181E-03   0.45502E-02 0.20005E+01 
c  Velocity[X]                                      0.14041E-03 
c  Velocity[Y]                                      0.13060E-03 
c  Velocity[Z]                                      0.42792E-02 
c  Pressure     0.36367E-04     131   0.92650E-02   0.25653E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59178E-08   0.16322E-08 0.99859E-01 
c  r22          0.10849E-01      13   0.52930E-08   0.17992E-08 0.10142E+00 
c  r33          0.21855E-01      15   0.57902E-08   0.12387E-07 0.12701E+00 
c  r12          0.93834E-03      18   0.64803E-08   0.29800E-09 0.60815E+00 
c  r13          0.46665E-02      19   0.66197E-08   0.14768E-08 0.19929E+00 
c  r23          0.39965E-02      20   0.57508E-08   0.12827E-08 0.19934E+00 
c  epsilon      0.10972E+02      11   0.35677E-08   0.97980E-02 0.16415E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.84116E-02 0.43274E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61353       0.0052521       0.0015068
v  Velocity[Y]            -0.57363         0.54437       0.0030771      0.00087294
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.486          359.99          87.647          169.83
v  r11                   0.0010589        0.081873        0.013067        0.018283
v  r22                    0.001109        0.082617        0.013347        0.018643
v  r33                   0.0016328         0.17432        0.027236          0.0372
v  r12                   -0.010665        0.013603     -0.00023368     -0.00030924
v  r13                   -0.045554        0.052789      9.2494e-05       0.0010134
v  r23                   -0.046709         0.05117      2.9908e-05      0.00057427
v  epsilon                0.068556          271.27          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9864e-05       0.0099178       0.0009241       0.0017423
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2788         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71347         0.85282


 TIME FOR THE TIME STEP             9906:        0.78336E+02

===============================================================


 INSTANT    0.990700000E-02   TIME STEP NUMBER            9907
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.537218143E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.189146335E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.362957790E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209598086E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133065092E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      40   0.81159E-03   0.45346E-02 0.19954E+01 
c  Velocity[X]                                      0.13950E-03 
c  Velocity[Y]                                      0.12903E-03 
c  Velocity[Z]                                      0.42661E-02 
c  Pressure     0.36985E-04     132   0.94123E-02   0.26089E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57625E-08   0.16432E-08 0.10019E+00 
c  r22          0.10849E-01      13   0.54636E-08   0.18327E-08 0.10197E+00 
c  r33          0.21855E-01      15   0.57257E-08   0.12490E-07 0.12755E+00 
c  r12          0.93834E-03      18   0.68791E-08   0.29985E-09 0.60627E+00 
c  r13          0.46665E-02      19   0.69739E-08   0.14909E-08 0.19984E+00 
c  r23          0.39965E-02      20   0.60984E-08   0.12865E-08 0.19954E+00 
c  epsilon      0.10972E+02      11   0.35310E-08   0.99794E-02 0.16649E+00 
c  TempC        0.25716E+06      16   0.15083E-04   0.84644E-02 0.43434E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385          0.6136       0.0052521       0.0015068
v  Velocity[Y]            -0.57364         0.54415       0.0030771      0.00087295
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.396          360.02           87.65          169.85
v  r11                   0.0010589        0.081872        0.013067        0.018283
v  r22                    0.001109        0.082616        0.013347        0.018643
v  r33                   0.0016328         0.17434        0.027236          0.0372
v  r12                   -0.010663        0.013598     -0.00023368     -0.00030924
v  r13                   -0.045557        0.052787      9.2496e-05       0.0010134
v  r23                   -0.046709        0.051161      2.9908e-05      0.00057427
v  epsilon                0.068556          271.32          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9863e-05       0.0099177       0.0009241       0.0017423
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2791         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71347         0.85282


 TIME FOR THE TIME STEP             9907:        0.81433E+02

===============================================================


 INSTANT    0.990800000E-02   TIME STEP NUMBER            9908
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.679818788E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.287582703E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934918E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.104717207E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.116940860E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.432542216E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81302E-03   0.45665E-02 0.19984E+01 
c  Velocity[X]                                      0.13945E-03 
c  Velocity[Y]                                      0.12916E-03 
c  Velocity[Z]                                      0.42979E-02 
c  Pressure     0.36356E-04     132   0.92536E-02   0.25647E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.58477E-08   0.16211E-08 0.99721E-01 
c  r22          0.10849E-01      13   0.51003E-08   0.18065E-08 0.10152E+00 
c  r33          0.21855E-01      15   0.55445E-08   0.12341E-07 0.12716E+00 
c  r12          0.93834E-03      18   0.68406E-08   0.29648E-09 0.60410E+00 
c  r13          0.46665E-02      19   0.63596E-08   0.14903E-08 0.19987E+00 
c  r23          0.39966E-02      20   0.55341E-08   0.12727E-08 0.19853E+00 
c  epsilon      0.10972E+02      11   0.35406E-08   0.96892E-02 0.16495E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.84376E-02 0.43334E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393         0.61354       0.0052522       0.0015068
v  Velocity[Y]            -0.57368         0.54426       0.0030771      0.00087296
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.451          360.06          87.698          169.89
v  r11                   0.0010589        0.081871        0.013067        0.018283
v  r22                   0.0011091        0.082615        0.013347        0.018643
v  r33                   0.0016328         0.17433        0.027236          0.0372
v  r12                   -0.010664          0.0136     -0.00023368     -0.00030924
v  r13                   -0.045554        0.052789      9.2497e-05       0.0010134
v  r23                   -0.046709        0.051183      2.9909e-05      0.00057427
v  epsilon                0.068557          271.31          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9862e-05       0.0099176      0.00092411       0.0017423
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2792         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8792         0.71347         0.85282


 TIME FOR THE TIME STEP             9908:        0.82896E+02

===============================================================


 INSTANT    0.990900000E-02   TIME STEP NUMBER            9909
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.427636234E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221733777E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.225496263E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.328527856E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.225250126E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81122E-03   0.45671E-02 0.20016E+01 
c  Velocity[X]                                      0.13974E-03 
c  Velocity[Y]                                      0.12971E-03 
c  Velocity[Z]                                      0.42977E-02 
c  Pressure     0.36592E-04     133   0.93152E-02   0.25812E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59207E-08   0.16430E-08 0.10017E+00 
c  r22          0.10849E-01      13   0.50232E-08   0.18282E-08 0.10224E+00 
c  r33          0.21855E-01      15   0.53060E-08   0.12514E-07 0.12792E+00 
c  r12          0.93834E-03      18   0.69524E-08   0.29957E-09 0.60482E+00 
c  r13          0.46665E-02      19   0.61148E-08   0.14927E-08 0.20051E+00 
c  r23          0.39966E-02      19   0.68665E-08   0.12800E-08 0.19971E+00 
c  epsilon      0.10972E+02      11   0.34118E-08   0.99281E-02 0.16610E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84455E-02 0.43318E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61352       0.0052522       0.0015067
v  Velocity[Y]            -0.57357         0.54444       0.0030771      0.00087296
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.391          360.09          87.691          169.91
v  r11                   0.0010589        0.081875        0.013067        0.018283
v  r22                   0.0011091        0.082615        0.013347        0.018643
v  r33                   0.0016329          0.1743        0.027236          0.0372
v  r12                   -0.010663        0.013596     -0.00023368     -0.00030924
v  r13                   -0.045555         0.05279      9.2499e-05       0.0010134
v  r23                   -0.046709         0.05117       2.991e-05      0.00057427
v  epsilon                0.068557          271.27          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9862e-05       0.0099177      0.00092411       0.0017423
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017897           5.279         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71347         0.85282


 TIME FOR THE TIME STEP             9909:        0.83250E+02

===============================================================


 INSTANT    0.991000000E-02   TIME STEP NUMBER            9910
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.387339568E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136615685E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.274966636E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.274452559E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125573045E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      40   0.81166E-03   0.45225E-02 0.19925E+01 
c  Velocity[X]                                      0.13929E-03 
c  Velocity[Y]                                      0.12965E-03 
c  Velocity[Z]                                      0.42536E-02 
c  Pressure     0.36853E-04     131   0.93861E-02   0.25996E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.63634E-08   0.16305E-08 0.99476E-01 
c  r22          0.10849E-01      13   0.53607E-08   0.18133E-08 0.10154E+00 
c  r33          0.21855E-01      15   0.55040E-08   0.12426E-07 0.12708E+00 
c  r12          0.93834E-03      19   0.57685E-08   0.29516E-09 0.60507E+00 
c  r13          0.46665E-02      20   0.60802E-08   0.14728E-08 0.19906E+00 
c  r23          0.39966E-02      19   0.66697E-08   0.12742E-08 0.19827E+00 
c  epsilon      0.10972E+02      11   0.32235E-08   0.10045E-01 0.16696E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.83789E-02 0.43181E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61357       0.0052522       0.0015068
v  Velocity[Y]            -0.57358         0.54412       0.0030771      0.00087294
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.421          360.07          87.702           169.9
v  r11                   0.0010589        0.081872        0.013067        0.018283
v  r22                   0.0011091        0.082615        0.013347        0.018643
v  r33                   0.0016329         0.17431        0.027236          0.0372
v  r12                   -0.010664        0.013602     -0.00023368     -0.00030924
v  r13                   -0.045557        0.052791      9.2501e-05       0.0010134
v  r23                   -0.046709        0.051157      2.9911e-05      0.00057426
v  epsilon                0.068557          271.28          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9863e-05       0.0099177      0.00092411       0.0017423
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2783         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71347         0.85282


 TIME FOR THE TIME STEP             9910:        0.83473E+02

===============================================================


 INSTANT    0.991100000E-02   TIME STEP NUMBER            9911
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.900845171E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.939587787E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.616748365E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172457282E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283233153E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81123E-03   0.46053E-02 0.20098E+01 
c  Velocity[X]                                      0.14090E-03 
c  Velocity[Y]                                      0.12997E-03 
c  Velocity[Z]                                      0.43344E-02 
c  Pressure     0.36817E-04     133   0.93797E-02   0.25971E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.66554E-08   0.16516E-08 0.10045E+00 
c  r22          0.10850E-01      13   0.52910E-08   0.18432E-08 0.10254E+00 
c  r33          0.21855E-01      15   0.63986E-08   0.12619E-07 0.12842E+00 
c  r12          0.93834E-03      19   0.58539E-08   0.30026E-09 0.60745E+00 
c  r13          0.46665E-02      20   0.70725E-08   0.15087E-08 0.20103E+00 
c  r23          0.39966E-02      19   0.68371E-08   0.13065E-08 0.20147E+00 
c  epsilon      0.10972E+02      11   0.33143E-08   0.10177E-01 0.17101E+00 
c  TempC        0.25716E+06      16   0.15125E-04   0.85276E-02 0.43593E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61357       0.0052522       0.0015067
v  Velocity[Y]            -0.57359         0.54413       0.0030771      0.00087298
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                 -36.42          360.03          87.656          169.86
v  r11                   0.0010589        0.081868        0.013067        0.018283
v  r22                   0.0011091        0.082611        0.013347        0.018643
v  r33                   0.0016329         0.17435        0.027236          0.0372
v  r12                   -0.010663        0.013598     -0.00023368     -0.00030924
v  r13                   -0.045554         0.05279      9.2502e-05       0.0010134
v  r23                   -0.046709        0.051185      2.9912e-05      0.00057427
v  epsilon                0.068558          271.31          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9865e-05       0.0099176      0.00092411       0.0017423
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2773         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71348         0.85282


 TIME FOR THE TIME STEP             9911:        0.84552E+02

===============================================================


 INSTANT    0.991200000E-02   TIME STEP NUMBER            9912
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106211972E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.423277771E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166020283E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.368412670E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.349135027E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81266E-03   0.45430E-02 0.19964E+01 
c  Velocity[X]                                      0.13989E-03 
c  Velocity[Y]                                      0.13001E-03 
c  Velocity[Z]                                      0.42731E-02 
c  Pressure     0.36171E-04     132   0.92086E-02   0.25516E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.62533E-08   0.16586E-08 0.10033E+00 
c  r22          0.10850E-01      13   0.52571E-08   0.18656E-08 0.10261E+00 
c  r33          0.21855E-01      15   0.58238E-08   0.12680E-07 0.12795E+00 
c  r12          0.93834E-03      19   0.57746E-08   0.30100E-09 0.60678E+00 
c  r13          0.46665E-02      20   0.59872E-08   0.15011E-08 0.20052E+00 
c  r23          0.39966E-02      19   0.64940E-08   0.12847E-08 0.19923E+00 
c  epsilon      0.10972E+02      11   0.33906E-08   0.10289E-01 0.16807E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.84632E-02 0.43439E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63395         0.61352       0.0052522       0.0015068
v  Velocity[Y]            -0.57374          0.5443       0.0030772      0.00087298
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.444          359.99          87.648          169.84
v  r11                   0.0010589        0.081865        0.013067        0.018283
v  r22                   0.0011091        0.082612        0.013347        0.018643
v  r33                   0.0016329         0.17434        0.027236          0.0372
v  r12                   -0.010661        0.013598     -0.00023368     -0.00030924
v  r13                   -0.045553         0.05279      9.2504e-05       0.0010134
v  r23                    -0.04671        0.051176      2.9913e-05      0.00057427
v  epsilon                0.068558          271.31          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9864e-05       0.0099176      0.00092411       0.0017423
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2771         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71347         0.85282


 TIME FOR THE TIME STEP             9912:        0.82296E+02

===============================================================


 INSTANT    0.991300000E-02   TIME STEP NUMBER            9913
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.548257244E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.251206637E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145265796E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.117753927E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169981600E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81090E-03   0.45281E-02 0.19935E+01 
c  Velocity[X]                                      0.13854E-03 
c  Velocity[Y]                                      0.12967E-03 
c  Velocity[Z]                                      0.42599E-02 
c  Pressure     0.36695E-04     133   0.93387E-02   0.25884E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60160E-08   0.16298E-08 0.99976E-01 
c  r22          0.10850E-01      13   0.55650E-08   0.18468E-08 0.10163E+00 
c  r33          0.21855E-01      15   0.54045E-08   0.12510E-07 0.12719E+00 
c  r12          0.93834E-03      19   0.57955E-08   0.29756E-09 0.60373E+00 
c  r13          0.46665E-02      19   0.72399E-08   0.15106E-08 0.19976E+00 
c  r23          0.39966E-02      19   0.63349E-08   0.12715E-08 0.19872E+00 
c  epsilon      0.10972E+02      11   0.35527E-08   0.10119E-01 0.16655E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.83772E-02 0.43175E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61356       0.0052522       0.0015067
v  Velocity[Y]            -0.57361         0.54445       0.0030771      0.00087297
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.384          360.05          87.678          169.88
v  r11                    0.001059        0.081861        0.013067        0.018283
v  r22                   0.0011091        0.082613        0.013347        0.018643
v  r33                   0.0016329         0.17431        0.027236          0.0372
v  r12                   -0.010658        0.013599     -0.00023368     -0.00030924
v  r13                   -0.045558        0.052789      9.2507e-05       0.0010134
v  r23                    -0.04671         0.05116      2.9914e-05      0.00057427
v  epsilon                0.068558          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9863e-05       0.0099176      0.00092411       0.0017423
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2773         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71347         0.85282


 TIME FOR THE TIME STEP             9913:        0.81592E+02

===============================================================


 INSTANT    0.991400000E-02   TIME STEP NUMBER            9914
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.175219444E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.148497327E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.268736316E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.349308400E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.168412642E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      46   0.81238E-03   0.45929E-02 0.20078E+01 
c  Velocity[X]                                      0.13950E-03 
c  Velocity[Y]                                      0.13038E-03 
c  Velocity[Z]                                      0.43231E-02 
c  Pressure     0.36985E-04     132   0.94181E-02   0.26090E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55827E-08   0.16282E-08 0.10019E+00 
c  r22          0.10850E-01      13   0.51367E-08   0.18237E-08 0.10225E+00 
c  r33          0.21855E-01      15   0.62648E-08   0.12429E-07 0.12807E+00 
c  r12          0.93834E-03      19   0.54937E-08   0.29774E-09 0.60467E+00 
c  r13          0.46665E-02      19   0.74089E-08   0.14737E-08 0.19969E+00 
c  r23          0.39966E-02      19   0.61437E-08   0.12861E-08 0.20032E+00 
c  epsilon      0.10972E+02      11   0.35925E-08   0.96592E-02 0.16415E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.84460E-02 0.43314E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61353       0.0052522       0.0015068
v  Velocity[Y]            -0.57367         0.54411       0.0030772      0.00087299
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.451          360.07          87.708          169.91
v  r11                    0.001059        0.081862        0.013067        0.018283
v  r22                   0.0011091        0.082614        0.013347        0.018643
v  r33                   0.0016329         0.17432        0.027236          0.0372
v  r12                   -0.010659        0.013596     -0.00023368     -0.00030924
v  r13                   -0.045555         0.05279      9.2509e-05       0.0010134
v  r23                    -0.04671         0.05118      2.9914e-05      0.00057427
v  epsilon                0.068559          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9861e-05       0.0099175      0.00092411       0.0017423
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2775         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71348         0.85282


 TIME FOR THE TIME STEP             9914:        0.82296E+02

===============================================================


 INSTANT    0.991500000E-02   TIME STEP NUMBER            9915
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.226659581E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.448800304E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.435565870E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935017E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.343760707E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.398774255E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81107E-03   0.45521E-02 0.19993E+01 
c  Velocity[X]                                      0.14017E-03 
c  Velocity[Y]                                      0.13007E-03 
c  Velocity[Z]                                      0.42819E-02 
c  Pressure     0.36471E-04     133   0.92847E-02   0.25727E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.58112E-08   0.16348E-08 0.10026E+00 
c  r22          0.10850E-01      13   0.49901E-08   0.18570E-08 0.10269E+00 
c  r33          0.21855E-01      15   0.60330E-08   0.12625E-07 0.12863E+00 
c  r12          0.93835E-03      19   0.54100E-08   0.29792E-09 0.60560E+00 
c  r13          0.46665E-02      20   0.58663E-08   0.15076E-08 0.20160E+00 
c  r23          0.39966E-02      19   0.68028E-08   0.12770E-08 0.19980E+00 
c  epsilon      0.10972E+02      11   0.35899E-08   0.10024E-01 0.16688E+00 
c  TempC        0.25716E+06      16   0.15100E-04   0.84978E-02 0.43467E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61352       0.0052522       0.0015068
v  Velocity[Y]            -0.57355         0.54416       0.0030772      0.00087301
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.393             360          87.636          169.84
v  r11                    0.001059        0.081859        0.013067        0.018283
v  r22                   0.0011091        0.082615        0.013347        0.018643
v  r33                   0.0016329         0.17435        0.027236          0.0372
v  r12                   -0.010663        0.013601     -0.00023368     -0.00030924
v  r13                   -0.045554        0.052786       9.251e-05       0.0010134
v  r23                   -0.046709        0.051164      2.9916e-05      0.00057427
v  epsilon                0.068559          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9859e-05       0.0099175      0.00092412       0.0017423
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2779         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71347         0.85282


 TIME FOR THE TIME STEP             9915:        0.83056E+02

===============================================================


 INSTANT    0.991600000E-02   TIME STEP NUMBER            9916
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161833022E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.374304550E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.345796303E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242089639E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181918149E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81190E-03   0.45120E-02 0.19906E+01 
c  Velocity[X]                                      0.13852E-03 
c  Velocity[Y]                                      0.12941E-03 
c  Velocity[Z]                                      0.42440E-02 
c  Pressure     0.36651E-04     133   0.93337E-02   0.25853E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.66722E-08   0.16434E-08 0.10023E+00 
c  r22          0.10850E-01      13   0.55183E-08   0.18388E-08 0.10205E+00 
c  r33          0.21855E-01      15   0.64648E-08   0.12595E-07 0.12770E+00 
c  r12          0.93835E-03      19   0.55716E-08   0.29870E-09 0.60545E+00 
c  r13          0.46665E-02      19   0.69758E-08   0.15038E-08 0.20040E+00 
c  r23          0.39966E-02      19   0.60476E-08   0.12815E-08 0.19927E+00 
c  epsilon      0.10972E+02      11   0.34440E-08   0.10272E-01 0.16845E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84054E-02 0.43357E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61354       0.0052522       0.0015068
v  Velocity[Y]            -0.57369          0.5443       0.0030772      0.00087301
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.445          360.02          87.658          169.86
v  r11                    0.001059         0.08185        0.013067        0.018283
v  r22                   0.0011091        0.082616        0.013347        0.018643
v  r33                   0.0016329         0.17434        0.027237          0.0372
v  r12                   -0.010663        0.013603     -0.00023368     -0.00030924
v  r13                   -0.045557        0.052787      9.2512e-05       0.0010134
v  r23                   -0.046709        0.051162      2.9917e-05      0.00057427
v  epsilon                0.068559          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9857e-05       0.0099177      0.00092412       0.0017423
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2786         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71347         0.85282


 TIME FOR THE TIME STEP             9916:        0.83015E+02

===============================================================


 INSTANT    0.991700000E-02   TIME STEP NUMBER            9917
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.313668186E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.137989834E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934902E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.829438151E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.159179819E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.234148917E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81199E-03   0.46036E-02 0.20081E+01 
c  Velocity[X]                                      0.14044E-03 
c  Velocity[Y]                                      0.13025E-03 
c  Velocity[Z]                                      0.43329E-02 
c  Pressure     0.36631E-04     133   0.93276E-02   0.25840E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.63502E-08   0.16790E-08 0.10149E+00 
c  r22          0.10850E-01      13   0.52552E-08   0.18615E-08 0.10297E+00 
c  r33          0.21855E-01      15   0.56831E-08   0.12872E-07 0.12970E+00 
c  r12          0.93835E-03      18   0.73276E-08   0.30685E-09 0.61224E+00 
c  r13          0.46665E-02      19   0.64224E-08   0.15240E-08 0.20171E+00 
c  r23          0.39966E-02      18   0.69829E-08   0.13180E-08 0.20321E+00 
c  epsilon      0.10972E+02      11   0.34484E-08   0.10459E-01 0.17342E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.83923E-02 0.43289E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61355       0.0052523       0.0015068
v  Velocity[Y]            -0.57364         0.54412       0.0030773      0.00087304
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.448          360.06          87.682          169.89
v  r11                    0.001059        0.081858        0.013067        0.018283
v  r22                   0.0011091        0.082615        0.013347        0.018643
v  r33                   0.0016329         0.17432        0.027237          0.0372
v  r12                   -0.010659        0.013605     -0.00023368     -0.00030924
v  r13                   -0.045556        0.052785      9.2513e-05       0.0010134
v  r23                   -0.046708        0.051185      2.9918e-05      0.00057427
v  epsilon                 0.06856          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9857e-05       0.0099178      0.00092412       0.0017423
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2784         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71347         0.85282


 TIME FOR THE TIME STEP             9917:        0.84281E+02

===============================================================


 INSTANT    0.991800000E-02   TIME STEP NUMBER            9918
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.115343018E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.318165933E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158122729E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155654057E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203529701E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81028E-03   0.45524E-02 0.19994E+01 
c  Velocity[X]                                      0.14016E-03 
c  Velocity[Y]                                      0.12964E-03 
c  Velocity[Z]                                      0.42826E-02 
c  Pressure     0.36288E-04     132   0.92386E-02   0.25597E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.64333E-08   0.16482E-08 0.10093E+00 
c  r22          0.10850E-01      13   0.57559E-08   0.18439E-08 0.10260E+00 
c  r33          0.21855E-01      15   0.56302E-08   0.12620E-07 0.12864E+00 
c  r12          0.93835E-03      19   0.53985E-08   0.29737E-09 0.60724E+00 
c  r13          0.46666E-02      19   0.64980E-08   0.14982E-08 0.20052E+00 
c  r23          0.39966E-02      19   0.61342E-08   0.12886E-08 0.20082E+00 
c  epsilon      0.10972E+02      11   0.33969E-08   0.99983E-02 0.16680E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.85010E-02 0.43410E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61351       0.0052523       0.0015068
v  Velocity[Y]            -0.57353         0.54426       0.0030772      0.00087302
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.471          360.05          87.689          169.88
v  r11                    0.001059        0.081871        0.013067        0.018283
v  r22                   0.0011091        0.082616        0.013347        0.018643
v  r33                   0.0016329         0.17434        0.027237          0.0372
v  r12                   -0.010655        0.013598     -0.00023368     -0.00030924
v  r13                   -0.045554        0.052787      9.2515e-05       0.0010134
v  r23                   -0.046707        0.051175      2.9919e-05      0.00057427
v  epsilon                 0.06856          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9855e-05       0.0099178      0.00092412       0.0017423
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2776         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71347         0.85282


 TIME FOR THE TIME STEP             9918:        0.83358E+02

===============================================================


 INSTANT    0.991900000E-02   TIME STEP NUMBER            9919
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.143065593E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.105824510E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.209496421E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.107642410E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155251776E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81201E-03   0.45419E-02 0.19957E+01 
c  Velocity[X]                                      0.13918E-03 
c  Velocity[Y]                                      0.13030E-03 
c  Velocity[Z]                                      0.42725E-02 
c  Pressure     0.36660E-04     132   0.93301E-02   0.25860E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59125E-08   0.16183E-08 0.99822E-01 
c  r22          0.10850E-01      13   0.52195E-08   0.18375E-08 0.10199E+00 
c  r33          0.21855E-01      15   0.54790E-08   0.12535E-07 0.12783E+00 
c  r12          0.93835E-03      18   0.60398E-08   0.29203E-09 0.60415E+00 
c  r13          0.46666E-02      19   0.62056E-08   0.14999E-08 0.20006E+00 
c  r23          0.39966E-02      19   0.52769E-08   0.12623E-08 0.19870E+00 
c  epsilon      0.10972E+02      11   0.34113E-08   0.98637E-02 0.16408E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.84603E-02 0.43373E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61355       0.0052523       0.0015068
v  Velocity[Y]            -0.57349         0.54425       0.0030773      0.00087305
v  Velocity[Z]              1.5657          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4369          4.3406          4.3632
v  Pressure                -36.386          360.01          87.642          169.84
v  r11                    0.001059        0.081884        0.013067        0.018283
v  r22                   0.0011091        0.082612        0.013347        0.018643
v  r33                    0.001633         0.17435        0.027237          0.0372
v  r12                   -0.010657        0.013599     -0.00023368     -0.00030924
v  r13                   -0.045556        0.052789      9.2517e-05       0.0010134
v  r23                   -0.046706        0.051163      2.9921e-05      0.00057427
v  epsilon                 0.06856          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9854e-05       0.0099179      0.00092412       0.0017423
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2774         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71347         0.85282


 TIME FOR THE TIME STEP             9919:        0.81755E+02

===============================================================


 INSTANT    0.992000000E-02   TIME STEP NUMBER            9920
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.406195829E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229644129E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934904E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.253705908E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.256802072E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.346256299E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81198E-03   0.45766E-02 0.20037E+01 
c  Velocity[X]                                      0.13946E-03 
c  Velocity[Y]                                      0.12919E-03 
c  Velocity[Z]                                      0.43079E-02 
c  Pressure     0.36831E-04     132   0.93789E-02   0.25981E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.62295E-08   0.16475E-08 0.10002E+00 
c  r22          0.10850E-01      13   0.47691E-08   0.18141E-08 0.10161E+00 
c  r33          0.21855E-01      15   0.56151E-08   0.12518E-07 0.12763E+00 
c  r12          0.93835E-03      18   0.59102E-08   0.29003E-09 0.60017E+00 
c  r13          0.46666E-02      19   0.62802E-08   0.14716E-08 0.19893E+00 
c  r23          0.39966E-02      18   0.65392E-08   0.12891E-08 0.19965E+00 
c  epsilon      0.10972E+02      11   0.34994E-08   0.99255E-02 0.16506E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84026E-02 0.43270E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61354       0.0052523       0.0015068
v  Velocity[Y]            -0.57359         0.54431       0.0030772      0.00087299
v  Velocity[Z]              1.5658          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4369          4.3406          4.3632
v  Pressure                -36.468          359.99          87.649          169.84
v  r11                    0.001059        0.081886        0.013067        0.018283
v  r22                   0.0011091        0.082613        0.013347        0.018643
v  r33                    0.001633         0.17434        0.027237          0.0372
v  r12                   -0.010663        0.013595     -0.00023368     -0.00030924
v  r13                   -0.045554         0.05279      9.2519e-05       0.0010134
v  r23                   -0.046706        0.051184      2.9922e-05      0.00057427
v  epsilon                0.068561          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9848e-05        0.009918      0.00092412       0.0017423
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2777         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71347         0.85282


 TIME FOR THE TIME STEP             9920:        0.82867E+02

===============================================================


 INSTANT    0.992100000E-02   TIME STEP NUMBER            9921
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150334491E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.910873001E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.895108500E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.135956683E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.138964921E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81137E-03   0.45594E-02 0.19995E+01 
c  Velocity[X]                                      0.14009E-03 
c  Velocity[Y]                                      0.13024E-03 
c  Velocity[Z]                                      0.42890E-02 
c  Pressure     0.36201E-04     133   0.92157E-02   0.25536E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54603E-08   0.16316E-08 0.99772E-01 
c  r22          0.10850E-01      12   0.65219E-08   0.18327E-08 0.10187E+00 
c  r33          0.21855E-01      14   0.67315E-08   0.12461E-07 0.12737E+00 
c  r12          0.93835E-03      18   0.55168E-08   0.29407E-09 0.60518E+00 
c  r13          0.46666E-02      19   0.62142E-08   0.14969E-08 0.20098E+00 
c  r23          0.39966E-02      19   0.52718E-08   0.12663E-08 0.19885E+00 
c  epsilon      0.10971E+02      11   0.33132E-08   0.99889E-02 0.16577E+00 
c  TempC        0.25716E+06      16   0.15107E-04   0.84414E-02 0.43388E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61352       0.0052523       0.0015068
v  Velocity[Y]            -0.57351          0.5444       0.0030772      0.00087301
v  Velocity[Z]              1.5659          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5797          5.4369          4.3406          4.3632
v  Pressure                -36.387           360.1          87.704          169.93
v  r11                    0.001059        0.081883        0.013067        0.018283
v  r22                   0.0011091        0.082616        0.013347        0.018643
v  r33                    0.001633         0.17433        0.027237          0.0372
v  r12                   -0.010662          0.0136     -0.00023368     -0.00030924
v  r13                   -0.045555        0.052789       9.252e-05       0.0010134
v  r23                   -0.046705        0.051172      2.9923e-05      0.00057427
v  epsilon                0.068561          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9842e-05       0.0099179      0.00092412       0.0017423
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2775         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71347         0.85282


 TIME FOR THE TIME STEP             9921:        0.84760E+02

===============================================================


 INSTANT    0.992200000E-02   TIME STEP NUMBER            9922
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226541003E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.153818010E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.194670574E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.506406511E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125241423E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81133E-03   0.45452E-02 0.19970E+01 
c  Velocity[X]                                      0.13921E-03 
c  Velocity[Y]                                      0.13030E-03 
c  Velocity[Z]                                      0.42757E-02 
c  Pressure     0.36665E-04     132   0.93360E-02   0.25863E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.53646E-08   0.16479E-08 0.10060E+00 
c  r22          0.10850E-01      13   0.48770E-08   0.18220E-08 0.10230E+00 
c  r33          0.21855E-01      14   0.71048E-08   0.12514E-07 0.12811E+00 
c  r12          0.93835E-03      18   0.54389E-08   0.29857E-09 0.60810E+00 
c  r13          0.46666E-02      19   0.67499E-08   0.14782E-08 0.20012E+00 
c  r23          0.39966E-02      19   0.59222E-08   0.12857E-08 0.20104E+00 
c  epsilon      0.10971E+02      11   0.33207E-08   0.97514E-02 0.16430E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84269E-02 0.43322E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63396         0.61357       0.0052523       0.0015068
v  Velocity[Y]            -0.57353         0.54418       0.0030773      0.00087303
v  Velocity[Z]              1.5659          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5797          5.4369          4.3406          4.3632
v  Pressure                -36.456          360.08          87.717          169.92
v  r11                   0.0010591        0.081873        0.013067        0.018283
v  r22                   0.0011091        0.082617        0.013347        0.018643
v  r33                    0.001633         0.17434        0.027237          0.0372
v  r12                   -0.010661        0.013596     -0.00023368     -0.00030924
v  r13                   -0.045557        0.052791      9.2523e-05       0.0010134
v  r23                   -0.046705        0.051161      2.9924e-05      0.00057427
v  epsilon                0.068561          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9837e-05       0.0099179      0.00092413       0.0017423
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2768         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71347         0.85282


 TIME FOR THE TIME STEP             9922:        0.82798E+02

===============================================================


 INSTANT    0.992300000E-02   TIME STEP NUMBER            9923
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199790294E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.316655423E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200377045E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.163628446E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122212543E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69809E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81180E-03   0.45705E-02 0.20021E+01 
c  Velocity[X]                                      0.14014E-03 
c  Velocity[Y]                                      0.13015E-03 
c  Velocity[Z]                                      0.43002E-02 
c  Pressure     0.36628E-04     132   0.93310E-02   0.25839E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52729E-08   0.16280E-08 0.99882E-01 
c  r22          0.10850E-01      13   0.44976E-08   0.18624E-08 0.10252E+00 
c  r33          0.21855E-01      15   0.59888E-08   0.12714E-07 0.12813E+00 
c  r12          0.93835E-03      18   0.53281E-08   0.29108E-09 0.60103E+00 
c  r13          0.46666E-02      19   0.70889E-08   0.15242E-08 0.20198E+00 
c  r23          0.39966E-02      19   0.55734E-08   0.12749E-08 0.19916E+00 
c  epsilon      0.10971E+02      11   0.34756E-08   0.10353E-01 0.16735E+00 
c  TempC        0.25716E+06      16   0.15105E-04   0.85150E-02 0.43560E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61356       0.0052524       0.0015068
v  Velocity[Y]            -0.57347         0.54414       0.0030773      0.00087303
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.426             360          87.649          169.84
v  r11                   0.0010591        0.081859        0.013067        0.018283
v  r22                   0.0011092        0.082618        0.013347        0.018643
v  r33                    0.001633         0.17437        0.027237          0.0372
v  r12                   -0.010662        0.013594     -0.00023368     -0.00030924
v  r13                   -0.045555         0.05279      9.2524e-05       0.0010134
v  r23                   -0.046705        0.051188      2.9925e-05      0.00057427
v  epsilon                0.068562          271.32          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9829e-05       0.0099179      0.00092413       0.0017423
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2764         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8764         0.71347         0.85282


 TIME FOR THE TIME STEP             9923:        0.80271E+02

===============================================================


 INSTANT    0.992400000E-02   TIME STEP NUMBER            9924
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.322514779E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.304274711E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203143810E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183339670E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319598950E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81194E-03   0.45461E-02 0.19957E+01 
c  Velocity[X]                                      0.13918E-03 
c  Velocity[Y]                                      0.13015E-03 
c  Velocity[Z]                                      0.42767E-02 
c  Pressure     0.36484E-04     133   0.92876E-02   0.25737E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52548E-08   0.16922E-08 0.10199E+00 
c  r22          0.10850E-01      13   0.45675E-08   0.18784E-08 0.10288E+00 
c  r33          0.21855E-01      15   0.61889E-08   0.12936E-07 0.12962E+00 
c  r12          0.93835E-03      18   0.52057E-08   0.31153E-09 0.61573E+00 
c  r13          0.46666E-02      19   0.64815E-08   0.15534E-08 0.20273E+00 
c  r23          0.39966E-02      19   0.52284E-08   0.13220E-08 0.20400E+00 
c  epsilon      0.10971E+02      11   0.35385E-08   0.10621E-01 0.17529E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.84654E-02 0.43379E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61352       0.0052524       0.0015068
v  Velocity[Y]            -0.57351         0.54425       0.0030773      0.00087302
v  Velocity[Z]              1.5657          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4369          4.3406          4.3632
v  Pressure                -36.469          360.04          87.659          169.87
v  r11                   0.0010591        0.081852        0.013067        0.018283
v  r22                   0.0011092        0.082619        0.013347        0.018643
v  r33                    0.001633         0.17435        0.027237          0.0372
v  r12                   -0.010661         0.01359     -0.00023368     -0.00030924
v  r13                   -0.045554         0.05279      9.2527e-05       0.0010134
v  r23                   -0.046705        0.051174      2.9927e-05      0.00057427
v  epsilon                0.068562          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9823e-05       0.0099179      0.00092413       0.0017423
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2767         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767         0.71347         0.85282


 TIME FOR THE TIME STEP             9924:        0.81223E+02

===============================================================


 INSTANT    0.992500000E-02   TIME STEP NUMBER            9925
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105382628E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.102456900E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.101724673E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.359110958E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186273962E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81179E-03   0.45499E-02 0.19950E+01 
c  Velocity[X]                                      0.13897E-03 
c  Velocity[Y]                                      0.13025E-03 
c  Velocity[Z]                                      0.42807E-02 
c  Pressure     0.36276E-04     131   0.92377E-02   0.25589E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.51402E-08   0.16431E-08 0.10046E+00 
c  r22          0.10850E-01      13   0.49010E-08   0.18169E-08 0.10199E+00 
c  r33          0.21855E-01      15   0.65230E-08   0.12503E-07 0.12786E+00 
c  r12          0.93835E-03      18   0.52972E-08   0.29643E-09 0.60632E+00 
c  r13          0.46666E-02      19   0.62878E-08   0.14999E-08 0.20049E+00 
c  r23          0.39966E-02      18   0.69998E-08   0.12896E-08 0.19994E+00 
c  epsilon      0.10971E+02      11   0.35212E-08   0.97175E-02 0.16542E+00 
c  TempC        0.25716E+06      16   0.15105E-04   0.83566E-02 0.43140E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391          0.6136       0.0052524       0.0015068
v  Velocity[Y]            -0.57339         0.54436       0.0030773      0.00087301
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.432          360.08          87.683           169.9
v  r11                   0.0010591        0.081844        0.013067        0.018283
v  r22                   0.0011092        0.082621        0.013347        0.018643
v  r33                    0.001633         0.17432        0.027237          0.0372
v  r12                   -0.010658        0.013582     -0.00023368     -0.00030924
v  r13                   -0.045557        0.052792      9.2529e-05       0.0010134
v  r23                   -0.046705        0.051167      2.9928e-05      0.00057427
v  epsilon                0.068562          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9817e-05       0.0099179      0.00092413       0.0017423
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2772         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71347         0.85282


 TIME FOR THE TIME STEP             9925:        0.82122E+02

===============================================================


 INSTANT    0.992600000E-02   TIME STEP NUMBER            9926
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.422697313E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.533428428E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.665515339E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.371408915E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158284318E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81121E-03   0.45536E-02 0.20002E+01 
c  Velocity[X]                                      0.14035E-03 
c  Velocity[Y]                                      0.13016E-03 
c  Velocity[Z]                                      0.42831E-02 
c  Pressure     0.36173E-04     132   0.92032E-02   0.25516E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.53627E-08   0.16588E-08 0.10084E+00 
c  r22          0.10850E-01      13   0.47999E-08   0.18320E-08 0.10239E+00 
c  r33          0.21855E-01      15   0.59071E-08   0.12591E-07 0.12845E+00 
c  r12          0.93835E-03      18   0.51557E-08   0.30110E-09 0.60890E+00 
c  r13          0.46666E-02      19   0.71150E-08   0.14859E-08 0.20034E+00 
c  r23          0.39966E-02      19   0.67238E-08   0.12954E-08 0.20113E+00 
c  epsilon      0.10971E+02      11   0.34519E-08   0.96271E-02 0.16426E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.84130E-02 0.43280E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63396         0.61354       0.0052524       0.0015068
v  Velocity[Y]            -0.57347         0.54419       0.0030773      0.00087301
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.489          359.96          87.646          169.82
v  r11                   0.0010591         0.08184        0.013067        0.018283
v  r22                   0.0011092        0.082623        0.013347        0.018643
v  r33                    0.001633         0.17434        0.027237          0.0372
v  r12                   -0.010658        0.013574     -0.00023368     -0.00030924
v  r13                   -0.045554        0.052795      9.2531e-05       0.0010134
v  r23                   -0.046706        0.051197       2.993e-05      0.00057427
v  epsilon                0.068563           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9814e-05       0.0099179      0.00092413       0.0017423
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2782         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71347         0.85282


 TIME FOR THE TIME STEP             9926:        0.81768E+02

===============================================================


 INSTANT    0.992700000E-02   TIME STEP NUMBER            9927
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.203840438E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.800554470E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.113898626E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138402836E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145584568E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81157E-03   0.45571E-02 0.19997E+01 
c  Velocity[X]                                      0.14004E-03 
c  Velocity[Y]                                      0.12976E-03 
c  Velocity[Z]                                      0.42873E-02 
c  Pressure     0.36471E-04     133   0.92834E-02   0.25728E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55889E-08   0.16780E-08 0.10107E+00 
c  r22          0.10850E-01      13   0.46330E-08   0.18732E-08 0.10267E+00 
c  r33          0.21855E-01      15   0.53273E-08   0.12903E-07 0.12930E+00 
c  r12          0.93835E-03      18   0.57307E-08   0.30359E-09 0.60999E+00 
c  r13          0.46666E-02      19   0.56898E-08   0.15184E-08 0.20137E+00 
c  r23          0.39966E-02      19   0.60625E-08   0.12956E-08 0.20105E+00 
c  epsilon      0.10971E+02      11   0.34479E-08   0.10345E-01 0.17030E+00 
c  TempC        0.25716E+06      16   0.15079E-04   0.85098E-02 0.43539E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61354       0.0052524       0.0015068
v  Velocity[Y]            -0.57339         0.54431       0.0030773      0.00087301
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                 -36.41          360.06          87.665          169.88
v  r11                   0.0010591        0.081838        0.013067        0.018283
v  r22                   0.0011092        0.082626        0.013347        0.018643
v  r33                    0.001633         0.17437        0.027237          0.0372
v  r12                   -0.010659        0.013579     -0.00023368     -0.00030924
v  r13                   -0.045554        0.052796      9.2534e-05       0.0010134
v  r23                   -0.046706        0.051187      2.9931e-05      0.00057427
v  epsilon                0.068563          271.32          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9811e-05       0.0099178      0.00092413       0.0017423
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2784         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71347         0.85282


 TIME FOR THE TIME STEP             9927:        0.82939E+02

===============================================================


 INSTANT    0.992800000E-02   TIME STEP NUMBER            9928
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.673034883E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.770224104E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.197180142E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.271553336E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.745022961E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81188E-03   0.45317E-02 0.19928E+01 
c  Velocity[X]                                      0.13887E-03 
c  Velocity[Y]                                      0.12947E-03 
c  Velocity[Z]                                      0.42633E-02 
c  Pressure     0.36833E-04     132   0.93811E-02   0.25983E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54396E-08   0.16834E-08 0.10163E+00 
c  r22          0.10850E-01      13   0.44823E-08   0.18159E-08 0.10215E+00 
c  r33          0.21855E-01      15   0.65227E-08   0.12669E-07 0.12899E+00 
c  r12          0.93835E-03      18   0.54377E-08   0.30009E-09 0.60855E+00 
c  r13          0.46666E-02      19   0.66694E-08   0.14952E-08 0.20049E+00 
c  r23          0.39966E-02      19   0.57469E-08   0.13119E-08 0.20216E+00 
c  epsilon      0.10971E+02      11   0.34139E-08   0.97173E-02 0.16534E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.84102E-02 0.43304E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61357       0.0052524       0.0015068
v  Velocity[Y]            -0.57348         0.54441       0.0030773      0.00087299
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.465          360.05          87.675          169.88
v  r11                   0.0010591        0.081835        0.013067        0.018283
v  r22                   0.0011092        0.082629        0.013347        0.018643
v  r33                   0.0016331         0.17435        0.027237          0.0372
v  r12                   -0.010657        0.013577     -0.00023368     -0.00030924
v  r13                   -0.045557        0.052798      9.2535e-05       0.0010134
v  r23                   -0.046707        0.051178      2.9932e-05      0.00057427
v  epsilon                0.068563          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9804e-05       0.0099177      0.00092414       0.0017423
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2786         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71348         0.85282


 TIME FOR THE TIME STEP             9928:        0.82416E+02

===============================================================


 INSTANT    0.992900000E-02   TIME STEP NUMBER            9929
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.368028628E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105653555E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.136224362E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.455612987E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.296964191E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      40   0.81183E-03   0.45724E-02 0.20012E+01 
c  Velocity[X]                                      0.13901E-03 
c  Velocity[Y]                                      0.13026E-03 
c  Velocity[Z]                                      0.43032E-02 
c  Pressure     0.36507E-04     133   0.92947E-02   0.25752E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50052E-08   0.16391E-08 0.10051E+00 
c  r22          0.10850E-01      13   0.48164E-08   0.18648E-08 0.10281E+00 
c  r33          0.21855E-01      16   0.57993E-08   0.12631E-07 0.12830E+00 
c  r12          0.93835E-03      18   0.58472E-08   0.29461E-09 0.60366E+00 
c  r13          0.46666E-02      19   0.73693E-08   0.15194E-08 0.20182E+00 
c  r23          0.39966E-02      19   0.59030E-08   0.12778E-08 0.19941E+00 
c  epsilon      0.10971E+02      11   0.35032E-08   0.10054E-01 0.16652E+00 
c  TempC        0.25716E+06      16   0.15142E-04   0.84438E-02 0.43347E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -0.634         0.61355       0.0052524       0.0015068
v  Velocity[Y]            -0.57347         0.54411       0.0030774        0.000873
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.426          360.04          87.666          169.88
v  r11                   0.0010591        0.081828        0.013067        0.018283
v  r22                   0.0011092        0.082626        0.013348        0.018643
v  r33                   0.0016331         0.17432        0.027237          0.0372
v  r12                   -0.010654        0.013582     -0.00023368     -0.00030924
v  r13                   -0.045556        0.052798      9.2538e-05       0.0010134
v  r23                   -0.046708        0.051205      2.9934e-05      0.00057427
v  epsilon                0.068564          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9801e-05       0.0099176      0.00092414       0.0017423
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2782         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71347         0.85282


 TIME FOR THE TIME STEP             9929:        0.80105E+02

===============================================================


 INSTANT    0.993000000E-02   TIME STEP NUMBER            9930
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.264257656E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.382025384E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.521530326E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.165104652E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.455866275E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81170E-03   0.45900E-02 0.20080E+01 
c  Velocity[X]                                      0.13987E-03 
c  Velocity[Y]                                      0.13126E-03 
c  Velocity[Z]                                      0.43189E-02 
c  Pressure     0.36615E-04     131   0.93215E-02   0.25828E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.49266E-08   0.17082E-08 0.10229E+00 
c  r22          0.10850E-01      13   0.49350E-08   0.18991E-08 0.10319E+00 
c  r33          0.21855E-01      14   0.70471E-08   0.13044E-07 0.13000E+00 
c  r12          0.93835E-03      18   0.58192E-08   0.29913E-09 0.60684E+00 
c  r13          0.46666E-02      19   0.61775E-08   0.15419E-08 0.20199E+00 
c  r23          0.39966E-02      19   0.55788E-08   0.13190E-08 0.20306E+00 
c  epsilon      0.10971E+02      11   0.33232E-08   0.10860E-01 0.17550E+00 
c  TempC        0.25716E+06      16   0.15106E-04   0.84717E-02 0.43369E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63403          0.6135       0.0052525       0.0015069
v  Velocity[Y]            -0.57349         0.54415       0.0030773      0.00087294
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.463          360.01          87.688          169.88
v  r11                   0.0010591        0.081831        0.013067        0.018283
v  r22                   0.0011092        0.082628        0.013348        0.018643
v  r33                   0.0016331         0.17434        0.027237          0.0372
v  r12                   -0.010656        0.013589     -0.00023368     -0.00030924
v  r13                   -0.045555        0.052799       9.254e-05       0.0010134
v  r23                   -0.046709        0.051182      2.9935e-05      0.00057427
v  epsilon                0.068564          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9797e-05       0.0099174      0.00092414       0.0017423
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2772         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71347         0.85282


 TIME FOR THE TIME STEP             9930:        0.80481E+02

===============================================================


 INSTANT    0.993100000E-02   TIME STEP NUMBER            9931
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.300317100E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.825065297E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.915718787E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935021E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.260169336E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.146603525E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81195E-03   0.45527E-02 0.19976E+01 
c  Velocity[X]                                      0.13920E-03 
c  Velocity[Y]                                      0.12998E-03 
c  Velocity[Z]                                      0.42835E-02 
c  Pressure     0.36510E-04     133   0.92844E-02   0.25754E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54096E-08   0.16278E-08 0.10004E+00 
c  r22          0.10850E-01      13   0.49785E-08   0.18197E-08 0.10206E+00 
c  r33          0.21855E-01      15   0.52997E-08   0.12422E-07 0.12786E+00 
c  r12          0.93835E-03      18   0.59534E-08   0.29397E-09 0.60549E+00 
c  r13          0.46666E-02      19   0.65987E-08   0.15066E-08 0.20095E+00 
c  r23          0.39966E-02      19   0.57057E-08   0.12805E-08 0.20024E+00 
c  epsilon      0.10971E+02      11   0.32650E-08   0.95810E-02 0.16252E+00 
c  TempC        0.25716E+06      16   0.15098E-04   0.84032E-02 0.43254E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61358       0.0052525       0.0015069
v  Velocity[Y]            -0.57347         0.54427       0.0030773      0.00087296
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.388          360.02          87.649          169.86
v  r11                   0.0010591        0.081825        0.013067        0.018283
v  r22                   0.0011092         0.08263        0.013348        0.018643
v  r33                   0.0016331         0.17436        0.027237          0.0372
v  r12                   -0.010659        0.013594     -0.00023368     -0.00030924
v  r13                   -0.045557          0.0528      9.2542e-05       0.0010134
v  r23                    -0.04671        0.051168      2.9936e-05      0.00057428
v  epsilon                0.068564          271.32          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9791e-05       0.0099175      0.00092414       0.0017423
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2776         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71348         0.85282


 TIME FOR THE TIME STEP             9931:        0.80827E+02

===============================================================


 INSTANT    0.993200000E-02   TIME STEP NUMBER            9932
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.737087849E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221256984E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934901E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.745777038E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.317321843E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.364563820E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81174E-03   0.45466E-02 0.19980E+01 
c  Velocity[X]                                      0.13960E-03 
c  Velocity[Y]                                      0.13016E-03 
c  Velocity[Z]                                      0.42769E-02 
c  Pressure     0.36504E-04     131   0.92937E-02   0.25750E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.53239E-08   0.16363E-08 0.10064E+00 
c  r22          0.10850E-01      13   0.52460E-08   0.18567E-08 0.10279E+00 
c  r33          0.21855E-01      15   0.56670E-08   0.12616E-07 0.12852E+00 
c  r12          0.93835E-03      18   0.69171E-08   0.29655E-09 0.60524E+00 
c  r13          0.46666E-02      19   0.59690E-08   0.15091E-08 0.20133E+00 
c  r23          0.39966E-02      19   0.54984E-08   0.12655E-08 0.19978E+00 
c  epsilon      0.10971E+02      11   0.32480E-08   0.10068E-01 0.16583E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.84319E-02 0.43369E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61356       0.0052525       0.0015068
v  Velocity[Y]            -0.57345         0.54442       0.0030773      0.00087294
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.488          359.98          87.654          169.84
v  r11                   0.0010591        0.081827        0.013067        0.018283
v  r22                   0.0011092        0.082632        0.013348        0.018643
v  r33                   0.0016331         0.17435        0.027237          0.0372
v  r12                   -0.010657        0.013597     -0.00023369     -0.00030924
v  r13                   -0.045554        0.052801      9.2543e-05       0.0010134
v  r23                    -0.04671        0.051194      2.9937e-05      0.00057428
v  epsilon                0.068564           271.3          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9789e-05       0.0099177      0.00092414       0.0017423
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2776         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71347         0.85282


 TIME FOR THE TIME STEP             9932:        0.84736E+02

===============================================================


 INSTANT    0.993300000E-02   TIME STEP NUMBER            9933
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.830288279E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120204744E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.973996551E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153448221E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.441264619E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81209E-03   0.45314E-02 0.19940E+01 
c  Velocity[X]                                      0.14020E-03 
c  Velocity[Y]                                      0.12918E-03 
c  Velocity[Z]                                      0.42620E-02 
c  Pressure     0.36493E-04     132   0.92901E-02   0.25743E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54747E-08   0.16394E-08 0.10091E+00 
c  r22          0.10850E-01      13   0.51891E-08   0.18330E-08 0.10228E+00 
c  r33          0.21855E-01      15   0.65000E-08   0.12522E-07 0.12815E+00 
c  r12          0.93835E-03      18   0.54379E-08   0.30279E-09 0.61022E+00 
c  r13          0.46666E-02      19   0.66462E-08   0.15061E-08 0.20096E+00 
c  r23          0.39966E-02      19   0.55752E-08   0.12769E-08 0.20039E+00 
c  epsilon      0.10971E+02      11   0.34352E-08   0.97133E-02 0.16519E+00 
c  TempC        0.25716E+06      16   0.15089E-04   0.84431E-02 0.43311E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61351       0.0052525       0.0015068
v  Velocity[Y]            -0.57322         0.54409       0.0030772      0.00087292
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                 -36.42          360.08           87.69           169.9
v  r11                   0.0010591        0.081824        0.013067        0.018283
v  r22                   0.0011092        0.082632        0.013348        0.018643
v  r33                   0.0016331         0.17433        0.027237          0.0372
v  r12                   -0.010655         0.01359     -0.00023369     -0.00030924
v  r13                   -0.045555          0.0528      9.2545e-05       0.0010134
v  r23                   -0.046711        0.051184      2.9938e-05      0.00057428
v  epsilon                0.068565          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9786e-05       0.0099179      0.00092414       0.0017423
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017898           5.278         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71347         0.85282


 TIME FOR THE TIME STEP             9933:        0.81093E+02

===============================================================


 INSTANT    0.993400000E-02   TIME STEP NUMBER            9934
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.532096818E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.376445458E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119003906E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935017E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.464007573E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.154539843E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81133E-03   0.45490E-02 0.19954E+01 
c  Velocity[X]                                      0.13926E-03 
c  Velocity[Y]                                      0.12998E-03 
c  Velocity[Z]                                      0.42798E-02 
c  Pressure     0.36701E-04     132   0.93385E-02   0.25889E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57951E-08   0.16359E-08 0.10048E+00 
c  r22          0.10850E-01      13   0.55288E-08   0.18165E-08 0.10209E+00 
c  r33          0.21855E-01      15   0.58834E-08   0.12404E-07 0.12777E+00 
c  r12          0.93835E-03      18   0.64538E-08   0.29540E-09 0.60568E+00 
c  r13          0.46666E-02      19   0.71535E-08   0.14707E-08 0.19944E+00 
c  r23          0.39966E-02      19   0.51776E-08   0.12680E-08 0.20012E+00 
c  epsilon      0.10971E+02      11   0.34918E-08   0.95248E-02 0.16405E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.83810E-02 0.43138E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63404         0.61358       0.0052525       0.0015069
v  Velocity[Y]            -0.57331         0.54409       0.0030773      0.00087294
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.429          360.01           87.64          169.84
v  r11                   0.0010591        0.081822        0.013067        0.018283
v  r22                   0.0011093        0.082632        0.013348        0.018643
v  r33                   0.0016331         0.17433        0.027237          0.0372
v  r12                   -0.010661        0.013586     -0.00023369     -0.00030924
v  r13                   -0.045557        0.052802      9.2547e-05       0.0010134
v  r23                   -0.046711        0.051173      2.9939e-05      0.00057428
v  epsilon                0.068565          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9785e-05        0.009918      0.00092414       0.0017423
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2782         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71347         0.85282


 TIME FOR THE TIME STEP             9934:        0.82447E+02

===============================================================


 INSTANT    0.993500000E-02   TIME STEP NUMBER            9935
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117742073E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.193868195E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934909E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127048635E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.557997729E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.508544958E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81187E-03   0.45777E-02 0.20047E+01 
c  Velocity[X]                                      0.13978E-03 
c  Velocity[Y]                                      0.13027E-03 
c  Velocity[Z]                                      0.43076E-02 
c  Pressure     0.36610E-04     131   0.93174E-02   0.25826E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55501E-08   0.16597E-08 0.10060E+00 
c  r22          0.10850E-01      13   0.50571E-08   0.18796E-08 0.10304E+00 
c  r33          0.21855E-01      15   0.55429E-08   0.12828E-07 0.12900E+00 
c  r12          0.93835E-03      18   0.54034E-08   0.30074E-09 0.60608E+00 
c  r13          0.46666E-02      19   0.52599E-08   0.15285E-08 0.20197E+00 
c  r23          0.39966E-02      19   0.61316E-08   0.13067E-08 0.20086E+00 
c  epsilon      0.10971E+02      11   0.32984E-08   0.10147E-01 0.16765E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.84333E-02 0.43314E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63399         0.61357       0.0052525       0.0015069
v  Velocity[Y]             -0.5733         0.54423       0.0030773      0.00087294
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.393          360.04          87.659          169.86
v  r11                   0.0010591        0.081817        0.013067        0.018283
v  r22                   0.0011093        0.082632        0.013348        0.018643
v  r33                   0.0016331         0.17436        0.027237          0.0372
v  r12                   -0.010665        0.013581     -0.00023369     -0.00030924
v  r13                   -0.045555        0.052803      9.2549e-05       0.0010134
v  r23                   -0.046712          0.0512       2.994e-05      0.00057428
v  epsilon                0.068565           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9784e-05        0.009918      0.00092415       0.0017423
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2776         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71347         0.85282


 TIME FOR THE TIME STEP             9935:        0.81754E+02

===============================================================


 INSTANT    0.993600000E-02   TIME STEP NUMBER            9936
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.558096217E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179067460E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.177635685E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.167146970E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110480087E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81191E-03   0.45424E-02 0.19980E+01 
c  Velocity[X]                                      0.13990E-03 
c  Velocity[Y]                                      0.13084E-03 
c  Velocity[Z]                                      0.42717E-02 
c  Pressure     0.36333E-04     133   0.92539E-02   0.25630E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57871E-08   0.16914E-08 0.10133E+00 
c  r22          0.10850E-01      13   0.50818E-08   0.18861E-08 0.10273E+00 
c  r33          0.21855E-01      15   0.59812E-08   0.13040E-07 0.12973E+00 
c  r12          0.93835E-03      18   0.51788E-08   0.29985E-09 0.60621E+00 
c  r13          0.46666E-02      19   0.53302E-08   0.15499E-08 0.20269E+00 
c  r23          0.39966E-02      19   0.60855E-08   0.13274E-08 0.20305E+00 
c  epsilon      0.10971E+02      11   0.35445E-08   0.10884E-01 0.17527E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.85120E-02 0.43572E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63401          0.6135       0.0052526       0.0015069
v  Velocity[Y]            -0.57336         0.54437       0.0030773      0.00087293
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.432          360.07           87.69          169.89
v  r11                   0.0010592         0.08182        0.013068        0.018283
v  r22                   0.0011093        0.082634        0.013348        0.018643
v  r33                   0.0016331         0.17435        0.027237          0.0372
v  r12                   -0.010663        0.013578     -0.00023369     -0.00030924
v  r13                   -0.045553        0.052804      9.2552e-05       0.0010134
v  r23                   -0.046712        0.051181      2.9941e-05      0.00057428
v  epsilon                0.068565          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9781e-05        0.009918      0.00092415       0.0017423
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2777         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71347         0.85282


 TIME FOR THE TIME STEP             9936:        0.79986E+02

===============================================================


 INSTANT    0.993700000E-02   TIME STEP NUMBER            9937
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.264475653E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.152543488E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.132544796E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.876945487E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.178773344E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81141E-03   0.45510E-02 0.19975E+01 
c  Velocity[X]                                      0.13933E-03 
c  Velocity[Y]                                      0.13005E-03 
c  Velocity[Z]                                      0.42816E-02 
c  Pressure     0.36497E-04     133   0.92878E-02   0.25745E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.56571E-08   0.16402E-08 0.10007E+00 
c  r22          0.10850E-01      13   0.52738E-08   0.18259E-08 0.10185E+00 
c  r33          0.21855E-01      15   0.53953E-08   0.12491E-07 0.12760E+00 
c  r12          0.93836E-03      18   0.52871E-08   0.30043E-09 0.60756E+00 
c  r13          0.46666E-02      19   0.58943E-08   0.15179E-08 0.20117E+00 
c  r23          0.39966E-02      19   0.67767E-08   0.12820E-08 0.19915E+00 
c  epsilon      0.10971E+02      11   0.34881E-08   0.98532E-02 0.16441E+00 
c  TempC        0.25716E+06      16   0.15102E-04   0.83968E-02 0.43248E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61356       0.0052526       0.0015069
v  Velocity[Y]            -0.57324          0.5442       0.0030773      0.00087296
v  Velocity[Z]              1.5657          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4369          4.3406          4.3632
v  Pressure                -36.426          360.16          87.736          169.96
v  r11                   0.0010592        0.081818        0.013068        0.018283
v  r22                   0.0011093         0.08263        0.013348        0.018643
v  r33                   0.0016332         0.17431        0.027237          0.0372
v  r12                   -0.010659        0.013572     -0.00023369     -0.00030924
v  r13                   -0.045557        0.052802      9.2553e-05       0.0010134
v  r23                   -0.046712        0.051177      2.9942e-05      0.00057428
v  epsilon                0.068566          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9781e-05        0.009918      0.00092415       0.0017423
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2777         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71347         0.85282


 TIME FOR THE TIME STEP             9937:        0.80409E+02

===============================================================


 INSTANT    0.993800000E-02   TIME STEP NUMBER            9938
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.326248901E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.715463774E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.123581962E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935024E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.205791741E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.420253921E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81191E-03   0.45640E-02 0.19989E+01 
c  Velocity[X]                                      0.14006E-03 
c  Velocity[Y]                                      0.12954E-03 
c  Velocity[Z]                                      0.42944E-02 
c  Pressure     0.36370E-04     133   0.92563E-02   0.25656E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55956E-08   0.16325E-08 0.10021E+00 
c  r22          0.10850E-01      13   0.56313E-08   0.18172E-08 0.10197E+00 
c  r33          0.21855E-01      15   0.54586E-08   0.12409E-07 0.12759E+00 
c  r12          0.93836E-03      18   0.59140E-08   0.29878E-09 0.60623E+00 
c  r13          0.46666E-02      19   0.73261E-08   0.14978E-08 0.20068E+00 
c  r23          0.39966E-02      19   0.61758E-08   0.12792E-08 0.19946E+00 
c  epsilon      0.10971E+02      11   0.33881E-08   0.95626E-02 0.16260E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.84552E-02 0.43410E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61352       0.0052526       0.0015069
v  Velocity[Y]            -0.57325         0.54431       0.0030773      0.00087291
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.489          360.01          87.668          169.85
v  r11                   0.0010592        0.081823        0.013068        0.018283
v  r22                   0.0011093         0.08263        0.013348        0.018643
v  r33                   0.0016332         0.17432        0.027237          0.0372
v  r12                   -0.010655         0.01358     -0.00023369     -0.00030924
v  r13                   -0.045554        0.052803      9.2555e-05       0.0010134
v  r23                   -0.046711        0.051209      2.9942e-05      0.00057428
v  epsilon                0.068566          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9778e-05       0.0099179      0.00092415       0.0017423
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2788         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71347         0.85282


 TIME FOR THE TIME STEP             9938:        0.82138E+02

===============================================================


 INSTANT    0.993900000E-02   TIME STEP NUMBER            9939
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.272450355E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.971706162E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116699998E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.297169258E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.329534177E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81119E-03   0.45448E-02 0.19963E+01 
c  Velocity[X]                                      0.14048E-03 
c  Velocity[Y]                                      0.12991E-03 
c  Velocity[Z]                                      0.42744E-02 
c  Pressure     0.35920E-04     133   0.91503E-02   0.25339E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.63302E-08   0.16158E-08 0.99593E-01 
c  r22          0.10850E-01      13   0.57159E-08   0.18435E-08 0.10221E+00 
c  r33          0.21855E-01      15   0.64738E-08   0.12468E-07 0.12735E+00 
c  r12          0.93836E-03      18   0.54937E-08   0.29074E-09 0.60292E+00 
c  r13          0.46666E-02      19   0.64461E-08   0.15083E-08 0.20084E+00 
c  r23          0.39966E-02      19   0.61349E-08   0.12497E-08 0.19731E+00 
c  epsilon      0.10971E+02      11   0.32525E-08   0.97334E-02 0.16303E+00 
c  TempC        0.25716E+06      16   0.15112E-04   0.85263E-02 0.43520E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397          0.6135       0.0052526       0.0015069
v  Velocity[Y]            -0.57323         0.54402       0.0030773      0.00087294
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.392          360.02           87.64          169.84
v  r11                   0.0010592        0.081831        0.013068        0.018283
v  r22                   0.0011093        0.082631        0.013348        0.018643
v  r33                   0.0016332         0.17435        0.027237          0.0372
v  r12                   -0.010653        0.013578     -0.00023369     -0.00030924
v  r13                   -0.045553          0.0528      9.2557e-05       0.0010134
v  r23                   -0.046711        0.051203      2.9944e-05      0.00057428
v  epsilon                0.068566           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9774e-05       0.0099178      0.00092415       0.0017423
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2789         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71347         0.85282


 TIME FOR THE TIME STEP             9939:        0.82101E+02

===============================================================


 INSTANT    0.994000000E-02   TIME STEP NUMBER            9940
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283354033E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.983148941E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.598141924E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.180558796E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.241191609E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81248E-03   0.45502E-02 0.19976E+01 
c  Velocity[X]                                      0.13900E-03 
c  Velocity[Y]                                      0.12923E-03 
c  Velocity[Z]                                      0.42820E-02 
c  Pressure     0.36722E-04     133   0.93442E-02   0.25904E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.62901E-08   0.16639E-08 0.10099E+00 
c  r22          0.10850E-01      13   0.54990E-08   0.18860E-08 0.10335E+00 
c  r33          0.21855E-01      15   0.59079E-08   0.12802E-07 0.12925E+00 
c  r12          0.93836E-03      18   0.50319E-08   0.30146E-09 0.60849E+00 
c  r13          0.46666E-02      19   0.65560E-08   0.15258E-08 0.20194E+00 
c  r23          0.39966E-02      19   0.57893E-08   0.12996E-08 0.20143E+00 
c  epsilon      0.10971E+02      11   0.33307E-08   0.98891E-02 0.16550E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.83571E-02 0.43149E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61354       0.0052526       0.0015069
v  Velocity[Y]            -0.57347         0.54406       0.0030773      0.00087293
v  Velocity[Z]              1.5654          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4368          4.3406          4.3632
v  Pressure                -36.458          360.09          87.706          169.92
v  r11                   0.0010592        0.081849        0.013068        0.018283
v  r22                   0.0011093        0.082631        0.013348        0.018643
v  r33                   0.0016332         0.17432        0.027237          0.0372
v  r12                   -0.010653        0.013583     -0.00023369     -0.00030924
v  r13                   -0.045556        0.052799      9.2559e-05       0.0010134
v  r23                   -0.046711        0.051187      2.9945e-05      0.00057428
v  epsilon                0.068567          271.32          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9773e-05       0.0099178      0.00092415       0.0017423
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2786         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71347         0.85282


 TIME FOR THE TIME STEP             9940:        0.82790E+02

===============================================================


 INSTANT    0.994100000E-02   TIME STEP NUMBER            9941
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.102000358E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.313782362E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.861124601E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935030E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.233296470E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.527736987E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935016E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81177E-03   0.45784E-02 0.20047E+01 
c  Velocity[X]                                      0.13965E-03 
c  Velocity[Y]                                      0.13045E-03 
c  Velocity[Z]                                      0.43083E-02 
c  Pressure     0.36628E-04     132   0.93227E-02   0.25839E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.62324E-08   0.16138E-08 0.99774E-01 
c  r22          0.10850E-01      13   0.55126E-08   0.18431E-08 0.10278E+00 
c  r33          0.21855E-01      15   0.60217E-08   0.12468E-07 0.12800E+00 
c  r12          0.93836E-03      18   0.51711E-08   0.29551E-09 0.60772E+00 
c  r13          0.46666E-02      19   0.73117E-08   0.15108E-08 0.20168E+00 
c  r23          0.39966E-02      19   0.57164E-08   0.12605E-08 0.19804E+00 
c  epsilon      0.10971E+02      11   0.32905E-08   0.96371E-02 0.16370E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84222E-02 0.43307E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61354       0.0052527       0.0015069
v  Velocity[Y]            -0.57337         0.54417       0.0030774      0.00087298
v  Velocity[Z]              1.5654          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4368          4.3406          4.3632
v  Pressure                 -36.42          360.02           87.65          169.85
v  r11                   0.0010592        0.081857        0.013068        0.018283
v  r22                   0.0011093        0.082632        0.013348        0.018643
v  r33                   0.0016332         0.17429        0.027237          0.0372
v  r12                   -0.010652         0.01358     -0.00023369     -0.00030924
v  r13                   -0.045555        0.052799      9.2561e-05       0.0010134
v  r23                   -0.046711        0.051181      2.9945e-05      0.00057428
v  epsilon                0.068567          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9772e-05       0.0099178      0.00092415       0.0017423
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2782         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71348         0.85282


 TIME FOR THE TIME STEP             9941:        0.81335E+02

===============================================================


 INSTANT    0.994200000E-02   TIME STEP NUMBER            9942
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.112581739E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.169817016E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.187643681E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.107601580E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.112402662E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81106E-03   0.45372E-02 0.19970E+01 
c  Velocity[X]                                      0.13892E-03 
c  Velocity[Y]                                      0.12984E-03 
c  Velocity[Z]                                      0.42684E-02 
c  Pressure     0.36658E-04     132   0.93390E-02   0.25859E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60802E-08   0.16715E-08 0.10093E+00 
c  r22          0.10850E-01      13   0.52775E-08   0.18421E-08 0.10225E+00 
c  r33          0.21855E-01      15   0.59000E-08   0.12788E-07 0.12899E+00 
c  r12          0.93836E-03      18   0.53706E-08   0.29697E-09 0.60663E+00 
c  r13          0.46666E-02      19   0.67588E-08   0.15112E-08 0.20114E+00 
c  r23          0.39966E-02      19   0.56235E-08   0.13093E-08 0.20169E+00 
c  epsilon      0.10971E+02      11   0.33055E-08   0.10491E-01 0.17303E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.83753E-02 0.43155E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389          0.6135       0.0052527       0.0015069
v  Velocity[Y]            -0.57341         0.54428       0.0030774        0.000873
v  Velocity[Z]              1.5652          5.4368          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4368          4.3406          4.3632
v  Pressure                -36.433          360.01          87.662          169.86
v  r11                   0.0010592        0.081868        0.013068        0.018283
v  r22                   0.0011093        0.082632        0.013348        0.018643
v  r33                   0.0016332         0.17429        0.027237          0.0372
v  r12                   -0.010656        0.013578     -0.00023369     -0.00030924
v  r13                   -0.045554        0.052798      9.2562e-05       0.0010134
v  r23                   -0.046711        0.051206      2.9946e-05      0.00057428
v  epsilon                0.068567          271.28          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9772e-05       0.0099178      0.00092416       0.0017423
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2786         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71347         0.85282


 TIME FOR THE TIME STEP             9942:        0.84407E+02

===============================================================


 INSTANT    0.994300000E-02   TIME STEP NUMBER            9943
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.206338424E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.230025970E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129428753E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122569845E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.404700113E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81238E-03   0.45252E-02 0.19926E+01 
c  Velocity[X]                                      0.13914E-03 
c  Velocity[Y]                                      0.12995E-03 
c  Velocity[Z]                                      0.42562E-02 
c  Pressure     0.36352E-04     131   0.92513E-02   0.25643E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60914E-08   0.16501E-08 0.10018E+00 
c  r22          0.10850E-01      13   0.48826E-08   0.18744E-08 0.10299E+00 
c  r33          0.21855E-01      14   0.70674E-08   0.12727E-07 0.12859E+00 
c  r12          0.93836E-03      18   0.48804E-08   0.29566E-09 0.60208E+00 
c  r13          0.46666E-02      19   0.59579E-08   0.15085E-08 0.20098E+00 
c  r23          0.39966E-02      19   0.54357E-08   0.12913E-08 0.19944E+00 
c  epsilon      0.10971E+02      11   0.33078E-08   0.10037E-01 0.16653E+00 
c  TempC        0.25716E+06      16   0.15091E-04   0.84670E-02 0.43456E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61354       0.0052527       0.0015069
v  Velocity[Y]             -0.5733         0.54437       0.0030774      0.00087298
v  Velocity[Z]              1.5653          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4368          4.3406          4.3632
v  Pressure                -36.392          360.11          87.706          169.92
v  r11                   0.0010592        0.081868        0.013068        0.018283
v  r22                   0.0011093        0.082631        0.013348        0.018643
v  r33                   0.0016332         0.17431        0.027237          0.0372
v  r12                   -0.010656        0.013582     -0.00023369     -0.00030924
v  r13                   -0.045556        0.052798      9.2564e-05       0.0010134
v  r23                    -0.04671        0.051197      2.9946e-05      0.00057428
v  epsilon                0.068567          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9771e-05       0.0099178      0.00092416       0.0017423
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2782         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71348         0.85282


 TIME FOR THE TIME STEP             9943:        0.77249E+02

===============================================================


 INSTANT    0.994400000E-02   TIME STEP NUMBER            9944
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.721426367E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.420655925E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.419146845E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.313777630E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.279098008E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      45   0.81127E-03   0.45595E-02 0.19994E+01 
c  Velocity[X]                                      0.14032E-03 
c  Velocity[Y]                                      0.13001E-03 
c  Velocity[Z]                                      0.42891E-02 
c  Pressure     0.36137E-04     132   0.92055E-02   0.25492E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60939E-08   0.16367E-08 0.99842E-01 
c  r22          0.10850E-01      13   0.51946E-08   0.18669E-08 0.10248E+00 
c  r33          0.21855E-01      15   0.52718E-08   0.12692E-07 0.12795E+00 
c  r12          0.93836E-03      18   0.56504E-08   0.29658E-09 0.60409E+00 
c  r13          0.46666E-02      18   0.69657E-08   0.15418E-08 0.20177E+00 
c  r23          0.39966E-02      18   0.65527E-08   0.12843E-08 0.19882E+00 
c  epsilon      0.10971E+02      11   0.32932E-08   0.10063E-01 0.16516E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.84842E-02 0.43411E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61353       0.0052527       0.0015069
v  Velocity[Y]            -0.57337         0.54413       0.0030774      0.00087298
v  Velocity[Z]              1.5654          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4368          4.3406          4.3632
v  Pressure                -36.478          360.01          87.659          169.84
v  r11                   0.0010592        0.081867        0.013068        0.018283
v  r22                   0.0011093         0.08263        0.013348        0.018643
v  r33                   0.0016332         0.17429        0.027237          0.0372
v  r12                   -0.010657        0.013585     -0.00023369     -0.00030924
v  r13                   -0.045553        0.052798      9.2566e-05       0.0010134
v  r23                    -0.04671        0.051192      2.9947e-05      0.00057428
v  epsilon                0.068568          271.32          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9768e-05       0.0099179      0.00092416       0.0017423
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017898           5.278         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71347         0.85282


 TIME FOR THE TIME STEP             9944:        0.82283E+02

===============================================================


 INSTANT    0.994500000E-02   TIME STEP NUMBER            9945
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221940851E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.273058207E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.460466004E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.398313390E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.915890230E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81143E-03   0.45620E-02 0.19998E+01 
c  Velocity[X]                                      0.13997E-03 
c  Velocity[Y]                                      0.12964E-03 
c  Velocity[Z]                                      0.42923E-02 
c  Pressure     0.36366E-04     132   0.92621E-02   0.25653E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.61473E-08   0.16549E-08 0.10045E+00 
c  r22          0.10850E-01      13   0.52180E-08   0.18308E-08 0.10177E+00 
c  r33          0.21855E-01      15   0.66356E-08   0.12518E-07 0.12750E+00 
c  r12          0.93836E-03      18   0.52850E-08   0.29752E-09 0.60610E+00 
c  r13          0.46666E-02      19   0.72730E-08   0.14981E-08 0.19995E+00 
c  r23          0.39966E-02      19   0.51030E-08   0.12774E-08 0.19881E+00 
c  epsilon      0.10971E+02      11   0.33046E-08   0.98601E-02 0.16560E+00 
c  TempC        0.25716E+06      16   0.15098E-04   0.83909E-02 0.43221E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61351       0.0052527       0.0015069
v  Velocity[Y]            -0.57335         0.54421       0.0030774      0.00087296
v  Velocity[Z]              1.5652          5.4368          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4368          4.3406          4.3632
v  Pressure                -36.417          360.01          87.635          169.84
v  r11                   0.0010592        0.081867        0.013068        0.018283
v  r22                   0.0011094        0.082625        0.013348        0.018643
v  r33                   0.0016333         0.17427        0.027237          0.0372
v  r12                   -0.010654        0.013588     -0.00023369     -0.00030924
v  r13                   -0.045555        0.052797      9.2569e-05       0.0010134
v  r23                   -0.046709        0.051213      2.9948e-05      0.00057428
v  epsilon                0.068568          271.27          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9767e-05       0.0099179      0.00092416       0.0017423
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2778         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71347         0.85282


 TIME FOR THE TIME STEP             9945:        0.78011E+02

===============================================================


 INSTANT    0.994600000E-02   TIME STEP NUMBER            9946
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.109877633E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.118943330E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.529464368E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.102847592E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.326182195E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81196E-03   0.45314E-02 0.19946E+01 
c  Velocity[X]                                      0.13922E-03 
c  Velocity[Y]                                      0.12935E-03 
c  Velocity[Z]                                      0.42628E-02 
c  Pressure     0.36458E-04     133   0.92828E-02   0.25718E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59576E-08   0.16554E-08 0.10019E+00 
c  r22          0.10850E-01      13   0.56595E-08   0.18337E-08 0.10164E+00 
c  r33          0.21855E-01      15   0.58725E-08   0.12530E-07 0.12761E+00 
c  r12          0.93836E-03      18   0.61297E-08   0.30675E-09 0.61016E+00 
c  r13          0.46666E-02      20   0.60902E-08   0.15113E-08 0.20060E+00 
c  r23          0.39966E-02      19   0.63235E-08   0.12827E-08 0.19984E+00 
c  epsilon      0.10971E+02      11   0.32460E-08   0.99645E-02 0.16646E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.84099E-02 0.43272E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61356       0.0052528       0.0015069
v  Velocity[Y]            -0.57339         0.54432       0.0030774      0.00087296
v  Velocity[Z]              1.5655          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4368          4.3406          4.3632
v  Pressure                -36.449          360.05          87.677          169.89
v  r11                   0.0010593        0.081866        0.013068        0.018283
v  r22                   0.0011094        0.082625        0.013348        0.018643
v  r33                   0.0016333         0.17428        0.027237          0.0372
v  r12                   -0.010656        0.013588     -0.00023369     -0.00030924
v  r13                   -0.045557        0.052797      9.2571e-05       0.0010134
v  r23                   -0.046708        0.051196       2.995e-05      0.00057428
v  epsilon                0.068568          271.28          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9765e-05       0.0099179      0.00092416       0.0017423
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2769         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71347         0.85282


 TIME FOR THE TIME STEP             9946:        0.78477E+02

===============================================================


 INSTANT    0.994700000E-02   TIME STEP NUMBER            9947
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232434711E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.266244760E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.378315684E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.589219330E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.628071925E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      44   0.81194E-03   0.45356E-02 0.19950E+01 
c  Velocity[X]                                      0.13977E-03 
c  Velocity[Y]                                      0.13011E-03 
c  Velocity[Z]                                      0.42658E-02 
c  Pressure     0.36456E-04     133   0.92813E-02   0.25716E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.58457E-08   0.16793E-08 0.10115E+00 
c  r22          0.10850E-01      13   0.56917E-08   0.18383E-08 0.10211E+00 
c  r33          0.21855E-01      15   0.53437E-08   0.12617E-07 0.12828E+00 
c  r12          0.93836E-03      18   0.60235E-08   0.29590E-09 0.60591E+00 
c  r13          0.46666E-02      19   0.64792E-08   0.14873E-08 0.20018E+00 
c  r23          0.39966E-02      19   0.62576E-08   0.12962E-08 0.20115E+00 
c  epsilon      0.10971E+02      11   0.33436E-08   0.96681E-02 0.16397E+00 
c  TempC        0.25716E+06      16   0.15125E-04   0.84523E-02 0.43384E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61355       0.0052528       0.0015069
v  Velocity[Y]            -0.57332         0.54414       0.0030774      0.00087298
v  Velocity[Z]              1.5653          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4368          4.3406          4.3632
v  Pressure                -36.446          360.06           87.68          169.89
v  r11                   0.0010593        0.081868        0.013068        0.018283
v  r22                   0.0011094        0.082625        0.013348        0.018643
v  r33                   0.0016333         0.17432        0.027237          0.0372
v  r12                   -0.010654        0.013588     -0.00023369     -0.00030924
v  r13                   -0.045554        0.052798      9.2572e-05       0.0010134
v  r23                   -0.046706        0.051179      2.9951e-05      0.00057428
v  epsilon                0.068568           271.3          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9763e-05        0.009918      0.00092416       0.0017423
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2763         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8763         0.71348         0.85282


 TIME FOR THE TIME STEP             9947:        0.78552E+02

===============================================================


 INSTANT    0.994800000E-02   TIME STEP NUMBER            9948
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.264463047E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.845313339E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.344042888E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.818122601E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.220130197E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81177E-03   0.45659E-02 0.20029E+01 
c  Velocity[X]                                      0.14063E-03 
c  Velocity[Y]                                      0.13099E-03 
c  Velocity[Z]                                      0.42942E-02 
c  Pressure     0.36654E-04     133   0.93287E-02   0.25857E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57277E-08   0.16901E-08 0.10180E+00 
c  r22          0.10850E-01      13   0.56685E-08   0.18484E-08 0.10256E+00 
c  r33          0.21855E-01      15   0.52158E-08   0.12825E-07 0.12955E+00 
c  r12          0.93836E-03      18   0.66149E-08   0.30100E-09 0.60950E+00 
c  r13          0.46666E-02      19   0.62496E-08   0.15116E-08 0.20179E+00 
c  r23          0.39966E-02      19   0.60801E-08   0.13149E-08 0.20274E+00 
c  epsilon      0.10971E+02      11   0.33900E-08   0.10263E-01 0.17168E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.84854E-02 0.43459E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -0.634          0.6135       0.0052529       0.0015069
v  Velocity[Y]            -0.57341         0.54422       0.0030774      0.00087298
v  Velocity[Z]              1.5652          5.4368          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4368          4.3406          4.3632
v  Pressure                -36.442          360.04           87.67          169.87
v  r11                   0.0010593        0.081862        0.013068        0.018283
v  r22                   0.0011094        0.082627        0.013348        0.018643
v  r33                   0.0016333         0.17432        0.027237          0.0372
v  r12                   -0.010655        0.013587     -0.00023369     -0.00030924
v  r13                   -0.045553        0.052797      9.2574e-05       0.0010134
v  r23                   -0.046705        0.051205      2.9952e-05      0.00057428
v  epsilon                0.068569          271.31          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9762e-05        0.009918      0.00092416       0.0017423
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2762         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8762         0.71347         0.85282


 TIME FOR THE TIME STEP             9948:        0.79759E+02

===============================================================


 INSTANT    0.994900000E-02   TIME STEP NUMBER            9949
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.279861364E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.280452212E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.336040660E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.125184344E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.150503982E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81085E-03   0.45322E-02 0.19923E+01 
c  Velocity[X]                                      0.13839E-03 
c  Velocity[Y]                                      0.12882E-03 
c  Velocity[Z]                                      0.42649E-02 
c  Pressure     0.36279E-04     133   0.92353E-02   0.25591E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.56458E-08   0.16481E-08 0.10081E+00 
c  r22          0.10850E-01      13   0.53414E-08   0.18274E-08 0.10190E+00 
c  r33          0.21855E-01      15   0.54507E-08   0.12454E-07 0.12781E+00 
c  r12          0.93836E-03      18   0.61911E-08   0.30156E-09 0.61192E+00 
c  r13          0.46666E-02      19   0.59090E-08   0.14969E-08 0.19987E+00 
c  r23          0.39966E-02      19   0.56905E-08   0.12736E-08 0.19958E+00 
c  epsilon      0.10971E+02      11   0.32689E-08   0.96347E-02 0.16521E+00 
c  TempC        0.25716E+06      16   0.15127E-04   0.84256E-02 0.43309E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61354       0.0052528       0.0015069
v  Velocity[Y]            -0.57337         0.54434       0.0030775      0.00087301
v  Velocity[Z]               1.565          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5787          5.4369          4.3406          4.3632
v  Pressure                -36.428          360.04          87.654          169.86
v  r11                   0.0010593        0.081857        0.013068        0.018283
v  r22                   0.0011094        0.082627        0.013348        0.018643
v  r33                   0.0016333         0.17429        0.027237          0.0372
v  r12                   -0.010656        0.013587     -0.00023369     -0.00030925
v  r13                   -0.045557        0.052796      9.2575e-05       0.0010134
v  r23                   -0.046703        0.051197      2.9953e-05      0.00057428
v  epsilon                0.068569          271.28          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.976e-05       0.0099181      0.00092417       0.0017423
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2771         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71347         0.85282


 TIME FOR THE TIME STEP             9949:        0.81166E+02

===============================================================


 INSTANT    0.995000000E-02   TIME STEP NUMBER            9950
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.864891940E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.344439471E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.616954813E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.973395222E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.985164810E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69808E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81226E-03   0.45657E-02 0.20025E+01 
c  Velocity[X]                                      0.13961E-03 
c  Velocity[Y]                                      0.12997E-03 
c  Velocity[Z]                                      0.42961E-02 
c  Pressure     0.36336E-04     131   0.92515E-02   0.25632E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.56483E-08   0.16422E-08 0.10028E+00 
c  r22          0.10850E-01      13   0.52397E-08   0.18529E-08 0.10246E+00 
c  r33          0.21855E-01      15   0.55136E-08   0.12600E-07 0.12800E+00 
c  r12          0.93836E-03      18   0.54284E-08   0.29524E-09 0.60695E+00 
c  r13          0.46666E-02      19   0.59093E-08   0.15160E-08 0.20084E+00 
c  r23          0.39966E-02      19   0.60566E-08   0.12877E-08 0.20007E+00 
c  epsilon      0.10971E+02      11   0.32691E-08   0.10076E-01 0.16750E+00 
c  TempC        0.25716E+06      16   0.15107E-04   0.84169E-02 0.43266E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397          0.6135       0.0052528       0.0015069
v  Velocity[Y]            -0.57337          0.5442       0.0030775      0.00087302
v  Velocity[Z]              1.5649          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5787          5.4369          4.3406          4.3632
v  Pressure                -36.452          360.01          87.678          169.86
v  r11                   0.0010593        0.081856        0.013068        0.018283
v  r22                   0.0011094        0.082626        0.013348        0.018643
v  r33                   0.0016333         0.17432        0.027237          0.0372
v  r12                   -0.010655        0.013588     -0.00023369     -0.00030925
v  r13                   -0.045554        0.052795      9.2578e-05       0.0010134
v  r23                   -0.046701        0.051186      2.9954e-05      0.00057428
v  epsilon                0.068569          271.26          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.976e-05       0.0099177      0.00092417       0.0017423
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2771          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71348         0.85282


 TIME FOR THE TIME STEP             9950:        0.82148E+02

===============================================================


 INSTANT    0.995100000E-02   TIME STEP NUMBER            9951
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.396621782E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.137876854E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201804334E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935016E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.184070777E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.314265771E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81223E-03   0.45549E-02 0.20000E+01 
c  Velocity[X]                                      0.13961E-03 
c  Velocity[Y]                                      0.12949E-03 
c  Velocity[Z]                                      0.42858E-02 
c  Pressure     0.36369E-04     133   0.92604E-02   0.25654E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.56802E-08   0.16573E-08 0.10030E+00 
c  r22          0.10850E-01      13   0.49405E-08   0.18555E-08 0.10219E+00 
c  r33          0.21855E-01      15   0.52500E-08   0.12729E-07 0.12797E+00 
c  r12          0.93836E-03      18   0.54188E-08   0.29518E-09 0.60490E+00 
c  r13          0.46666E-02      18   0.69053E-08   0.15203E-08 0.20110E+00 
c  r23          0.39966E-02      19   0.59416E-08   0.12758E-08 0.19879E+00 
c  epsilon      0.10971E+02      11   0.35233E-08   0.10401E-01 0.17006E+00 
c  TempC        0.25716E+06      16   0.15088E-04   0.85196E-02 0.43564E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61349       0.0052529       0.0015069
v  Velocity[Y]            -0.57333         0.54419       0.0030776      0.00087306
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.404          360.05          87.661          169.87
v  r11                   0.0010593        0.081859        0.013068        0.018283
v  r22                   0.0011094        0.082626        0.013348        0.018643
v  r33                   0.0016333         0.17435        0.027237          0.0372
v  r12                   -0.010654        0.013589     -0.00023369     -0.00030925
v  r13                   -0.045554        0.052794      9.2579e-05       0.0010134
v  r23                   -0.046699        0.051207      2.9956e-05      0.00057429
v  epsilon                0.068569          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.976e-05       0.0099173      0.00092417       0.0017423
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017898           5.278         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85282


 TIME FOR THE TIME STEP             9951:        0.82841E+02

===============================================================


 INSTANT    0.995200000E-02   TIME STEP NUMBER            9952
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.725435425E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.939573077E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.376286871E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.273862553E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.243707549E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81277E-03   0.45451E-02 0.19951E+01 
c  Velocity[X]                                      0.13936E-03 
c  Velocity[Y]                                      0.12939E-03 
c  Velocity[Z]                                      0.42764E-02 
c  Pressure     0.36572E-04     131   0.93072E-02   0.25798E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.53383E-08   0.16477E-08 0.10058E+00 
c  r22          0.10850E-01      13   0.48356E-08   0.18265E-08 0.10184E+00 
c  r33          0.21855E-01      15   0.54493E-08   0.12605E-07 0.12808E+00 
c  r12          0.93836E-03      18   0.52540E-08   0.29448E-09 0.60350E+00 
c  r13          0.46666E-02      18   0.69109E-08   0.15043E-08 0.20036E+00 
c  r23          0.39966E-02      19   0.58004E-08   0.12942E-08 0.20099E+00 
c  epsilon      0.10971E+02      11   0.34507E-08   0.99607E-02 0.16577E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.83979E-02 0.43269E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61351       0.0052529       0.0015069
v  Velocity[Y]            -0.57336         0.54423       0.0030774        0.000873
v  Velocity[Z]              1.5649          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5787          5.4369          4.3406          4.3632
v  Pressure                -36.465          360.05          87.671          169.88
v  r11                   0.0010593        0.081876        0.013068        0.018283
v  r22                   0.0011094        0.082626        0.013348        0.018643
v  r33                   0.0016333         0.17433        0.027237          0.0372
v  r12                   -0.010659        0.013592     -0.00023369     -0.00030925
v  r13                   -0.045556        0.052796      9.2581e-05       0.0010134
v  r23                   -0.046697        0.051186      2.9957e-05      0.00057429
v  epsilon                 0.06857          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9759e-05       0.0099175      0.00092417       0.0017423
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2775         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71348         0.85282


 TIME FOR THE TIME STEP             9952:        0.82475E+02

===============================================================


 INSTANT    0.995300000E-02   TIME STEP NUMBER            9953
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.341974528E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.546891808E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.248973336E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186567632E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.146155071E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69807E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81110E-03   0.45431E-02 0.19937E+01 
c  Velocity[X]                                      0.13923E-03 
c  Velocity[Y]                                      0.12993E-03 
c  Velocity[Z]                                      0.42740E-02 
c  Pressure     0.36361E-04     131   0.92550E-02   0.25650E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52392E-08   0.16631E-08 0.10067E+00 
c  r22          0.10850E-01      13   0.49696E-08   0.18397E-08 0.10211E+00 
c  r33          0.21855E-01      15   0.53716E-08   0.12575E-07 0.12791E+00 
c  r12          0.93836E-03      18   0.56132E-08   0.29786E-09 0.60642E+00 
c  r13          0.46666E-02      19   0.57839E-08   0.15181E-08 0.20122E+00 
c  r23          0.39966E-02      19   0.64121E-08   0.13020E-08 0.20092E+00 
c  epsilon      0.10971E+02      11   0.33296E-08   0.97831E-02 0.16491E+00 
c  TempC        0.25716E+06      16   0.15121E-04   0.84275E-02 0.43332E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161987


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61351       0.0052529       0.0015069
v  Velocity[Y]            -0.57323         0.54436       0.0030775      0.00087301
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.423          360.07          87.676          169.89
v  r11                   0.0010593        0.081886        0.013068        0.018283
v  r22                   0.0011095        0.082622        0.013348        0.018643
v  r33                   0.0016334         0.17431        0.027237          0.0372
v  r12                   -0.010658        0.013595     -0.00023369     -0.00030925
v  r13                   -0.045555        0.052797      9.2583e-05       0.0010134
v  r23                   -0.046695        0.051178      2.9958e-05      0.00057429
v  epsilon                 0.06857          271.27          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9759e-05       0.0099177      0.00092417       0.0017423
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2768         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71347         0.85282


 TIME FOR THE TIME STEP             9953:        0.81336E+02

===============================================================


 INSTANT    0.995400000E-02   TIME STEP NUMBER            9954
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.316089985E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125679079E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123548483E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.926781168E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.135826923E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81256E-03   0.45584E-02 0.20015E+01 
c  Velocity[X]                                      0.13972E-03 
c  Velocity[Y]                                      0.13077E-03 
c  Velocity[Z]                                      0.42879E-02 
c  Pressure     0.36560E-04     133   0.93068E-02   0.25790E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55588E-08   0.16784E-08 0.10114E+00 
c  r22          0.10850E-01      13   0.54990E-08   0.18355E-08 0.10215E+00 
c  r33          0.21855E-01      15   0.61238E-08   0.12752E-07 0.12896E+00 
c  r12          0.93836E-03      18   0.59802E-08   0.30364E-09 0.61109E+00 
c  r13          0.46666E-02      19   0.55388E-08   0.15108E-08 0.20084E+00 
c  r23          0.39966E-02      19   0.66409E-08   0.13313E-08 0.20376E+00 
c  epsilon      0.10971E+02      11   0.33936E-08   0.10240E-01 0.17140E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84799E-02 0.43383E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161985


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61349       0.0052529        0.001507
v  Velocity[Y]            -0.57334         0.54417       0.0030775        0.000873
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.472             360           87.66          169.84
v  r11                   0.0010593        0.081889        0.013068        0.018283
v  r22                   0.0011095        0.082623        0.013348        0.018643
v  r33                   0.0016334         0.17433        0.027237          0.0372
v  r12                   -0.010658        0.013595     -0.00023369     -0.00030925
v  r13                   -0.045553        0.052797      9.2586e-05       0.0010134
v  r23                   -0.046694        0.051202      2.9959e-05      0.00057429
v  epsilon                 0.06857          271.27          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9758e-05       0.0099178      0.00092417       0.0017423
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2774          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71348         0.85282


 TIME FOR THE TIME STEP             9954:        0.79174E+02

===============================================================


 INSTANT    0.995500000E-02   TIME STEP NUMBER            9955
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.400997716E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.121848358E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.110949700E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.219269051E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.142361237E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81205E-03   0.45579E-02 0.19986E+01 
c  Velocity[X]                                      0.13889E-03 
c  Velocity[Y]                                      0.12904E-03 
c  Velocity[Z]                                      0.42899E-02 
c  Pressure     0.36628E-04     132   0.93242E-02   0.25837E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59125E-08   0.16248E-08 0.99626E-01 
c  r22          0.10850E-01      13   0.58848E-08   0.18006E-08 0.10148E+00 
c  r33          0.21855E-01      15   0.66217E-08   0.12287E-07 0.12673E+00 
c  r12          0.93836E-03      18   0.66264E-08   0.29513E-09 0.60244E+00 
c  r13          0.46666E-02      19   0.64736E-08   0.14634E-08 0.19873E+00 
c  r23          0.39966E-02      19   0.67647E-08   0.12676E-08 0.19825E+00 
c  epsilon      0.10971E+02      11   0.33160E-08   0.97077E-02 0.16394E+00 
c  TempC        0.25716E+06      16   0.15089E-04   0.84161E-02 0.43305E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161986


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61355        0.005253        0.001507
v  Velocity[Y]            -0.57329         0.54411       0.0030775      0.00087302
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.436          360.08          87.676           169.9
v  r11                   0.0010593        0.081906        0.013068        0.018283
v  r22                   0.0011095        0.082624        0.013348        0.018643
v  r33                   0.0016334         0.17435        0.027237          0.0372
v  r12                   -0.010653        0.013597     -0.00023369     -0.00030925
v  r13                   -0.045556        0.052795      9.2587e-05       0.0010134
v  r23                   -0.046692        0.051188       2.996e-05      0.00057429
v  epsilon                 0.06857          271.31          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9754e-05       0.0099178      0.00092417       0.0017423
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2775          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71348         0.85283


 TIME FOR THE TIME STEP             9955:        0.78588E+02

===============================================================


 INSTANT    0.995600000E-02   TIME STEP NUMBER            9956
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.690524216E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.547806483E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934889E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.226701026E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.208769038E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232520400E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81202E-03   0.45643E-02 0.20015E+01 
c  Velocity[X]                                      0.13920E-03 
c  Velocity[Y]                                      0.12955E-03 
c  Velocity[Z]                                      0.42956E-02 
c  Pressure     0.36382E-04     133   0.92657E-02   0.25664E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60249E-08   0.16082E-08 0.99273E-01 
c  r22          0.10850E-01      13   0.61172E-08   0.18241E-08 0.10152E+00 
c  r33          0.21855E-01      15   0.58796E-08   0.12374E-07 0.12668E+00 
c  r12          0.93836E-03      18   0.61056E-08   0.29333E-09 0.60416E+00 
c  r13          0.46666E-02      19   0.55589E-08   0.15055E-08 0.20059E+00 
c  r23          0.39966E-02      20   0.55025E-08   0.12643E-08 0.19794E+00 
c  epsilon      0.10971E+02      11   0.33480E-08   0.98111E-02 0.16301E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84155E-02 0.43302E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161982


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61352        0.005253        0.001507
v  Velocity[Y]            -0.57343         0.54418       0.0030775      0.00087299
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.466          360.06          87.693          169.89
v  r11                   0.0010593        0.081917        0.013068        0.018283
v  r22                   0.0011095        0.082625        0.013348        0.018643
v  r33                   0.0016334         0.17434        0.027237          0.0372
v  r12                   -0.010648          0.0136     -0.00023369     -0.00030925
v  r13                   -0.045553        0.052797      9.2589e-05       0.0010134
v  r23                    -0.04669        0.051183      2.9961e-05      0.00057429
v  epsilon                0.068571           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9752e-05       0.0099176      0.00092418       0.0017423
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2776         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71348         0.85282


 TIME FOR THE TIME STEP             9956:        0.79747E+02

===============================================================


 INSTANT    0.995700000E-02   TIME STEP NUMBER            9957
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145375442E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.326159477E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.161460539E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.403030785E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.276039832E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81155E-03   0.45465E-02 0.19979E+01 
c  Velocity[X]                                      0.14033E-03 
c  Velocity[Y]                                      0.12938E-03 
c  Velocity[Z]                                      0.42768E-02 
c  Pressure     0.36546E-04     133   0.93052E-02   0.25781E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.61280E-08   0.16427E-08 0.10009E+00 
c  r22          0.10850E-01      13   0.63698E-08   0.18292E-08 0.10166E+00 
c  r33          0.21855E-01      15   0.51783E-08   0.12536E-07 0.12752E+00 
c  r12          0.93836E-03      18   0.58169E-08   0.29308E-09 0.60126E+00 
c  r13          0.46666E-02      19   0.57020E-08   0.14946E-08 0.20043E+00 
c  r23          0.39966E-02      20   0.57760E-08   0.12719E-08 0.19891E+00 
c  epsilon      0.10971E+02      11   0.32939E-08   0.99390E-02 0.16547E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.84343E-02 0.43360E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161981


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61348        0.005253        0.001507
v  Velocity[Y]            -0.57347         0.54432       0.0030776      0.00087302
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.436           360.1          87.693          169.91
v  r11                   0.0010593        0.081928        0.013068        0.018283
v  r22                   0.0011095        0.082627        0.013348        0.018643
v  r33                   0.0016334         0.17433        0.027238          0.0372
v  r12                   -0.010648        0.013595     -0.00023369     -0.00030925
v  r13                   -0.045554        0.052796      9.2591e-05       0.0010134
v  r23                   -0.046688        0.051165      2.9962e-05      0.00057429
v  epsilon                0.068571          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9753e-05       0.0099175      0.00092418       0.0017423
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017899           5.278         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85282


 TIME FOR THE TIME STEP             9957:        0.79281E+02

===============================================================


 INSTANT    0.995800000E-02   TIME STEP NUMBER            9958
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283700277E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100637216E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.331535895E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.233266733E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.515861475E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81237E-03   0.45062E-02 0.19880E+01 
c  Velocity[X]                                      0.13861E-03 
c  Velocity[Y]                                      0.13019E-03 
c  Velocity[Z]                                      0.42374E-02 
c  Pressure     0.36339E-04     131   0.92567E-02   0.25633E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.62767E-08   0.16383E-08 0.10006E+00 
c  r22          0.10850E-01      13   0.63169E-08   0.18190E-08 0.10163E+00 
c  r33          0.21855E-01      15   0.62538E-08   0.12511E-07 0.12746E+00 
c  r12          0.93837E-03      18   0.61782E-08   0.29508E-09 0.60302E+00 
c  r13          0.46666E-02      19   0.64586E-08   0.14811E-08 0.19976E+00 
c  r23          0.39966E-02      19   0.70076E-08   0.12843E-08 0.19986E+00 
c  epsilon      0.10971E+02      11   0.34273E-08   0.99899E-02 0.16798E+00 
c  TempC        0.25716E+06      16   0.15108E-04   0.84139E-02 0.43249E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393         0.61355       0.0052531        0.001507
v  Velocity[Y]            -0.57352         0.54407       0.0030774      0.00087294
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.477          360.01          87.659          169.85
v  r11                   0.0010593        0.081929        0.013068        0.018283
v  r22                   0.0011095        0.082628        0.013348        0.018643
v  r33                   0.0016334         0.17435        0.027238          0.0372
v  r12                   -0.010648        0.013596     -0.00023369     -0.00030925
v  r13                   -0.045555        0.052796      9.2593e-05       0.0010134
v  r23                   -0.046686        0.051199      2.9962e-05      0.00057429
v  epsilon                0.068571           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9755e-05       0.0099175      0.00092418       0.0017423
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2777         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85282


 TIME FOR THE TIME STEP             9958:        0.78676E+02

===============================================================


 INSTANT    0.995900000E-02   TIME STEP NUMBER            9959
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.147303003E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.404413998E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.533539210E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.241688820E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.331896643E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81237E-03   0.45603E-02 0.20020E+01 
c  Velocity[X]                                      0.14013E-03 
c  Velocity[Y]                                      0.12992E-03 
c  Velocity[Z]                                      0.42903E-02 
c  Pressure     0.36654E-04     131   0.93289E-02   0.25857E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.61645E-08   0.16264E-08 0.99640E-01 
c  r22          0.10850E-01      13   0.58070E-08   0.18358E-08 0.10182E+00 
c  r33          0.21855E-01      15   0.73570E-08   0.12486E-07 0.12715E+00 
c  r12          0.93837E-03      18   0.56786E-08   0.30261E-09 0.60472E+00 
c  r13          0.46666E-02      19   0.76927E-08   0.14934E-08 0.20001E+00 
c  r23          0.39966E-02      19   0.62897E-08   0.12613E-08 0.19809E+00 
c  epsilon      0.10971E+02      11   0.35406E-08   0.10017E-01 0.16646E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.85286E-02 0.43539E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393         0.61351       0.0052531       0.0015071
v  Velocity[Y]            -0.57339         0.54416       0.0030776      0.00087299
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                 -36.42          360.02          87.642          169.85
v  r11                   0.0010594        0.081928        0.013068        0.018283
v  r22                   0.0011095        0.082629        0.013348        0.018643
v  r33                   0.0016334         0.17438        0.027238          0.0372
v  r12                   -0.010647          0.0136     -0.00023369     -0.00030925
v  r13                   -0.045552        0.052796      9.2595e-05       0.0010134
v  r23                   -0.046684        0.051202      2.9964e-05      0.00057429
v  epsilon                0.068571          271.33          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9757e-05       0.0099176      0.00092418       0.0017423
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2782         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71347         0.85282


 TIME FOR THE TIME STEP             9959:        0.80024E+02

===============================================================


 INSTANT    0.996000000E-02   TIME STEP NUMBER            9960
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161667156E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.129584370E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.687399594E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.761684699E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.252445410E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81150E-03   0.45630E-02 0.20014E+01 
c  Velocity[X]                                      0.13998E-03 
c  Velocity[Y]                                      0.12994E-03 
c  Velocity[Z]                                      0.42931E-02 
c  Pressure     0.36398E-04     131   0.92758E-02   0.25675E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60028E-08   0.16411E-08 0.10036E+00 
c  r22          0.10850E-01      13   0.60089E-08   0.18089E-08 0.10150E+00 
c  r33          0.21855E-01      15   0.61802E-08   0.12481E-07 0.12768E+00 
c  r12          0.93837E-03      18   0.65593E-08   0.29906E-09 0.60745E+00 
c  r13          0.46666E-02      19   0.66842E-08   0.14749E-08 0.19903E+00 
c  r23          0.39966E-02      19   0.63964E-08   0.12861E-08 0.20043E+00 
c  epsilon      0.10971E+02      11   0.33360E-08   0.10179E-01 0.17055E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.84235E-02 0.43328E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61344       0.0052531        0.001507
v  Velocity[Y]             -0.5735         0.54435       0.0030775      0.00087294
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.483          360.04          87.677          169.87
v  r11                   0.0010594        0.081927        0.013068        0.018283
v  r22                   0.0011095         0.08263        0.013348        0.018643
v  r33                   0.0016335         0.17437        0.027238          0.0372
v  r12                   -0.010646        0.013605     -0.00023369     -0.00030925
v  r13                   -0.045552        0.052797      9.2597e-05       0.0010134
v  r23                   -0.046682        0.051192      2.9964e-05      0.00057429
v  epsilon                0.068572          271.34          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9757e-05       0.0099175      0.00092418       0.0017423
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2792          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8792         0.71348         0.85282


 TIME FOR THE TIME STEP             9960:        0.77983E+02

===============================================================


 INSTANT    0.996100000E-02   TIME STEP NUMBER            9961
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.531205964E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183170599E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106194180E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.424644055E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.675489852E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81200E-03   0.45434E-02 0.19950E+01 
c  Velocity[X]                                      0.13861E-03 
c  Velocity[Y]                                      0.13031E-03 
c  Velocity[Z]                                      0.42744E-02 
c  Pressure     0.36312E-04     132   0.92470E-02   0.25614E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57181E-08   0.16144E-08 0.99737E-01 
c  r22          0.10850E-01      13   0.55817E-08   0.18006E-08 0.10130E+00 
c  r33          0.21855E-01      15   0.56603E-08   0.12270E-07 0.12665E+00 
c  r12          0.93837E-03      18   0.54714E-08   0.29741E-09 0.60688E+00 
c  r13          0.46666E-02      18   0.71214E-08   0.14703E-08 0.19854E+00 
c  r23          0.39967E-02      19   0.60933E-08   0.12629E-08 0.19811E+00 
c  epsilon      0.10971E+02      11   0.33862E-08   0.97653E-02 0.16475E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.83610E-02 0.43152E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386          0.6135       0.0052532       0.0015071
v  Velocity[Y]            -0.57349         0.54401       0.0030775      0.00087296
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.461          360.03          87.641          169.85
v  r11                   0.0010594        0.081933        0.013068        0.018283
v  r22                   0.0011095        0.082626        0.013348        0.018643
v  r33                   0.0016335         0.17433        0.027238          0.0372
v  r12                   -0.010645        0.013603     -0.00023369     -0.00030925
v  r13                   -0.045556        0.052796      9.2598e-05       0.0010134
v  r23                   -0.046681        0.051215      2.9965e-05      0.00057429
v  epsilon                0.068572           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9761e-05       0.0099175      0.00092418       0.0017423
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2786          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71348         0.85282


 TIME FOR THE TIME STEP             9961:        0.79604E+02

===============================================================


 INSTANT    0.996200000E-02   TIME STEP NUMBER            9962
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.187598739E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.266055463E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934906E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.967453403E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319001081E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.184565510E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81286E-03   0.45474E-02 0.19971E+01 
c  Velocity[X]                                      0.14015E-03 
c  Velocity[Y]                                      0.13007E-03 
c  Velocity[Z]                                      0.42772E-02 
c  Pressure     0.36076E-04     133   0.91849E-02   0.25448E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55037E-08   0.16112E-08 0.99763E-01 
c  r22          0.10850E-01      13   0.57324E-08   0.18233E-08 0.10154E+00 
c  r33          0.21855E-01      15   0.55981E-08   0.12424E-07 0.12709E+00 
c  r12          0.93837E-03      18   0.51835E-08   0.29225E-09 0.60444E+00 
c  r13          0.46666E-02      18   0.68814E-08   0.15037E-08 0.19995E+00 
c  r23          0.39967E-02      19   0.60547E-08   0.12613E-08 0.19867E+00 
c  epsilon      0.10971E+02      11   0.34029E-08   0.99081E-02 0.16582E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.84221E-02 0.43290E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61347       0.0052532       0.0015071
v  Velocity[Y]            -0.57341         0.54405       0.0030776      0.00087295
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.458          360.04          87.675          169.87
v  r11                   0.0010594        0.081935        0.013068        0.018283
v  r22                   0.0011096        0.082626        0.013348        0.018643
v  r33                   0.0016335         0.17435        0.027238          0.0372
v  r12                   -0.010651        0.013605     -0.00023369     -0.00030925
v  r13                   -0.045554        0.052796      9.2601e-05       0.0010134
v  r23                    -0.04668        0.051216      2.9966e-05       0.0005743
v  epsilon                0.068572          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9763e-05       0.0099175      0.00092418       0.0017423
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2782         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71347         0.85282


 TIME FOR THE TIME STEP             9962:        0.80043E+02

===============================================================


 INSTANT    0.996300000E-02   TIME STEP NUMBER            9963
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158344879E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.765922754E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.317755193E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935014E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201897416E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.332473687E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      43   0.81201E-03   0.45487E-02 0.19980E+01 
c  Velocity[X]                                      0.14011E-03 
c  Velocity[Y]                                      0.12951E-03 
c  Velocity[Z]                                      0.42791E-02 
c  Pressure     0.36471E-04     132   0.92836E-02   0.25727E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54978E-08   0.16434E-08 0.10005E+00 
c  r22          0.10850E-01      13   0.53960E-08   0.18216E-08 0.10129E+00 
c  r33          0.21855E-01      15   0.56625E-08   0.12511E-07 0.12719E+00 
c  r12          0.93837E-03      17   0.69916E-08   0.29444E-09 0.60168E+00 
c  r13          0.46666E-02      19   0.57068E-08   0.14857E-08 0.19925E+00 
c  r23          0.39967E-02      19   0.64381E-08   0.12716E-08 0.19903E+00 
c  epsilon      0.10971E+02      11   0.33711E-08   0.10283E-01 0.16775E+00 
c  TempC        0.25716E+06      16   0.15106E-04   0.85581E-02 0.43638E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61345       0.0052532       0.0015071
v  Velocity[Y]            -0.57337         0.54422       0.0030776      0.00087295
v  Velocity[Z]              1.5652          5.4368          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4368          4.3406          4.3632
v  Pressure                -36.431          360.05           87.66          169.87
v  r11                   0.0010594        0.081942        0.013068        0.018283
v  r22                   0.0011096        0.082628        0.013348        0.018643
v  r33                   0.0016335         0.17439        0.027238          0.0372
v  r12                   -0.010646          0.0136     -0.00023369     -0.00030925
v  r13                   -0.045553        0.052796      9.2603e-05       0.0010134
v  r23                   -0.046679        0.051203      2.9968e-05       0.0005743
v  epsilon                0.068572          271.37          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9765e-05       0.0099175      0.00092419       0.0017423
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2783         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71348         0.85282


 TIME FOR THE TIME STEP             9963:        0.80647E+02

===============================================================


 INSTANT    0.996400000E-02   TIME STEP NUMBER            9964
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.137985341E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.397969643E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111424513E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.306900623E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.707132744E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81251E-03   0.45340E-02 0.19941E+01 
c  Velocity[X]                                      0.13865E-03 
c  Velocity[Y]                                      0.12944E-03 
c  Velocity[Z]                                      0.42659E-02 
c  Pressure     0.36693E-04     131   0.93480E-02   0.25884E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52647E-08   0.16589E-08 0.10081E+00 
c  r22          0.10850E-01      13   0.55963E-08   0.18396E-08 0.10223E+00 
c  r33          0.21855E-01      15   0.58877E-08   0.12666E-07 0.12853E+00 
c  r12          0.93837E-03      18   0.57516E-08   0.29441E-09 0.60553E+00 
c  r13          0.46666E-02      19   0.64405E-08   0.15040E-08 0.20098E+00 
c  r23          0.39967E-02      19   0.72592E-08   0.12985E-08 0.20118E+00 
c  epsilon      0.10971E+02      11   0.34076E-08   0.10117E-01 0.16807E+00 
c  TempC        0.25716E+06      16   0.15155E-04   0.84601E-02 0.43399E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338         0.61351       0.0052531       0.0015071
v  Velocity[Y]            -0.57346         0.54402       0.0030776      0.00087296
v  Velocity[Z]              1.5653          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4368          4.3406          4.3632
v  Pressure                -36.473          360.05          87.686          169.88
v  r11                   0.0010594        0.081947        0.013068        0.018283
v  r22                   0.0011096        0.082629        0.013348        0.018643
v  r33                   0.0016335         0.17437        0.027238          0.0372
v  r12                   -0.010645        0.013597     -0.00023369     -0.00030925
v  r13                   -0.045556        0.052794      9.2604e-05       0.0010134
v  r23                   -0.046678        0.051228      2.9968e-05       0.0005743
v  epsilon                0.068573          271.38          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9767e-05       0.0099174      0.00092419       0.0017423
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2778         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71348         0.85282


 TIME FOR THE TIME STEP             9964:        0.79750E+02

===============================================================


 INSTANT    0.996500000E-02   TIME STEP NUMBER            9965
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149322370E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.198517913E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.969814055E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.353070004E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.207753000E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      42   0.81156E-03   0.45583E-02 0.19980E+01 
c  Velocity[X]                                      0.13881E-03 
c  Velocity[Y]                                      0.12945E-03 
c  Velocity[Z]                                      0.42900E-02 
c  Pressure     0.36163E-04     132   0.92083E-02   0.25509E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.58053E-08   0.16329E-08 0.99842E-01 
c  r22          0.10850E-01      13   0.54534E-08   0.18452E-08 0.10199E+00 
c  r33          0.21855E-01      15   0.56197E-08   0.12577E-07 0.12745E+00 
c  r12          0.93837E-03      18   0.62480E-08   0.29178E-09 0.60388E+00 
c  r13          0.46666E-02      19   0.58908E-08   0.14958E-08 0.20003E+00 
c  r23          0.39967E-02      19   0.61712E-08   0.12755E-08 0.19857E+00 
c  epsilon      0.10971E+02      11   0.34205E-08   0.10163E-01 0.16765E+00 
c  TempC        0.25716E+06      16   0.15102E-04   0.83931E-02 0.43233E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61348       0.0052532       0.0015071
v  Velocity[Y]            -0.57341         0.54414       0.0030777      0.00087297
v  Velocity[Z]              1.5654          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4368          4.3406          4.3632
v  Pressure                -36.411          360.11          87.695          169.91
v  r11                   0.0010594        0.081959        0.013068        0.018283
v  r22                   0.0011096        0.082629        0.013348        0.018643
v  r33                   0.0016335         0.17434        0.027238          0.0372
v  r12                   -0.010648          0.0136     -0.00023369     -0.00030925
v  r13                   -0.045555        0.052792      9.2605e-05       0.0010134
v  r23                   -0.046678         0.05121      2.9969e-05       0.0005743
v  epsilon                0.068573          271.33          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9768e-05       0.0099175      0.00092419       0.0017423
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017899           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85282


 TIME FOR THE TIME STEP             9965:        0.80251E+02

===============================================================


 INSTANT    0.996600000E-02   TIME STEP NUMBER            9966
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.206332557E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.473251242E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.498165530E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190439917E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.331249430E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81221E-03   0.45639E-02 0.20028E+01 
c  Velocity[X]                                      0.14024E-03 
c  Velocity[Y]                                      0.13124E-03 
c  Velocity[Z]                                      0.42924E-02 
c  Pressure     0.36402E-04     132   0.92676E-02   0.25679E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50464E-08   0.16646E-08 0.10153E+00 
c  r22          0.10850E-01      13   0.55927E-08   0.18339E-08 0.10224E+00 
c  r33          0.21855E-01      15   0.53363E-08   0.12601E-07 0.12865E+00 
c  r12          0.93837E-03      18   0.58455E-08   0.29537E-09 0.60839E+00 
c  r13          0.46667E-02      19   0.57512E-08   0.14855E-08 0.20056E+00 
c  r23          0.39967E-02      19   0.61855E-08   0.12961E-08 0.20236E+00 
c  epsilon      0.10971E+02      11   0.32949E-08   0.10205E-01 0.17302E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.84195E-02 0.43280E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61345       0.0052533       0.0015072
v  Velocity[Y]            -0.57347         0.54428       0.0030776      0.00087297
v  Velocity[Z]              1.5654          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4368          4.3406          4.3632
v  Pressure                -36.478          360.01          87.655          169.84
v  r11                   0.0010594        0.081958        0.013068        0.018283
v  r22                   0.0011096        0.082628        0.013348        0.018643
v  r33                   0.0016336         0.17435        0.027238          0.0372
v  r12                   -0.010651        0.013599     -0.00023369     -0.00030925
v  r13                   -0.045553        0.052793      9.2607e-05       0.0010134
v  r23                   -0.046678        0.051193       2.997e-05       0.0005743
v  epsilon                0.068573          271.34          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9768e-05       0.0099175      0.00092419       0.0017423
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2782          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71348         0.85283


 TIME FOR THE TIME STEP             9966:        0.77419E+02

===============================================================


 INSTANT    0.996700000E-02   TIME STEP NUMBER            9967
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.362388835E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.193649489E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.141853080E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.176921506E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.594450008E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36447E+01      41   0.81172E-03   0.45235E-02 0.19925E+01 
c  Velocity[X]                                      0.13965E-03 
c  Velocity[Y]                                      0.12990E-03 
c  Velocity[Z]                                      0.42539E-02 
c  Pressure     0.36119E-04     132   0.92048E-02   0.25477E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50288E-08   0.16150E-08 0.99943E-01 
c  r22          0.10850E-01      13   0.52239E-08   0.18295E-08 0.10203E+00 
c  r33          0.21855E-01      15   0.52706E-08   0.12438E-07 0.12749E+00 
c  r12          0.93837E-03      18   0.55247E-08   0.29149E-09 0.60312E+00 
c  r13          0.46667E-02      19   0.54523E-08   0.14990E-08 0.20072E+00 
c  r23          0.39967E-02      19   0.61700E-08   0.12584E-08 0.19806E+00 
c  epsilon      0.10971E+02      11   0.33273E-08   0.99099E-02 0.16557E+00 
c  TempC        0.25716E+06      16   0.15108E-04   0.84837E-02 0.43435E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61351       0.0052532       0.0015071
v  Velocity[Y]            -0.57331         0.54403       0.0030776      0.00087295
v  Velocity[Z]              1.5652          5.4368          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4368          4.3406          4.3632
v  Pressure                -36.426          359.99           87.62          169.82
v  r11                   0.0010594        0.081952        0.013068        0.018283
v  r22                   0.0011096        0.082627        0.013348        0.018643
v  r33                   0.0016336         0.17438        0.027238          0.0372
v  r12                    -0.01065        0.013605      -0.0002337     -0.00030925
v  r13                   -0.045555        0.052792      9.2609e-05       0.0010134
v  r23                   -0.046678        0.051211      2.9971e-05       0.0005743
v  epsilon                0.068573          271.38          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9766e-05       0.0099176      0.00092419       0.0017423
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017899           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85282


 TIME FOR THE TIME STEP             9967:        0.81748E+02

===============================================================


 INSTANT    0.996800000E-02   TIME STEP NUMBER            9968
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.250114735E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.116283145E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934901E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.163079630E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.719470458E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.398628410E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81237E-03   0.45450E-02 0.19970E+01 
c  Velocity[X]                                      0.13900E-03 
c  Velocity[Y]                                      0.12922E-03 
c  Velocity[Z]                                      0.42768E-02 
c  Pressure     0.36818E-04     133   0.93809E-02   0.25972E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57499E-08   0.16405E-08 0.10048E+00 
c  r22          0.10850E-01      13   0.53630E-08   0.18243E-08 0.10198E+00 
c  r33          0.21855E-01      15   0.56210E-08   0.12436E-07 0.12779E+00 
c  r12          0.93837E-03      18   0.63550E-08   0.29829E-09 0.60895E+00 
c  r13          0.46667E-02      19   0.53751E-08   0.14867E-08 0.20047E+00 
c  r23          0.39967E-02      19   0.57451E-08   0.12702E-08 0.19940E+00 
c  epsilon      0.10971E+02      11   0.34148E-08   0.97046E-02 0.16395E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.84436E-02 0.43364E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61347       0.0052532       0.0015072
v  Velocity[Y]            -0.57337         0.54404       0.0030776      0.00087299
v  Velocity[Z]               1.565          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4368          4.3406          4.3632
v  Pressure                -36.458          360.05          87.687          169.88
v  r11                   0.0010594        0.081935        0.013068        0.018283
v  r22                   0.0011096        0.082627        0.013348        0.018643
v  r33                   0.0016336         0.17437        0.027238          0.0372
v  r12                   -0.010648        0.013602      -0.0002337     -0.00030925
v  r13                   -0.045553        0.052793       9.261e-05       0.0010134
v  r23                   -0.046678        0.051196      2.9972e-05       0.0005743
v  epsilon                0.068574          271.37          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9764e-05       0.0099176      0.00092419       0.0017423
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85282


 TIME FOR THE TIME STEP             9968:        0.81134E+02

===============================================================


 INSTANT    0.996900000E-02   TIME STEP NUMBER            9969
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155641595E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171967897E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.220057886E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140586689E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.132837629E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69806E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81196E-03   0.45792E-02 0.20041E+01 
c  Velocity[X]                                      0.14049E-03 
c  Velocity[Y]                                      0.13020E-03 
c  Velocity[Z]                                      0.43085E-02 
c  Pressure     0.36838E-04     133   0.93804E-02   0.25986E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52809E-08   0.16449E-08 0.10007E+00 
c  r22          0.10850E-01      13   0.51459E-08   0.18222E-08 0.10173E+00 
c  r33          0.21855E-01      14   0.71289E-08   0.12558E-07 0.12765E+00 
c  r12          0.93837E-03      18   0.57820E-08   0.29640E-09 0.60553E+00 
c  r13          0.46667E-02      18   0.72390E-08   0.15005E-08 0.20050E+00 
c  r23          0.39967E-02      19   0.54529E-08   0.12855E-08 0.19916E+00 
c  epsilon      0.10971E+02      11   0.34720E-08   0.10113E-01 0.16754E+00 
c  TempC        0.25716E+06      16   0.15120E-04   0.84591E-02 0.43411E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61344       0.0052532       0.0015072
v  Velocity[Y]             -0.5734         0.54412       0.0030776      0.00087299
v  Velocity[Z]              1.5652          5.4368          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4368          4.3406          4.3632
v  Pressure                -36.399          360.08          87.686          169.91
v  r11                   0.0010594        0.081917        0.013068        0.018283
v  r22                   0.0011096        0.082623        0.013348        0.018643
v  r33                   0.0016336         0.17435        0.027238        0.037201
v  r12                   -0.010648        0.013607      -0.0002337     -0.00030925
v  r13                   -0.045554        0.052794      9.2612e-05       0.0010135
v  r23                   -0.046678        0.051188      2.9972e-05       0.0005743
v  epsilon                0.068574          271.34          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9762e-05       0.0099176      0.00092419       0.0017423
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2776          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71348         0.85283


 TIME FOR THE TIME STEP             9969:        0.81461E+02

===============================================================


 INSTANT    0.997000000E-02   TIME STEP NUMBER            9970
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.397884079E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.504828651E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199897568E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.392126607E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.489382559E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81210E-03   0.45428E-02 0.19956E+01 
c  Velocity[X]                                      0.13881E-03 
c  Velocity[Y]                                      0.12976E-03 
c  Velocity[Z]                                      0.42742E-02 
c  Pressure     0.36363E-04     133   0.92573E-02   0.25650E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50433E-08   0.16621E-08 0.10045E+00 
c  r22          0.10850E-01      13   0.47810E-08   0.18518E-08 0.10204E+00 
c  r33          0.21855E-01      15   0.51990E-08   0.12801E-07 0.12860E+00 
c  r12          0.93837E-03      18   0.54626E-08   0.29759E-09 0.60618E+00 
c  r13          0.46667E-02      19   0.56111E-08   0.15136E-08 0.20078E+00 
c  r23          0.39967E-02      19   0.55859E-08   0.13012E-08 0.20081E+00 
c  epsilon      0.10971E+02      11   0.35197E-08   0.10509E-01 0.17064E+00 
c  TempC        0.25716E+06      16   0.15105E-04   0.83901E-02 0.43221E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391          0.6135       0.0052533       0.0015072
v  Velocity[Y]            -0.57361         0.54421       0.0030776      0.00087299
v  Velocity[Z]              1.5652          5.4368          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4368          4.3406          4.3632
v  Pressure                -36.505          360.02          87.667          169.86
v  r11                   0.0010594        0.081906        0.013068        0.018283
v  r22                   0.0011096        0.082625        0.013348        0.018643
v  r33                   0.0016336         0.17435        0.027238        0.037201
v  r12                   -0.010651        0.013599      -0.0002337     -0.00030925
v  r13                   -0.045556        0.052796      9.2613e-05       0.0010135
v  r23                   -0.046678        0.051214      2.9973e-05       0.0005743
v  epsilon                0.068574          271.35          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9761e-05       0.0099175       0.0009242       0.0017423
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2775         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71348         0.85282


 TIME FOR THE TIME STEP             9970:        0.78169E+02

===============================================================


 INSTANT    0.997100000E-02   TIME STEP NUMBER            9971
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.435281390E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120296826E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.158423251E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191917413E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.591335686E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81119E-03   0.45667E-02 0.20001E+01 
c  Velocity[X]                                      0.14004E-03 
c  Velocity[Y]                                      0.12955E-03 
c  Velocity[Z]                                      0.42971E-02 
c  Pressure     0.36543E-04     133   0.92993E-02   0.25778E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50920E-08   0.16468E-08 0.10025E+00 
c  r22          0.10850E-01      13   0.48761E-08   0.18304E-08 0.10178E+00 
c  r33          0.21855E-01      15   0.64909E-08   0.12532E-07 0.12791E+00 
c  r12          0.93837E-03      18   0.52491E-08   0.29795E-09 0.60635E+00 
c  r13          0.46667E-02      19   0.53964E-08   0.15060E-08 0.20024E+00 
c  r23          0.39967E-02      19   0.59634E-08   0.12908E-08 0.20053E+00 
c  epsilon      0.10971E+02      11   0.35600E-08   0.98691E-02 0.16593E+00 
c  TempC        0.25716E+06      16   0.15108E-04   0.84255E-02 0.43310E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61348       0.0052533       0.0015072
v  Velocity[Y]            -0.57344         0.54402       0.0030777      0.00087303
v  Velocity[Z]              1.5653          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4368          4.3406          4.3632
v  Pressure                -36.418          360.06          87.668          169.88
v  r11                   0.0010594        0.081895        0.013068        0.018283
v  r22                   0.0011097        0.082627        0.013348        0.018643
v  r33                   0.0016336         0.17437        0.027238        0.037201
v  r12                   -0.010654        0.013602      -0.0002337     -0.00030925
v  r13                   -0.045554        0.052797      9.2615e-05       0.0010135
v  r23                   -0.046679        0.051201      2.9974e-05       0.0005743
v  epsilon                0.068575          271.37          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9761e-05       0.0099174       0.0009242       0.0017423
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2772         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71347         0.85282


 TIME FOR THE TIME STEP             9971:        0.80238E+02

===============================================================


 INSTANT    0.997200000E-02   TIME STEP NUMBER            9972
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.132252122E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106784949E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.210339324E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.407586985E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168534168E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81210E-03   0.45587E-02 0.19992E+01 
c  Velocity[X]                                      0.14054E-03 
c  Velocity[Y]                                      0.13051E-03 
c  Velocity[Z]                                      0.42876E-02 
c  Pressure     0.36471E-04     134   0.92895E-02   0.25727E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54401E-08   0.17061E-08 0.10212E+00 
c  r22          0.10850E-01      13   0.48347E-08   0.18716E-08 0.10291E+00 
c  r33          0.21855E-01      15   0.62683E-08   0.13042E-07 0.13049E+00 
c  r12          0.93837E-03      18   0.53938E-08   0.30924E-09 0.61669E+00 
c  r13          0.46667E-02      18   0.63445E-08   0.15426E-08 0.20262E+00 
c  r23          0.39967E-02      18   0.67347E-08   0.13409E-08 0.20462E+00 
c  epsilon      0.10971E+02      11   0.34767E-08   0.10641E-01 0.17444E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.84576E-02 0.43403E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61344       0.0052533       0.0015072
v  Velocity[Y]            -0.57354         0.54416       0.0030777      0.00087303
v  Velocity[Z]              1.5654          5.4368          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4368          4.3406          4.3632
v  Pressure                -36.461          360.06          87.687          169.89
v  r11                   0.0010594        0.081886        0.013068        0.018283
v  r22                   0.0011097         0.08263        0.013348        0.018643
v  r33                   0.0016336         0.17436        0.027238        0.037201
v  r12                   -0.010659        0.013607      -0.0002337     -0.00030925
v  r13                   -0.045552        0.052798      9.2617e-05       0.0010135
v  r23                   -0.046679        0.051188      2.9975e-05       0.0005743
v  epsilon                0.068575          271.35          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.976e-05       0.0099175       0.0009242       0.0017423
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2775         0.11439         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71348         0.85282


 TIME FOR THE TIME STEP             9972:        0.85394E+02

===============================================================


 INSTANT    0.997300000E-02   TIME STEP NUMBER            9973
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.264982519E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.876892891E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.542714819E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.249809127E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.885996962E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81216E-03   0.45518E-02 0.19953E+01 
c  Velocity[X]                                      0.13970E-03 
c  Velocity[Y]                                      0.12952E-03 
c  Velocity[Z]                                      0.42826E-02 
c  Pressure     0.36345E-04     133   0.92544E-02   0.25638E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.49761E-08   0.16668E-08 0.10072E+00 
c  r22          0.10850E-01      13   0.48067E-08   0.18806E-08 0.10261E+00 
c  r33          0.21855E-01      15   0.63812E-08   0.12798E-07 0.12880E+00 
c  r12          0.93837E-03      18   0.49232E-08   0.30805E-09 0.61192E+00 
c  r13          0.46667E-02      19   0.56895E-08   0.15210E-08 0.20165E+00 
c  r23          0.39967E-02      19   0.62204E-08   0.13043E-08 0.20073E+00 
c  epsilon      0.10971E+02      11   0.34016E-08   0.10523E-01 0.16983E+00 
c  TempC        0.25716E+06      16   0.15101E-04   0.84039E-02 0.43279E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61349       0.0052533       0.0015072
v  Velocity[Y]            -0.57356         0.54417       0.0030777      0.00087302
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.451          360.02           87.64          169.85
v  r11                   0.0010594        0.081872        0.013068        0.018283
v  r22                   0.0011097        0.082632        0.013348        0.018643
v  r33                   0.0016337         0.17433        0.027238        0.037201
v  r12                    -0.01066        0.013607      -0.0002337     -0.00030925
v  r13                   -0.045556        0.052797      9.2618e-05       0.0010135
v  r23                   -0.046679         0.05119      2.9975e-05       0.0005743
v  epsilon                0.068575          271.34          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9757e-05       0.0099175       0.0009242       0.0017423
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2768          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71348         0.85282


 TIME FOR THE TIME STEP             9973:        0.80926E+02

===============================================================


 INSTANT    0.997400000E-02   TIME STEP NUMBER            9974
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.496162817E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.297650250E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.526749699E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.192689411E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934918E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232636822E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81213E-03   0.45361E-02 0.19945E+01 
c  Velocity[X]                                      0.13958E-03 
c  Velocity[Y]                                      0.12938E-03 
c  Velocity[Z]                                      0.42672E-02 
c  Pressure     0.36367E-04     133   0.92565E-02   0.25654E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.48638E-08   0.16297E-08 0.10012E+00 
c  r22          0.10850E-01      13   0.52280E-08   0.17976E-08 0.10116E+00 
c  r33          0.21855E-01      15   0.58328E-08   0.12286E-07 0.12694E+00 
c  r12          0.93837E-03      17   0.67433E-08   0.28791E-09 0.60275E+00 
c  r13          0.46667E-02      18   0.71594E-08   0.14619E-08 0.19916E+00 
c  r23          0.39967E-02      19   0.65630E-08   0.12642E-08 0.19861E+00 
c  epsilon      0.10971E+02      11   0.33526E-08   0.96499E-02 0.16262E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.84695E-02 0.43355E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61345       0.0052533       0.0015072
v  Velocity[Y]            -0.57372         0.54426       0.0030777      0.00087305
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.473          359.98          87.651          169.83
v  r11                   0.0010594        0.081867        0.013068        0.018283
v  r22                   0.0011097        0.082632        0.013348        0.018643
v  r33                   0.0016337         0.17434        0.027238        0.037201
v  r12                   -0.010663        0.013603      -0.0002337     -0.00030925
v  r13                   -0.045553        0.052799      9.2621e-05       0.0010135
v  r23                   -0.046679        0.051212      2.9976e-05      0.00057431
v  epsilon                0.068575          271.33          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9754e-05       0.0099175       0.0009242       0.0017423
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2763          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8763         0.71348         0.85282


 TIME FOR THE TIME STEP             9974:        0.82253E+02

===============================================================


 INSTANT    0.997500000E-02   TIME STEP NUMBER            9975
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.488093118E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149673025E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.134588869E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107732245E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.135525985E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81137E-03   0.45282E-02 0.19929E+01 
c  Velocity[X]                                      0.13940E-03 
c  Velocity[Y]                                      0.12959E-03 
c  Velocity[Z]                                      0.42592E-02 
c  Pressure     0.36475E-04     131   0.92844E-02   0.25729E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.48268E-08   0.16574E-08 0.10074E+00 
c  r22          0.10850E-01      13   0.49217E-08   0.18183E-08 0.10194E+00 
c  r33          0.21855E-01      14   0.69984E-08   0.12537E-07 0.12822E+00 
c  r12          0.93837E-03      17   0.69231E-08   0.29523E-09 0.60599E+00 
c  r13          0.46667E-02      18   0.71490E-08   0.14704E-08 0.19960E+00 
c  r23          0.39967E-02      19   0.69837E-08   0.12819E-08 0.19987E+00 
c  epsilon      0.10971E+02      11   0.35158E-08   0.99502E-02 0.16612E+00 
c  TempC        0.25716E+06      16   0.15091E-04   0.84731E-02 0.43426E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61351       0.0052533       0.0015072
v  Velocity[Y]             -0.5736         0.54438       0.0030778      0.00087307
v  Velocity[Z]               1.565          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4369          4.3406          4.3632
v  Pressure                -36.406          360.05          87.664          169.88
v  r11                   0.0010595         0.08186        0.013068        0.018283
v  r22                   0.0011097        0.082633        0.013348        0.018643
v  r33                   0.0016337         0.17437        0.027238        0.037201
v  r12                   -0.010661        0.013599      -0.0002337     -0.00030925
v  r13                   -0.045553        0.052799      9.2622e-05       0.0010135
v  r23                    -0.04668        0.051204      2.9976e-05      0.00057431
v  epsilon                0.068576          271.35          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9749e-05       0.0099175       0.0009242       0.0017423
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2764         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7406e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8764         0.71348         0.85282


 TIME FOR THE TIME STEP             9975:        0.78170E+02

===============================================================


 INSTANT    0.997600000E-02   TIME STEP NUMBER            9976
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.829242358E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.191593593E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168379469E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.132504884E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.584135463E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81260E-03   0.45587E-02 0.19988E+01 
c  Velocity[X]                                      0.13908E-03 
c  Velocity[Y]                                      0.13008E-03 
c  Velocity[Z]                                      0.42896E-02 
c  Pressure     0.36700E-04     132   0.93421E-02   0.25890E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50125E-08   0.16286E-08 0.10032E+00 
c  r22          0.10850E-01      13   0.51270E-08   0.18096E-08 0.10181E+00 
c  r33          0.21856E-01      15   0.51188E-08   0.12393E-07 0.12761E+00 
c  r12          0.93838E-03      17   0.68456E-08   0.29405E-09 0.60821E+00 
c  r13          0.46667E-02      19   0.56248E-08   0.14721E-08 0.19933E+00 
c  r23          0.39967E-02      19   0.59132E-08   0.12686E-08 0.19915E+00 
c  epsilon      0.10971E+02      11   0.33910E-08   0.98523E-02 0.16593E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83822E-02 0.43243E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392          0.6135       0.0052534       0.0015072
v  Velocity[Y]            -0.57365         0.54419       0.0030777      0.00087306
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.496             360          87.643          169.84
v  r11                   0.0010595        0.081856        0.013068        0.018283
v  r22                   0.0011097        0.082634        0.013348        0.018643
v  r33                   0.0016337         0.17434        0.027238        0.037201
v  r12                   -0.010659        0.013596      -0.0002337     -0.00030925
v  r13                   -0.045556          0.0528      9.2624e-05       0.0010135
v  r23                    -0.04668        0.051189      2.9978e-05      0.00057431
v  epsilon                0.068576          271.35          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9744e-05       0.0099175       0.0009242       0.0017423
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2769         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71347         0.85282


 TIME FOR THE TIME STEP             9976:        0.78225E+02

===============================================================


 INSTANT    0.997700000E-02   TIME STEP NUMBER            9977
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.449357480E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.120810545E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.267447259E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.307670796E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.220012178E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81122E-03   0.45825E-02 0.20045E+01 
c  Velocity[X]                                      0.13970E-03 
c  Velocity[Y]                                      0.13012E-03 
c  Velocity[Z]                                      0.43127E-02 
c  Pressure     0.36727E-04     131   0.93545E-02   0.25908E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.56227E-08   0.16486E-08 0.10034E+00 
c  r22          0.10850E-01      13   0.48017E-08   0.18463E-08 0.10216E+00 
c  r33          0.21856E-01      14   0.67931E-08   0.12598E-07 0.12801E+00 
c  r12          0.93838E-03      18   0.49237E-08   0.30128E-09 0.61277E+00 
c  r13          0.46667E-02      19   0.60088E-08   0.15073E-08 0.20045E+00 
c  r23          0.39967E-02      19   0.56716E-08   0.12803E-08 0.19923E+00 
c  epsilon      0.10971E+02      11   0.31565E-08   0.10104E-01 0.16631E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.84321E-02 0.43315E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61347       0.0052534       0.0015072
v  Velocity[Y]            -0.57368         0.54413       0.0030778      0.00087308
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.432          360.04          87.638          169.85
v  r11                   0.0010595        0.081857        0.013068        0.018283
v  r22                   0.0011097         0.08263        0.013348        0.018643
v  r33                   0.0016337         0.17432        0.027238        0.037201
v  r12                   -0.010661        0.013597      -0.0002337     -0.00030925
v  r13                   -0.045555        0.052799      9.2625e-05       0.0010135
v  r23                    -0.04668         0.05121      2.9978e-05      0.00057431
v  epsilon                0.068576          271.32          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9739e-05       0.0099176      0.00092421       0.0017423
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2776         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71348         0.85282


 TIME FOR THE TIME STEP             9977:        0.76784E+02

===============================================================


 INSTANT    0.997800000E-02   TIME STEP NUMBER            9978
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.407145113E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181037530E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.403490852E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.124684239E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.326990691E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      44   0.81212E-03   0.45483E-02 0.19985E+01 
c  Velocity[X]                                      0.13954E-03 
c  Velocity[Y]                                      0.13023E-03 
c  Velocity[Z]                                      0.42785E-02 
c  Pressure     0.36352E-04     133   0.92602E-02   0.25644E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55617E-08   0.16808E-08 0.10148E+00 
c  r22          0.10850E-01      13   0.51037E-08   0.18509E-08 0.10237E+00 
c  r33          0.21856E-01      15   0.62230E-08   0.12804E-07 0.12936E+00 
c  r12          0.93838E-03      18   0.57374E-08   0.31099E-09 0.61956E+00 
c  r13          0.46667E-02      19   0.73591E-08   0.15063E-08 0.20082E+00 
c  r23          0.39967E-02      19   0.61784E-08   0.13313E-08 0.20457E+00 
c  epsilon      0.10971E+02      11   0.31882E-08   0.10259E-01 0.17154E+00 
c  TempC        0.25716E+06      16   0.15125E-04   0.84905E-02 0.43392E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63399         0.61351       0.0052534       0.0015072
v  Velocity[Y]            -0.57369         0.54424       0.0030779      0.00087309
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.468          360.03          87.659          169.85
v  r11                   0.0010595        0.081858        0.013068        0.018283
v  r22                   0.0011097        0.082631        0.013348        0.018643
v  r33                   0.0016337         0.17434        0.027238        0.037201
v  r12                   -0.010671        0.013598      -0.0002337     -0.00030925
v  r13                   -0.045553        0.052799      9.2626e-05       0.0010135
v  r23                   -0.046681        0.051205      2.9979e-05      0.00057431
v  epsilon                0.068576          271.33          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9733e-05       0.0099175      0.00092421       0.0017423
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2779          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71348         0.85282


 TIME FOR THE TIME STEP             9978:        0.79403E+02

===============================================================


 INSTANT    0.997900000E-02   TIME STEP NUMBER            9979
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.301595670E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.358445956E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.164918621E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.378587934E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239190190E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      40   0.81203E-03   0.45397E-02 0.19945E+01 
c  Velocity[X]                                      0.13911E-03 
c  Velocity[Y]                                      0.12945E-03 
c  Velocity[Z]                                      0.42712E-02 
c  Pressure     0.36369E-04     133   0.92607E-02   0.25654E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52128E-08   0.16579E-08 0.10097E+00 
c  r22          0.10850E-01      13   0.50303E-08   0.18324E-08 0.10211E+00 
c  r33          0.21856E-01      15   0.58828E-08   0.12536E-07 0.12811E+00 
c  r12          0.93838E-03      18   0.51045E-08   0.30262E-09 0.61561E+00 
c  r13          0.46667E-02      19   0.60834E-08   0.15006E-08 0.20004E+00 
c  r23          0.39967E-02      19   0.54441E-08   0.12961E-08 0.20141E+00 
c  epsilon      0.10971E+02      11   0.32567E-08   0.96252E-02 0.16284E+00 
c  TempC        0.25716E+06      16   0.15110E-04   0.84560E-02 0.43415E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61348       0.0052533       0.0015072
v  Velocity[Y]            -0.57366         0.54432       0.0030778      0.00087305
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.469          360.08          87.667          169.89
v  r11                   0.0010595        0.081874        0.013068        0.018283
v  r22                   0.0011098        0.082632        0.013348        0.018643
v  r33                   0.0016338         0.17436        0.027238        0.037201
v  r12                   -0.010674        0.013603      -0.0002337     -0.00030925
v  r13                   -0.045556        0.052798      9.2627e-05       0.0010135
v  r23                   -0.046681        0.051189       2.998e-05      0.00057431
v  epsilon                0.068577          271.37          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9727e-05       0.0099176      0.00092421       0.0017424
v  CourantNb               0.44263             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2778          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71348         0.85282


 TIME FOR THE TIME STEP             9979:        0.79667E+02

===============================================================


 INSTANT    0.998000000E-02   TIME STEP NUMBER            9980
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.380407852E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.135530370E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283509514E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.265355897E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.187040611E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81240E-03   0.45718E-02 0.20040E+01 
c  Velocity[X]                                      0.14020E-03 
c  Velocity[Y]                                      0.13033E-03 
c  Velocity[Z]                                      0.43013E-02 
c  Pressure     0.36637E-04     133   0.93348E-02   0.25845E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50573E-08   0.16411E-08 0.10029E+00 
c  r22          0.10850E-01      13   0.50029E-08   0.18262E-08 0.10178E+00 
c  r33          0.21856E-01      15   0.54360E-08   0.12451E-07 0.12738E+00 
c  r12          0.93838E-03      17   0.69515E-08   0.29607E-09 0.60894E+00 
c  r13          0.46667E-02      19   0.54825E-08   0.14888E-08 0.20024E+00 
c  r23          0.39967E-02      19   0.57448E-08   0.12577E-08 0.19809E+00 
c  epsilon      0.10971E+02      11   0.34469E-08   0.98768E-02 0.16489E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.84283E-02 0.43343E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61342       0.0052533       0.0015072
v  Velocity[Y]            -0.57378         0.54412       0.0030778      0.00087307
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.438          360.02          87.656          169.84
v  r11                   0.0010595        0.081882        0.013068        0.018283
v  r22                   0.0011098        0.082633        0.013348        0.018643
v  r33                   0.0016338         0.17439        0.027238        0.037201
v  r12                   -0.010676        0.013606      -0.0002337     -0.00030925
v  r13                   -0.045553        0.052799      9.2629e-05       0.0010135
v  r23                   -0.046681        0.051211      2.9981e-05      0.00057431
v  epsilon                0.068577          271.38          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9722e-05       0.0099176      0.00092421       0.0017424
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb               0.00179           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85283


 TIME FOR THE TIME STEP             9980:        0.77175E+02

===============================================================


 INSTANT    0.998100000E-02   TIME STEP NUMBER            9981
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.147792376E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.866402671E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.617674807E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.152728207E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.968334168E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81161E-03   0.45602E-02 0.20015E+01 
c  Velocity[X]                                      0.13975E-03 
c  Velocity[Y]                                      0.12984E-03 
c  Velocity[Z]                                      0.42906E-02 
c  Pressure     0.36222E-04     132   0.92242E-02   0.25552E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.51035E-08   0.16666E-08 0.10123E+00 
c  r22          0.10850E-01      13   0.52281E-08   0.18179E-08 0.10157E+00 
c  r33          0.21856E-01      15   0.56642E-08   0.12512E-07 0.12810E+00 
c  r12          0.93838E-03      18   0.53262E-08   0.30343E-09 0.61404E+00 
c  r13          0.46667E-02      19   0.58547E-08   0.14880E-08 0.19966E+00 
c  r23          0.39967E-02      19   0.58213E-08   0.12891E-08 0.20087E+00 
c  epsilon      0.10971E+02      11   0.34624E-08   0.97929E-02 0.16502E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.84057E-02 0.43272E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61348       0.0052534       0.0015072
v  Velocity[Y]             -0.5737         0.54426       0.0030779      0.00087311
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.441          360.02          87.647          169.85
v  r11                   0.0010595        0.081883        0.013068        0.018283
v  r22                   0.0011098        0.082634        0.013348        0.018643
v  r33                   0.0016338         0.17438        0.027238        0.037201
v  r12                   -0.010673        0.013607      -0.0002337     -0.00030925
v  r13                   -0.045554        0.052797       9.263e-05       0.0010135
v  r23                   -0.046682        0.051202      2.9982e-05      0.00057431
v  epsilon                0.068577          271.39          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9719e-05       0.0099175      0.00092421       0.0017424
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2784          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71348         0.85282


 TIME FOR THE TIME STEP             9981:        0.78741E+02

===============================================================


 INSTANT    0.998200000E-02   TIME STEP NUMBER            9982
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.146242614E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.838014249E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.112310902E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.318578791E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.662325595E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      45   0.81200E-03   0.45289E-02 0.19922E+01 
c  Velocity[X]                                      0.13864E-03 
c  Velocity[Y]                                      0.12949E-03 
c  Velocity[Z]                                      0.42608E-02 
c  Pressure     0.36438E-04     133   0.92799E-02   0.25704E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.53584E-08   0.16371E-08 0.10019E+00 
c  r22          0.10850E-01      13   0.52489E-08   0.18210E-08 0.10154E+00 
c  r33          0.21856E-01      15   0.55051E-08   0.12531E-07 0.12783E+00 
c  r12          0.93838E-03      18   0.54031E-08   0.29246E-09 0.60704E+00 
c  r13          0.46667E-02      19   0.56977E-08   0.14874E-08 0.19967E+00 
c  r23          0.39967E-02      19   0.53326E-08   0.12842E-08 0.19993E+00 
c  epsilon      0.10971E+02      11   0.34057E-08   0.10016E-01 0.16741E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.83597E-02 0.43078E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61346       0.0052534       0.0015072
v  Velocity[Y]            -0.57378         0.54441       0.0030779       0.0008731
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.459          360.05          87.669          169.87
v  r11                   0.0010595        0.081884        0.013068        0.018283
v  r22                   0.0011098        0.082634        0.013348        0.018643
v  r33                   0.0016338         0.17435        0.027238        0.037201
v  r12                   -0.010672        0.013609      -0.0002337     -0.00030925
v  r13                   -0.045556        0.052797      9.2632e-05       0.0010135
v  r23                   -0.046682        0.051174      2.9983e-05      0.00057431
v  epsilon                0.068577          271.35          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9719e-05       0.0099176      0.00092421       0.0017424
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2784          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71348         0.85283


 TIME FOR THE TIME STEP             9982:        0.78566E+02

===============================================================


 INSTANT    0.998300000E-02   TIME STEP NUMBER            9983
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.149339036E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.147924760E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.143049862E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.266297024E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.124728625E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      44   0.81140E-03   0.45701E-02 0.20010E+01 
c  Velocity[X]                                      0.13961E-03 
c  Velocity[Y]                                      0.13021E-03 
c  Velocity[Z]                                      0.43003E-02 
c  Pressure     0.36489E-04     133   0.92926E-02   0.25740E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55772E-08   0.16291E-08 0.99651E-01 
c  r22          0.10850E-01      13   0.53568E-08   0.18180E-08 0.10140E+00 
c  r33          0.21856E-01      15   0.54070E-08   0.12441E-07 0.12681E+00 
c  r12          0.93838E-03      18   0.54042E-08   0.30125E-09 0.61165E+00 
c  r13          0.46667E-02      19   0.61173E-08   0.14891E-08 0.19933E+00 
c  r23          0.39967E-02      19   0.56288E-08   0.12816E-08 0.19871E+00 
c  epsilon      0.10971E+02      11   0.32763E-08   0.99264E-02 0.16555E+00 
c  TempC        0.25716E+06      16   0.15103E-04   0.85201E-02 0.43561E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61345       0.0052533       0.0015072
v  Velocity[Y]            -0.57372          0.5441       0.0030779       0.0008731
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.432          360.04          87.649          169.86
v  r11                   0.0010595         0.08188        0.013068        0.018283
v  r22                   0.0011098        0.082633        0.013348        0.018643
v  r33                   0.0016338         0.17436        0.027238        0.037201
v  r12                    -0.01067        0.013611      -0.0002337     -0.00030925
v  r13                   -0.045553        0.052797      9.2633e-05       0.0010135
v  r23                   -0.046682        0.051199      2.9983e-05      0.00057431
v  epsilon                0.068577          271.36          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9722e-05       0.0099179      0.00092421       0.0017424
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2783          0.1144         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71348         0.85282


 TIME FOR THE TIME STEP             9983:        0.78782E+02

===============================================================


 INSTANT    0.998400000E-02   TIME STEP NUMBER            9984
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.465708223E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.306142053E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116584688E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.100022163E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.389388151E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81243E-03   0.45481E-02 0.19979E+01 
c  Velocity[X]                                      0.14053E-03 
c  Velocity[Y]                                      0.13026E-03 
c  Velocity[Z]                                      0.42773E-02 
c  Pressure     0.36708E-04     133   0.93434E-02   0.25895E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54342E-08   0.16679E-08 0.10108E+00 
c  r22          0.10850E-01      13   0.54588E-08   0.18429E-08 0.10230E+00 
c  r33          0.21856E-01      15   0.57248E-08   0.12628E-07 0.12831E+00 
c  r12          0.93838E-03      18   0.62593E-08   0.30829E-09 0.61770E+00 
c  r13          0.46667E-02      19   0.59431E-08   0.15116E-08 0.20112E+00 
c  r23          0.39967E-02      19   0.55804E-08   0.13041E-08 0.20214E+00 
c  epsilon      0.10971E+02      11   0.33656E-08   0.10274E-01 0.17152E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.84762E-02 0.43391E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63395         0.61346       0.0052534       0.0015072
v  Velocity[Y]             -0.5738         0.54412       0.0030779      0.00087307
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.499          360.06          87.685          169.89
v  r11                   0.0010595        0.081879        0.013068        0.018283
v  r22                   0.0011098        0.082629        0.013348        0.018643
v  r33                   0.0016338         0.17439        0.027238        0.037201
v  r12                   -0.010669        0.013606      -0.0002337     -0.00030925
v  r13                   -0.045553        0.052799      9.2634e-05       0.0010135
v  r23                   -0.046683         0.05119      2.9984e-05      0.00057431
v  epsilon                0.068578          271.39          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9723e-05       0.0099182      0.00092421       0.0017424
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb               0.00179           5.278         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71347         0.85282


 TIME FOR THE TIME STEP             9984:        0.80291E+02

===============================================================


 INSTANT    0.998500000E-02   TIME STEP NUMBER            9985
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.109738004E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117230824E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.809564357E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100751579E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129492102E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81084E-03   0.45180E-02 0.19923E+01 
c  Velocity[X]                                      0.13869E-03 
c  Velocity[Y]                                      0.12949E-03 
c  Velocity[Z]                                      0.42498E-02 
c  Pressure     0.36198E-04     132   0.92142E-02   0.25533E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57636E-08   0.16510E-08 0.10023E+00 
c  r22          0.10850E-01      13   0.55680E-08   0.18359E-08 0.10204E+00 
c  r33          0.21856E-01      15   0.65617E-08   0.12573E-07 0.12783E+00 
c  r12          0.93838E-03      18   0.70680E-08   0.30368E-09 0.61580E+00 
c  r13          0.46667E-02      19   0.65035E-08   0.14841E-08 0.19915E+00 
c  r23          0.39967E-02      19   0.50537E-08   0.12821E-08 0.19990E+00 
c  epsilon      0.10971E+02      11   0.35906E-08   0.10027E-01 0.16619E+00 
c  TempC        0.25716E+06      16   0.15094E-04   0.83614E-02 0.43132E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63395         0.61346       0.0052535       0.0015072
v  Velocity[Y]            -0.57377         0.54423       0.0030779      0.00087306
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.419          360.02          87.634          169.84
v  r11                   0.0010595        0.081871        0.013068        0.018283
v  r22                   0.0011098        0.082629        0.013348        0.018643
v  r33                   0.0016339         0.17437        0.027238        0.037201
v  r12                   -0.010669        0.013601      -0.0002337     -0.00030925
v  r13                   -0.045556        0.052797      9.2635e-05       0.0010135
v  r23                   -0.046684        0.051183      2.9985e-05      0.00057431
v  epsilon                0.068578          271.39          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9725e-05       0.0099183      0.00092422       0.0017424
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2773          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71348         0.85282


 TIME FOR THE TIME STEP             9985:        0.80396E+02

===============================================================


 INSTANT    0.998600000E-02   TIME STEP NUMBER            9986
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.387925340E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.798865591E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934907E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.223295768E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.224638790E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.128369884E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81249E-03   0.45763E-02 0.20035E+01 
c  Velocity[X]                                      0.13966E-03 
c  Velocity[Y]                                      0.13050E-03 
c  Velocity[Z]                                      0.43061E-02 
c  Pressure     0.36675E-04     132   0.93426E-02   0.25871E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.61837E-08   0.15908E-08 0.98847E-01 
c  r22          0.10850E-01      13   0.56079E-08   0.18257E-08 0.10153E+00 
c  r33          0.21856E-01      15   0.61917E-08   0.12356E-07 0.12686E+00 
c  r12          0.93838E-03      18   0.71651E-08   0.29590E-09 0.60616E+00 
c  r13          0.46667E-02      19   0.67362E-08   0.15072E-08 0.19988E+00 
c  r23          0.39967E-02      19   0.52357E-08   0.12524E-08 0.19769E+00 
c  epsilon      0.10971E+02      11   0.36645E-08   0.98482E-02 0.16454E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84455E-02 0.43345E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63396         0.61343       0.0052534       0.0015072
v  Velocity[Y]            -0.57374         0.54439       0.0030778      0.00087305
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.441             360          87.663          169.84
v  r11                   0.0010595        0.081865        0.013068        0.018283
v  r22                   0.0011098        0.082629        0.013348        0.018643
v  r33                   0.0016339         0.17434        0.027238        0.037201
v  r12                   -0.010672        0.013599      -0.0002337     -0.00030925
v  r13                   -0.045554        0.052796      9.2637e-05       0.0010135
v  r23                   -0.046686        0.051198      2.9986e-05      0.00057431
v  epsilon                0.068578          271.34          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9725e-05       0.0099184      0.00092422       0.0017424
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2774          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71348         0.85282


 TIME FOR THE TIME STEP             9986:        0.79571E+02

===============================================================


 INSTANT    0.998700000E-02   TIME STEP NUMBER            9987
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.246415028E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.430941658E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.103423022E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935021E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.124842990E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.222669404E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      46   0.81183E-03   0.45719E-02 0.20031E+01 
c  Velocity[X]                                      0.13981E-03 
c  Velocity[Y]                                      0.12975E-03 
c  Velocity[Z]                                      0.43024E-02 
c  Pressure     0.36753E-04     133   0.93549E-02   0.25926E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.56759E-08   0.16170E-08 0.99277E-01 
c  r22          0.10850E-01      13   0.60088E-08   0.17910E-08 0.10102E+00 
c  r33          0.21856E-01      15   0.57190E-08   0.12224E-07 0.12642E+00 
c  r12          0.93838E-03      19   0.53829E-08   0.29839E-09 0.60809E+00 
c  r13          0.46667E-02      19   0.61622E-08   0.14683E-08 0.19867E+00 
c  r23          0.39967E-02      19   0.57856E-08   0.12700E-08 0.19808E+00 
c  epsilon      0.10971E+02      11   0.34248E-08   0.94518E-02 0.16169E+00 
c  TempC        0.25716E+06      16   0.15095E-04   0.84938E-02 0.43474E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61346       0.0052534       0.0015072
v  Velocity[Y]            -0.57388         0.54408       0.0030779      0.00087309
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.395          360.05          87.651          169.87
v  r11                   0.0010595         0.08186        0.013068        0.018283
v  r22                   0.0011099        0.082629        0.013348        0.018643
v  r33                   0.0016339         0.17436        0.027238        0.037201
v  r12                   -0.010672        0.013599      -0.0002337     -0.00030925
v  r13                   -0.045553        0.052794      9.2638e-05       0.0010135
v  r23                    -0.04669         0.05119      2.9987e-05      0.00057432
v  epsilon                0.068578          271.35          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9726e-05       0.0099185      0.00092422       0.0017424
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85282


 TIME FOR THE TIME STEP             9987:        0.81463E+02

===============================================================


 INSTANT    0.998800000E-02   TIME STEP NUMBER            9988
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205273629E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.576345227E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149831750E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.259833761E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.486243520E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81303E-03   0.45499E-02 0.19963E+01 
c  Velocity[X]                                      0.13858E-03 
c  Velocity[Y]                                      0.12942E-03 
c  Velocity[Z]                                      0.42819E-02 
c  Pressure     0.36541E-04     132   0.93009E-02   0.25778E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.58455E-08   0.16407E-08 0.10022E+00 
c  r22          0.10850E-01      13   0.56038E-08   0.18286E-08 0.10183E+00 
c  r33          0.21856E-01      15   0.64173E-08   0.12654E-07 0.12825E+00 
c  r12          0.93838E-03      18   0.67091E-08   0.29515E-09 0.60707E+00 
c  r13          0.46667E-02      19   0.71052E-08   0.15144E-08 0.20104E+00 
c  r23          0.39967E-02      19   0.60736E-08   0.12899E-08 0.19998E+00 
c  epsilon      0.10971E+02      11   0.36581E-08   0.10158E-01 0.16849E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.84069E-02 0.43296E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -0.634         0.61345       0.0052534       0.0015072
v  Velocity[Y]            -0.57387          0.5441       0.0030779      0.00087307
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.412          360.07          87.691           169.9
v  r11                   0.0010595        0.081859        0.013068        0.018283
v  r22                   0.0011099         0.08263        0.013348        0.018643
v  r33                   0.0016339         0.17438        0.027238        0.037201
v  r12                   -0.010671        0.013602      -0.0002337     -0.00030925
v  r13                   -0.045555        0.052795      9.2639e-05       0.0010135
v  r23                   -0.046694        0.051183      2.9988e-05      0.00057432
v  epsilon                0.068579          271.38          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9727e-05       0.0099186      0.00092422       0.0017424
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2778          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71348         0.85283


 TIME FOR THE TIME STEP             9988:        0.78114E+02

===============================================================


 INSTANT    0.998900000E-02   TIME STEP NUMBER            9989
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.152596957E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.885901238E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.187817381E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935012E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.197119680E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106675730E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81092E-03   0.45573E-02 0.19982E+01 
c  Velocity[X]                                      0.13957E-03 
c  Velocity[Y]                                      0.12965E-03 
c  Velocity[Z]                                      0.42881E-02 
c  Pressure     0.36620E-04     133   0.93254E-02   0.25831E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60790E-08   0.16519E-08 0.10019E+00 
c  r22          0.10850E-01      13   0.59405E-08   0.18643E-08 0.10241E+00 
c  r33          0.21856E-01      15   0.59812E-08   0.12684E-07 0.12796E+00 
c  r12          0.93838E-03      18   0.66606E-08   0.30431E-09 0.61533E+00 
c  r13          0.46667E-02      19   0.71113E-08   0.15376E-08 0.20236E+00 
c  r23          0.39967E-02      19   0.60456E-08   0.12936E-08 0.20026E+00 
c  epsilon      0.10971E+02      11   0.35092E-08   0.10231E-01 0.16865E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.83925E-02 0.43200E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63399         0.61343       0.0052534       0.0015072
v  Velocity[Y]            -0.57397         0.54428        0.003078       0.0008731
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.407          360.02          87.642          169.85
v  r11                   0.0010595        0.081854        0.013068        0.018283
v  r22                   0.0011099         0.08263        0.013348        0.018643
v  r33                   0.0016339         0.17437        0.027238        0.037201
v  r12                   -0.010675          0.0136      -0.0002337     -0.00030925
v  r13                   -0.045555        0.052792      9.2641e-05       0.0010135
v  r23                   -0.046699        0.051206      2.9989e-05      0.00057432
v  epsilon                0.068579          271.37          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9727e-05       0.0099186      0.00092422       0.0017424
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb               0.00179           5.277          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71348         0.85282


 TIME FOR THE TIME STEP             9989:        0.81160E+02

===============================================================


 INSTANT    0.999000000E-02   TIME STEP NUMBER            9990
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.296461565E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127493898E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934908E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.337309084E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.293397472E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.302180512E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81172E-03   0.45552E-02 0.19995E+01 
c  Velocity[X]                                      0.13970E-03 
c  Velocity[Y]                                      0.12932E-03 
c  Velocity[Z]                                      0.42862E-02 
c  Pressure     0.36314E-04     131   0.92453E-02   0.25616E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59191E-08   0.16530E-08 0.10013E+00 
c  r22          0.10850E-01      13   0.60498E-08   0.18368E-08 0.10152E+00 
c  r33          0.21856E-01      15   0.59825E-08   0.12720E-07 0.12798E+00 
c  r12          0.93838E-03      18   0.65081E-08   0.29922E-09 0.61160E+00 
c  r13          0.46667E-02      19   0.69350E-08   0.15087E-08 0.20013E+00 
c  r23          0.39967E-02      19   0.65813E-08   0.12955E-08 0.20049E+00 
c  epsilon      0.10971E+02      11   0.34309E-08   0.10771E-01 0.17526E+00 
c  TempC        0.25716E+06      16   0.15103E-04   0.84336E-02 0.43305E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -0.634         0.61347       0.0052535       0.0015072
v  Velocity[Y]            -0.57378          0.5444       0.0030779      0.00087307
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.468          360.05          87.694          169.89
v  r11                   0.0010595        0.081853        0.013068        0.018283
v  r22                   0.0011099        0.082629        0.013348        0.018643
v  r33                   0.0016339         0.17435        0.027238        0.037201
v  r12                   -0.010677        0.013598      -0.0002337     -0.00030926
v  r13                   -0.045553        0.052794      9.2643e-05       0.0010135
v  r23                   -0.046703        0.051188       2.999e-05      0.00057432
v  epsilon                0.068579          271.33          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9723e-05       0.0099185      0.00092422       0.0017424
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2771         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71348         0.85282


 TIME FOR THE TIME STEP             9990:        0.82162E+02

===============================================================


 INSTANT    0.999100000E-02   TIME STEP NUMBER            9991
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.285604960E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.925529170E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.410055874E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935019E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.501114269E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115765712E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81188E-03   0.45542E-02 0.19973E+01 
c  Velocity[X]                                      0.13907E-03 
c  Velocity[Y]                                      0.12986E-03 
c  Velocity[Z]                                      0.42853E-02 
c  Pressure     0.36332E-04     133   0.92478E-02   0.25629E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.58314E-08   0.16059E-08 0.99254E-01 
c  r22          0.10850E-01      13   0.62941E-08   0.17761E-08 0.10054E+00 
c  r33          0.21856E-01      15   0.73084E-08   0.12201E-07 0.12625E+00 
c  r12          0.93838E-03      18   0.68038E-08   0.29397E-09 0.60943E+00 
c  r13          0.46667E-02      19   0.73907E-08   0.14589E-08 0.19765E+00 
c  r23          0.39967E-02      20   0.56635E-08   0.12640E-08 0.19793E+00 
c  epsilon      0.10971E+02      11   0.34835E-08   0.95534E-02 0.16322E+00 
c  TempC        0.25716E+06      16   0.15090E-04   0.84278E-02 0.43363E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61346       0.0052534       0.0015071
v  Velocity[Y]            -0.57386         0.54423        0.003078      0.00087312
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.409          360.03          87.649          169.85
v  r11                   0.0010595        0.081849        0.013068        0.018283
v  r22                   0.0011099        0.082627        0.013348        0.018643
v  r33                   0.0016339         0.17436        0.027238        0.037201
v  r12                   -0.010675        0.013596      -0.0002337     -0.00030926
v  r13                   -0.045556        0.052794      9.2644e-05       0.0010135
v  r23                   -0.046707        0.051177       2.999e-05      0.00057432
v  epsilon                0.068579          271.33          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9724e-05       0.0099184      0.00092422       0.0017424
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2779          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71348         0.85282


 TIME FOR THE TIME STEP             9991:        0.78567E+02

===============================================================


 INSTANT    0.999200000E-02   TIME STEP NUMBER            9992
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.526024717E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.370632954E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115698416E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.938354912E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.143998963E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69805E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81175E-03   0.45444E-02 0.19965E+01 
c  Velocity[X]                                      0.13932E-03 
c  Velocity[Y]                                      0.13018E-03 
c  Velocity[Z]                                      0.42749E-02 
c  Pressure     0.36552E-04     132   0.93055E-02   0.25784E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57446E-08   0.16015E-08 0.99160E-01 
c  r22          0.10850E-01      13   0.66957E-08   0.17652E-08 0.10047E+00 
c  r33          0.21856E-01      15   0.70850E-08   0.12160E-07 0.12606E+00 
c  r12          0.93838E-03      18   0.69894E-08   0.29002E-09 0.60406E+00 
c  r13          0.46667E-02      20   0.63260E-08   0.14607E-08 0.19842E+00 
c  r23          0.39967E-02      19   0.70557E-08   0.12624E-08 0.19760E+00 
c  epsilon      0.10971E+02      11   0.35380E-08   0.93963E-02 0.16137E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.84591E-02 0.43394E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61343       0.0052533       0.0015071
v  Velocity[Y]            -0.57384         0.54436        0.003078       0.0008731
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.413          360.01          87.652          169.84
v  r11                   0.0010596        0.081845        0.013068        0.018283
v  r22                   0.0011099        0.082628        0.013348        0.018643
v  r33                    0.001634         0.17438        0.027238        0.037201
v  r12                   -0.010671        0.013596      -0.0002337     -0.00030926
v  r13                   -0.045553        0.052797      9.2646e-05       0.0010135
v  r23                    -0.04671        0.051169      2.9991e-05      0.00057432
v  epsilon                0.068579          271.35          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9721e-05       0.0099182      0.00092423       0.0017424
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2783          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71348         0.85283


 TIME FOR THE TIME STEP             9992:        0.79835E+02

===============================================================


 INSTANT    0.999300000E-02   TIME STEP NUMBER            9993
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160143106E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111002174E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.515539889E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.102974913E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282084498E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81141E-03   0.45306E-02 0.19920E+01 
c  Velocity[X]                                      0.13957E-03 
c  Velocity[Y]                                      0.12979E-03 
c  Velocity[Z]                                      0.42612E-02 
c  Pressure     0.36494E-04     131   0.92969E-02   0.25743E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55224E-08   0.16254E-08 0.99439E-01 
c  r22          0.10850E-01      13   0.62860E-08   0.18033E-08 0.10097E+00 
c  r33          0.21856E-01      15   0.57646E-08   0.12357E-07 0.12659E+00 
c  r12          0.93838E-03      18   0.62334E-08   0.29332E-09 0.60624E+00 
c  r13          0.46667E-02      19   0.66681E-08   0.14704E-08 0.19889E+00 
c  r23          0.39967E-02      19   0.62391E-08   0.12695E-08 0.19734E+00 
c  epsilon      0.10971E+02      11   0.32548E-08   0.97427E-02 0.16419E+00 
c  TempC        0.25716E+06      16   0.15090E-04   0.84864E-02 0.43444E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61346       0.0052533       0.0015071
v  Velocity[Y]            -0.57384          0.5443        0.003078       0.0008731
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                 -36.39          360.13          87.717          169.94
v  r11                   0.0010596        0.081842        0.013068        0.018283
v  r22                   0.0011099        0.082624        0.013348        0.018643
v  r33                    0.001634         0.17437        0.027238        0.037201
v  r12                   -0.010668        0.013596      -0.0002337     -0.00030926
v  r13                   -0.045554        0.052795      9.2647e-05       0.0010135
v  r23                   -0.046713        0.051193      2.9992e-05      0.00057432
v  epsilon                0.068579          271.36          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9719e-05       0.0099181      0.00092423       0.0017424
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2791          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71348         0.85283


 TIME FOR THE TIME STEP             9993:        0.76683E+02

===============================================================


 INSTANT    0.999400000E-02   TIME STEP NUMBER            9994
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.987302629E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.432742917E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.233546159E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.320943931E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.216644512E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81189E-03   0.45444E-02 0.19951E+01 
c  Velocity[X]                                      0.13821E-03 
c  Velocity[Y]                                      0.12943E-03 
c  Velocity[Z]                                      0.42768E-02 
c  Pressure     0.36300E-04     132   0.92331E-02   0.25606E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52852E-08   0.16026E-08 0.98801E-01 
c  r22          0.10850E-01      13   0.58696E-08   0.18017E-08 0.10061E+00 
c  r33          0.21856E-01      15   0.53060E-08   0.12311E-07 0.12612E+00 
c  r12          0.93838E-03      18   0.58906E-08   0.29290E-09 0.60490E+00 
c  r13          0.46667E-02      19   0.61698E-08   0.14688E-08 0.19827E+00 
c  r23          0.39967E-02      19   0.65710E-08   0.12543E-08 0.19684E+00 
c  epsilon      0.10971E+02      11   0.31983E-08   0.97377E-02 0.16335E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.84441E-02 0.43315E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61345       0.0052533       0.0015071
v  Velocity[Y]            -0.57378         0.54436        0.003078       0.0008731
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.419          360.06          87.675          169.88
v  r11                   0.0010596         0.08184        0.013068        0.018283
v  r22                     0.00111        0.082625        0.013348        0.018643
v  r33                    0.001634         0.17433        0.027238        0.037201
v  r12                   -0.010667        0.013596      -0.0002337     -0.00030926
v  r13                   -0.045556        0.052796      9.2649e-05       0.0010135
v  r23                   -0.046715        0.051181      2.9992e-05      0.00057432
v  epsilon                 0.06858          271.32          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9715e-05        0.009918      0.00092423       0.0017424
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2787          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71348         0.85282


 TIME FOR THE TIME STEP             9994:        0.79351E+02

===============================================================


 INSTANT    0.999500000E-02   TIME STEP NUMBER            9995
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.875132789E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.204976369E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.388057708E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226929905E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203656695E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81109E-03   0.45500E-02 0.19983E+01 
c  Velocity[X]                                      0.14030E-03 
c  Velocity[Y]                                      0.12941E-03 
c  Velocity[Z]                                      0.42803E-02 
c  Pressure     0.36629E-04     132   0.93227E-02   0.25839E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55879E-08   0.16223E-08 0.99455E-01 
c  r22          0.10850E-01      13   0.57769E-08   0.18145E-08 0.10072E+00 
c  r33          0.21856E-01      15   0.59095E-08   0.12459E-07 0.12669E+00 
c  r12          0.93839E-03      18   0.52012E-08   0.29475E-09 0.60616E+00 
c  r13          0.46667E-02      19   0.63239E-08   0.14982E-08 0.19923E+00 
c  r23          0.39967E-02      19   0.62156E-08   0.12647E-08 0.19791E+00 
c  epsilon      0.10971E+02      11   0.33061E-08   0.10086E-01 0.16552E+00 
c  TempC        0.25716E+06      16   0.15097E-04   0.84082E-02 0.43222E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61347       0.0052533       0.0015071
v  Velocity[Y]            -0.57376         0.54422       0.0030781      0.00087314
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.397          360.02          87.633          169.84
v  r11                   0.0010596        0.081833        0.013068        0.018283
v  r22                     0.00111        0.082625        0.013348        0.018643
v  r33                    0.001634         0.17435        0.027238        0.037201
v  r12                   -0.010663        0.013596      -0.0002337     -0.00030926
v  r13                   -0.045554        0.052794       9.265e-05       0.0010135
v  r23                   -0.046717        0.051175      2.9993e-05      0.00057432
v  epsilon                 0.06858          271.32          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9715e-05       0.0099181      0.00092423       0.0017424
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb               0.00179           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85282


 TIME FOR THE TIME STEP             9995:        0.81114E+02

===============================================================


 INSTANT    0.999600000E-02   TIME STEP NUMBER            9996
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208994437E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100711522E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934898E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.718988215E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249371027E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.449364677E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81263E-03   0.45444E-02 0.19970E+01 
c  Velocity[X]                                      0.13893E-03 
c  Velocity[Y]                                      0.13060E-03 
c  Velocity[Z]                                      0.42749E-02 
c  Pressure     0.36661E-04     133   0.93322E-02   0.25861E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.53490E-08   0.16263E-08 0.99757E-01 
c  r22          0.10850E-01      13   0.54738E-08   0.18362E-08 0.10133E+00 
c  r33          0.21856E-01      15   0.58143E-08   0.12467E-07 0.12706E+00 
c  r12          0.93839E-03      18   0.51262E-08   0.30224E-09 0.61104E+00 
c  r13          0.46667E-02      19   0.67778E-08   0.15352E-08 0.20092E+00 
c  r23          0.39967E-02      19   0.50658E-08   0.12663E-08 0.19845E+00 
c  epsilon      0.10971E+02      11   0.33739E-08   0.10010E-01 0.16495E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.84322E-02 0.43295E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61347       0.0052533       0.0015071
v  Velocity[Y]            -0.57361         0.54426        0.003078      0.00087313
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.447          360.01          87.661          169.85
v  r11                   0.0010596        0.081828        0.013068        0.018283
v  r22                     0.00111        0.082627        0.013348        0.018643
v  r33                    0.001634         0.17437        0.027238        0.037201
v  r12                   -0.010667        0.013595     -0.00023371     -0.00030926
v  r13                   -0.045552        0.052795      9.2652e-05       0.0010135
v  r23                   -0.046719        0.051204      2.9994e-05      0.00057432
v  epsilon                 0.06858          271.35          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9713e-05       0.0099182      0.00092423       0.0017424
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2774          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71348         0.85282


 TIME FOR THE TIME STEP             9996:        0.80490E+02

===============================================================


 INSTANT    0.999700000E-02   TIME STEP NUMBER            9997
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226411129E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181914131E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.615819486E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.222234979E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.945287800E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81215E-03   0.45233E-02 0.19921E+01 
c  Velocity[X]                                      0.13820E-03 
c  Velocity[Y]                                      0.12977E-03 
c  Velocity[Z]                                      0.42553E-02 
c  Pressure     0.36189E-04     133   0.92208E-02   0.25527E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57351E-08   0.16519E-08 0.10034E+00 
c  r22          0.10850E-01      13   0.52769E-08   0.18268E-08 0.10183E+00 
c  r33          0.21856E-01      15   0.52652E-08   0.12632E-07 0.12841E+00 
c  r12          0.93839E-03      18   0.49660E-08   0.29969E-09 0.61392E+00 
c  r13          0.46667E-02      19   0.56915E-08   0.14968E-08 0.20001E+00 
c  r23          0.39967E-02      19   0.57334E-08   0.13121E-08 0.20237E+00 
c  epsilon      0.10971E+02      11   0.33566E-08   0.10060E-01 0.16997E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.84074E-02 0.43294E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61349       0.0052533       0.0015071
v  Velocity[Y]            -0.57369         0.54441        0.003078      0.00087311
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                 -36.41          360.08           87.69           169.9
v  r11                   0.0010596        0.081829        0.013068        0.018283
v  r22                     0.00111        0.082628        0.013348        0.018643
v  r33                    0.001634         0.17435        0.027238        0.037201
v  r12                   -0.010669        0.013592     -0.00023371     -0.00030926
v  r13                   -0.045556        0.052794      9.2654e-05       0.0010135
v  r23                    -0.04672        0.051196      2.9995e-05      0.00057432
v  epsilon                 0.06858          271.36          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9713e-05       0.0099181      0.00092423       0.0017424
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2774         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71348         0.85282


 TIME FOR THE TIME STEP             9997:        0.79339E+02

===============================================================


 INSTANT    0.999800000E-02   TIME STEP NUMBER            9998
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.247476699E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.193118489E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188916124E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.155659315E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153663970E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81137E-03   0.45494E-02 0.19987E+01 
c  Velocity[X]                                      0.13975E-03 
c  Velocity[Y]                                      0.13000E-03 
c  Velocity[Z]                                      0.42797E-02 
c  Pressure     0.36651E-04     132   0.93404E-02   0.25854E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.63121E-08   0.16132E-08 0.98904E-01 
c  r22          0.10850E-01      13   0.54030E-08   0.18355E-08 0.10190E+00 
c  r33          0.21856E-01      15   0.59344E-08   0.12474E-07 0.12741E+00 
c  r12          0.93839E-03      18   0.58806E-08   0.29547E-09 0.60613E+00 
c  r13          0.46667E-02      19   0.59771E-08   0.14877E-08 0.20005E+00 
c  r23          0.39967E-02      19   0.57250E-08   0.12702E-08 0.19847E+00 
c  epsilon      0.10971E+02      11   0.34632E-08   0.98203E-02 0.16507E+00 
c  TempC        0.25716E+06      16   0.15120E-04   0.83988E-02 0.43253E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63399         0.61346       0.0052534       0.0015071
v  Velocity[Y]             -0.5735         0.54425        0.003078       0.0008731
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.431          360.01          87.666          169.85
v  r11                   0.0010596        0.081832        0.013068        0.018283
v  r22                     0.00111        0.082627        0.013348        0.018643
v  r33                   0.0016341         0.17433        0.027238        0.037201
v  r12                   -0.010669        0.013593     -0.00023371     -0.00030926
v  r13                   -0.045554        0.052794      9.2655e-05       0.0010135
v  r23                    -0.04672        0.051187      2.9996e-05      0.00057432
v  epsilon                 0.06858          271.33          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9714e-05       0.0099181      0.00092423       0.0017424
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2768          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71348         0.85283


 TIME FOR THE TIME STEP             9998:        0.81181E+02

===============================================================


 INSTANT    0.999900000E-02   TIME STEP NUMBER            9999
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.378634671E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.269826850E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.941314157E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188448727E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.340753211E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81117E-03   0.45521E-02 0.19981E+01 
c  Velocity[X]                                      0.13934E-03 
c  Velocity[Y]                                      0.12970E-03 
c  Velocity[Z]                                      0.42830E-02 
c  Pressure     0.36517E-04     132   0.92982E-02   0.25759E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59994E-08   0.16253E-08 0.99592E-01 
c  r22          0.10850E-01      13   0.48497E-08   0.18011E-08 0.10107E+00 
c  r33          0.21856E-01      15   0.53928E-08   0.12319E-07 0.12654E+00 
c  r12          0.93839E-03      18   0.53793E-08   0.29376E-09 0.60637E+00 
c  r13          0.46667E-02      19   0.62802E-08   0.14723E-08 0.19836E+00 
c  r23          0.39967E-02      19   0.68063E-08   0.12590E-08 0.19817E+00 
c  epsilon      0.10971E+02      11   0.34639E-08   0.97159E-02 0.16378E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.85449E-02 0.43608E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61348       0.0052534       0.0015071
v  Velocity[Y]            -0.57365         0.54422       0.0030782      0.00087315
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                 -36.42          360.09          87.688          169.91
v  r11                   0.0010596        0.081849        0.013068        0.018283
v  r22                     0.00111        0.082628        0.013348        0.018643
v  r33                   0.0016341         0.17435        0.027239        0.037201
v  r12                   -0.010669          0.0136     -0.00023371     -0.00030926
v  r13                   -0.045553        0.052793      9.2657e-05       0.0010135
v  r23                   -0.046721        0.051203      2.9997e-05      0.00057432
v  epsilon                 0.06858          271.34          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9715e-05       0.0099182      0.00092424       0.0017424
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85282


 TIME FOR THE TIME STEP             9999:        0.79881E+02

===============================================================


 INSTANT    0.100000000E-01   TIME STEP NUMBER           10000
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.377428221E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.360777139E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.167756850E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.199923209E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.599686386E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81219E-03   0.45538E-02 0.19979E+01 
c  Velocity[X]                                      0.13952E-03 
c  Velocity[Y]                                      0.12932E-03 
c  Velocity[Z]                                      0.42849E-02 
c  Pressure     0.36639E-04     133   0.93346E-02   0.25846E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57917E-08   0.16260E-08 0.99500E-01 
c  r22          0.10850E-01      13   0.52715E-08   0.18367E-08 0.10165E+00 
c  r33          0.21856E-01      15   0.58450E-08   0.12540E-07 0.12711E+00 
c  r12          0.93839E-03      18   0.62791E-08   0.29800E-09 0.60798E+00 
c  r13          0.46667E-02      19   0.68445E-08   0.14960E-08 0.19937E+00 
c  r23          0.39967E-02      19   0.68013E-08   0.12685E-08 0.19829E+00 
c  epsilon      0.10971E+02      11   0.34347E-08   0.10045E-01 0.16471E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.83853E-02 0.43251E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63401         0.61349       0.0052534       0.0015071
v  Velocity[Y]            -0.57349         0.54427       0.0030781       0.0008731
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.417          360.09          87.698          169.91
v  r11                   0.0010596        0.081865        0.013068        0.018283
v  r22                     0.00111        0.082627        0.013348        0.018643
v  r33                   0.0016341         0.17437        0.027239        0.037201
v  r12                   -0.010668        0.013604     -0.00023371     -0.00030926
v  r13                   -0.045556        0.052794      9.2658e-05       0.0010135
v  r23                   -0.046721        0.051191      2.9998e-05      0.00057432
v  epsilon                 0.06858          271.35          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9717e-05       0.0099182      0.00092424       0.0017424
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2782          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71348         0.85283


 TIME FOR THE TIME STEP            10000:        0.81621E+02

===============================================================


 INSTANT    0.100010000E-01   TIME STEP NUMBER           10001
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106496857E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.176847388E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208666875E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935014E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.272871522E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.423164267E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81099E-03   0.45616E-02 0.20027E+01 
c  Velocity[X]                                      0.13956E-03 
c  Velocity[Y]                                      0.13069E-03 
c  Velocity[Z]                                      0.42914E-02 
c  Pressure     0.36350E-04     134   0.92565E-02   0.25642E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.62261E-08   0.16351E-08 0.99511E-01 
c  r22          0.10850E-01      13   0.53903E-08   0.18199E-08 0.10135E+00 
c  r33          0.21856E-01      15   0.63960E-08   0.12500E-07 0.12711E+00 
c  r12          0.93839E-03      18   0.66883E-08   0.29493E-09 0.60894E+00 
c  r13          0.46667E-02      20   0.62131E-08   0.14946E-08 0.19955E+00 
c  r23          0.39967E-02      19   0.62188E-08   0.12766E-08 0.19881E+00 
c  epsilon      0.10971E+02      11   0.34327E-08   0.98531E-02 0.16411E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.83752E-02 0.43211E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393         0.61347       0.0052534       0.0015071
v  Velocity[Y]            -0.57347         0.54443       0.0030781      0.00087312
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.434          360.01          87.657          169.85
v  r11                   0.0010596        0.081869        0.013068        0.018283
v  r22                     0.00111        0.082628        0.013348        0.018643
v  r33                   0.0016341         0.17436        0.027239        0.037201
v  r12                   -0.010667        0.013607     -0.00023371     -0.00030926
v  r13                   -0.045555        0.052793      9.2659e-05       0.0010135
v  r23                   -0.046722        0.051173      2.9999e-05      0.00057433
v  epsilon                 0.06858          271.36          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9719e-05       0.0099181      0.00092424       0.0017424
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017901           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7405e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85282


 TIME FOR THE TIME STEP            10001:        0.80477E+02

===============================================================


 INSTANT    0.100020000E-01   TIME STEP NUMBER           10002
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.422260612E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.167456393E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.251540283E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.481676057E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.459203330E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81172E-03   0.45493E-02 0.19971E+01 
c  Velocity[X]                                      0.13966E-03 
c  Velocity[Y]                                      0.12986E-03 
c  Velocity[Z]                                      0.42797E-02 
c  Pressure     0.36354E-04     131   0.92484E-02   0.25643E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.58489E-08   0.16042E-08 0.98920E-01 
c  r22          0.10850E-01      13   0.55672E-08   0.18196E-08 0.10117E+00 
c  r33          0.21856E-01      15   0.68886E-08   0.12314E-07 0.12633E+00 
c  r12          0.93839E-03      18   0.72363E-08   0.29049E-09 0.60531E+00 
c  r13          0.46667E-02      19   0.72095E-08   0.14773E-08 0.19883E+00 
c  r23          0.39967E-02      19   0.72136E-08   0.12520E-08 0.19740E+00 
c  epsilon      0.10971E+02      11   0.33945E-08   0.97439E-02 0.16436E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.84883E-02 0.43414E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393         0.61347       0.0052534       0.0015071
v  Velocity[Y]            -0.57344          0.5442        0.003078      0.00087309
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.447             360          87.664          169.85
v  r11                   0.0010596        0.081866        0.013068        0.018283
v  r22                   0.0011101        0.082625        0.013348        0.018643
v  r33                   0.0016341         0.17434        0.027239        0.037201
v  r12                   -0.010666          0.0136     -0.00023371     -0.00030926
v  r13                   -0.045553        0.052795      9.2661e-05       0.0010135
v  r23                   -0.046722        0.051195      3.0001e-05      0.00057433
v  epsilon                0.068581          271.32          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.972e-05       0.0099181      0.00092424       0.0017424
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85282


 TIME FOR THE TIME STEP            10002:        0.81127E+02

===============================================================


 INSTANT    0.100030000E-01   TIME STEP NUMBER           10003
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.582303899E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.326915262E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.299360118E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.940880262E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.456024841E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81233E-03   0.45200E-02 0.19916E+01 
c  Velocity[X]                                      0.13893E-03 
c  Velocity[Y]                                      0.12964E-03 
c  Velocity[Z]                                      0.42514E-02 
c  Pressure     0.36226E-04     131   0.92249E-02   0.25553E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.58170E-08   0.16455E-08 0.10012E+00 
c  r22          0.10850E-01      13   0.55910E-08   0.18065E-08 0.10130E+00 
c  r33          0.21856E-01      16   0.56879E-08   0.12543E-07 0.12769E+00 
c  r12          0.93839E-03      18   0.69378E-08   0.29865E-09 0.60661E+00 
c  r13          0.46667E-02      20   0.56962E-08   0.15012E-08 0.19980E+00 
c  r23          0.39967E-02      20   0.55308E-08   0.13139E-08 0.20130E+00 
c  epsilon      0.10971E+02      11   0.34129E-08   0.10238E-01 0.17166E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.84448E-02 0.43355E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393          0.6135       0.0052534       0.0015071
v  Velocity[Y]            -0.57337         0.54431        0.003078      0.00087308
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.388          360.06          87.673          169.89
v  r11                   0.0010596        0.081875        0.013068        0.018283
v  r22                   0.0011101        0.082626        0.013348        0.018643
v  r33                   0.0016341         0.17434        0.027239        0.037201
v  r12                   -0.010664        0.013601     -0.00023371     -0.00030926
v  r13                   -0.045555        0.052795      9.2663e-05       0.0010135
v  r23                   -0.046723        0.051191      3.0001e-05      0.00057433
v  epsilon                0.068581          271.36          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9723e-05       0.0099182      0.00092424       0.0017424
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2778         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71347         0.85282


 TIME FOR THE TIME STEP            10003:        0.80346E+02

===============================================================


 INSTANT    0.100040000E-01   TIME STEP NUMBER           10004
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.303980474E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157374786E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.714275659E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.432706110E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.288397541E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81181E-03   0.45346E-02 0.19962E+01 
c  Velocity[X]                                      0.13894E-03 
c  Velocity[Y]                                      0.12965E-03 
c  Velocity[Z]                                      0.42661E-02 
c  Pressure     0.36755E-04     133   0.93587E-02   0.25927E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60562E-08   0.16621E-08 0.10046E+00 
c  r22          0.10850E-01      13   0.53566E-08   0.17940E-08 0.10135E+00 
c  r33          0.21856E-01      15   0.66429E-08   0.12442E-07 0.12761E+00 
c  r12          0.93839E-03      19   0.56373E-08   0.30140E-09 0.61247E+00 
c  r13          0.46667E-02      19   0.68549E-08   0.14593E-08 0.19844E+00 
c  r23          0.39967E-02      19   0.68965E-08   0.12991E-08 0.20118E+00 
c  epsilon      0.10971E+02      11   0.35456E-08   0.96795E-02 0.16456E+00 
c  TempC        0.25716E+06      16   0.15174E-04   0.84570E-02 0.43365E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61346       0.0052534       0.0015071
v  Velocity[Y]            -0.57332         0.54432        0.003078      0.00087307
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.437          360.04           87.67          169.88
v  r11                   0.0010596        0.081876        0.013068        0.018283
v  r22                   0.0011101        0.082628        0.013348        0.018643
v  r33                   0.0016341         0.17437        0.027239        0.037201
v  r12                   -0.010666        0.013606     -0.00023371     -0.00030926
v  r13                   -0.045553        0.052797      9.2664e-05       0.0010135
v  r23                   -0.046723        0.051176      3.0002e-05      0.00057433
v  epsilon                0.068581          271.37          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9723e-05       0.0099181      0.00092424       0.0017424
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2774          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71348         0.85282


 TIME FOR THE TIME STEP            10004:        0.80938E+02

===============================================================


 INSTANT    0.100050000E-01   TIME STEP NUMBER           10005
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173733277E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.853670806E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.288356975E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.434764167E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.546317384E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      44   0.81133E-03   0.45538E-02 0.19996E+01 
c  Velocity[X]                                      0.13992E-03 
c  Velocity[Y]                                      0.12993E-03 
c  Velocity[Z]                                      0.42839E-02 
c  Pressure     0.36311E-04     133   0.92506E-02   0.25614E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.61583E-08   0.16250E-08 0.99712E-01 
c  r22          0.10850E-01      13   0.52893E-08   0.17987E-08 0.10126E+00 
c  r33          0.21856E-01      15   0.65067E-08   0.12280E-07 0.12668E+00 
c  r12          0.93839E-03      19   0.58223E-08   0.29174E-09 0.60391E+00 
c  r13          0.46667E-02      19   0.64856E-08   0.14563E-08 0.19852E+00 
c  r23          0.39967E-02      19   0.69483E-08   0.12684E-08 0.19873E+00 
c  epsilon      0.10971E+02      11   0.34104E-08   0.97266E-02 0.16306E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.83788E-02 0.43175E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63377         0.61351       0.0052535       0.0015072
v  Velocity[Y]            -0.57352         0.54437       0.0030781      0.00087314
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.428          360.06          87.676          169.88
v  r11                   0.0010596        0.081881        0.013068        0.018283
v  r22                   0.0011101        0.082631        0.013348        0.018643
v  r33                   0.0016342         0.17436        0.027239        0.037201
v  r12                   -0.010667        0.013607     -0.00023371     -0.00030926
v  r13                   -0.045554        0.052796      9.2665e-05       0.0010135
v  r23                   -0.046723        0.051201      3.0003e-05      0.00057433
v  epsilon                0.068581          271.38          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9724e-05       0.0099181      0.00092424       0.0017424
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2775          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71348         0.85282


 TIME FOR THE TIME STEP            10005:        0.80484E+02

===============================================================


 INSTANT    0.100060000E-01   TIME STEP NUMBER           10006
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.608143298E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.488634272E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.561842645E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209610301E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.419282131E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81199E-03   0.45599E-02 0.19992E+01 
c  Velocity[X]                                      0.13840E-03 
c  Velocity[Y]                                      0.13020E-03 
c  Velocity[Z]                                      0.42913E-02 
c  Pressure     0.36601E-04     132   0.93217E-02   0.25820E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60353E-08   0.16592E-08 0.10037E+00 
c  r22          0.10850E-01      13   0.55510E-08   0.18447E-08 0.10203E+00 
c  r33          0.21856E-01      16   0.62986E-08   0.12751E-07 0.12840E+00 
c  r12          0.93839E-03      19   0.60724E-08   0.29756E-09 0.60856E+00 
c  r13          0.46667E-02      19   0.71701E-08   0.14981E-08 0.20044E+00 
c  r23          0.39967E-02      19   0.66513E-08   0.13065E-08 0.20169E+00 
c  epsilon      0.10971E+02      11   0.35593E-08   0.10383E-01 0.16834E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.83612E-02 0.43167E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385          0.6135       0.0052536       0.0015072
v  Velocity[Y]            -0.57341         0.54444       0.0030781      0.00087313
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.455          360.02          87.661          169.85
v  r11                   0.0010596        0.081884        0.013068        0.018283
v  r22                   0.0011101        0.082633        0.013348        0.018643
v  r33                   0.0016342         0.17433        0.027239        0.037201
v  r12                   -0.010666        0.013609     -0.00023371     -0.00030926
v  r13                   -0.045556        0.052796      9.2666e-05       0.0010135
v  r23                   -0.046723        0.051189      3.0004e-05      0.00057433
v  epsilon                0.068581          271.34          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9723e-05       0.0099181      0.00092425       0.0017424
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2776          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71348         0.85282


 TIME FOR THE TIME STEP            10006:        0.80896E+02

===============================================================


 INSTANT    0.100070000E-01   TIME STEP NUMBER           10007
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179354389E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.311168208E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161702679E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145247097E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.467414033E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81133E-03   0.45747E-02 0.20031E+01 
c  Velocity[X]                                      0.14094E-03 
c  Velocity[Y]                                      0.13030E-03 
c  Velocity[Z]                                      0.43034E-02 
c  Pressure     0.36729E-04     133   0.93506E-02   0.25909E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.61713E-08   0.16325E-08 0.99305E-01 
c  r22          0.10850E-01      13   0.53907E-08   0.18329E-08 0.10186E+00 
c  r33          0.21856E-01      15   0.74586E-08   0.12531E-07 0.12731E+00 
c  r12          0.93839E-03      19   0.56557E-08   0.29521E-09 0.60491E+00 
c  r13          0.46667E-02      19   0.70519E-08   0.15056E-08 0.20025E+00 
c  r23          0.39967E-02      19   0.72551E-08   0.12920E-08 0.19940E+00 
c  epsilon      0.10971E+02      11   0.35721E-08   0.10088E-01 0.16641E+00 
c  TempC        0.25716E+06      16   0.15105E-04   0.85030E-02 0.43521E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61347       0.0052535       0.0015072
v  Velocity[Y]            -0.57343         0.54427       0.0030781      0.00087315
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.425          360.06          87.676          169.89
v  r11                   0.0010596        0.081882        0.013068        0.018283
v  r22                   0.0011101        0.082633        0.013348        0.018643
v  r33                   0.0016342         0.17436        0.027239        0.037201
v  r12                   -0.010665        0.013604     -0.00023371     -0.00030926
v  r13                   -0.045553        0.052794      9.2667e-05       0.0010135
v  r23                   -0.046723        0.051175      3.0005e-05      0.00057433
v  epsilon                0.068581          271.35          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9722e-05       0.0099177      0.00092425       0.0017424
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2778          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71348         0.85282


 TIME FOR THE TIME STEP            10007:        0.78624E+02

===============================================================


 INSTANT    0.100080000E-01   TIME STEP NUMBER           10008
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.109138560E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.322342346E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.426899993E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100448890E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140449050E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81272E-03   0.45339E-02 0.19917E+01 
c  Velocity[X]                                      0.13943E-03 
c  Velocity[Y]                                      0.12969E-03 
c  Velocity[Z]                                      0.42647E-02 
c  Pressure     0.36209E-04     133   0.92191E-02   0.25542E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.67482E-08   0.16762E-08 0.10078E+00 
c  r22          0.10850E-01      13   0.58598E-08   0.18277E-08 0.10194E+00 
c  r33          0.21856E-01      15   0.70241E-08   0.12560E-07 0.12784E+00 
c  r12          0.93839E-03      19   0.66132E-08   0.30023E-09 0.60853E+00 
c  r13          0.46667E-02      19   0.72917E-08   0.14756E-08 0.19989E+00 
c  r23          0.39967E-02      19   0.65903E-08   0.12931E-08 0.20072E+00 
c  epsilon      0.10971E+02      11   0.34708E-08   0.10028E-01 0.16581E+00 
c  TempC        0.25716E+06      16   0.15164E-04   0.85016E-02 0.43528E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388          0.6135       0.0052536       0.0015072
v  Velocity[Y]            -0.57329         0.54421       0.0030781      0.00087313
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.426          360.04          87.676          169.87
v  r11                   0.0010596        0.081882        0.013068        0.018283
v  r22                   0.0011101        0.082634        0.013348        0.018643
v  r33                   0.0016342         0.17439        0.027239        0.037201
v  r12                   -0.010663        0.013606     -0.00023371     -0.00030926
v  r13                   -0.045552        0.052796      9.2669e-05       0.0010135
v  r23                   -0.046723        0.051195      3.0006e-05      0.00057433
v  epsilon                0.068581          271.37          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9719e-05       0.0099177      0.00092425       0.0017424
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2776          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71348         0.85282


 TIME FOR THE TIME STEP            10008:        0.77277E+02

===============================================================


 INSTANT    0.100090000E-01   TIME STEP NUMBER           10009
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168329294E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.174661173E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.113814522E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935016E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.319381638E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.294452715E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81144E-03   0.45284E-02 0.19950E+01 
c  Velocity[X]                                      0.13863E-03 
c  Velocity[Y]                                      0.12972E-03 
c  Velocity[Z]                                      0.42600E-02 
c  Pressure     0.36463E-04     134   0.92804E-02   0.25722E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.68256E-08   0.16592E-08 0.10040E+00 
c  r22          0.10850E-01      13   0.54348E-08   0.18222E-08 0.10176E+00 
c  r33          0.21856E-01      15   0.72373E-08   0.12631E-07 0.12814E+00 
c  r12          0.93839E-03      19   0.57573E-08   0.29762E-09 0.60570E+00 
c  r13          0.46667E-02      20   0.59522E-08   0.14874E-08 0.19975E+00 
c  r23          0.39967E-02      19   0.64445E-08   0.13139E-08 0.20149E+00 
c  epsilon      0.10971E+02      11   0.35176E-08   0.10352E-01 0.17153E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.84330E-02 0.43322E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388          0.6135       0.0052535       0.0015072
v  Velocity[Y]            -0.57335         0.54425       0.0030782      0.00087318
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.437          360.09          87.675           169.9
v  r11                   0.0010596        0.081882        0.013068        0.018283
v  r22                   0.0011101         0.08263        0.013348        0.018643
v  r33                   0.0016342         0.17437        0.027239        0.037201
v  r12                   -0.010663        0.013601     -0.00023371     -0.00030926
v  r13                   -0.045557        0.052795       9.267e-05       0.0010135
v  r23                   -0.046722        0.051196      3.0007e-05      0.00057433
v  epsilon                0.068581          271.38          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9717e-05       0.0099177      0.00092425       0.0017424
v  CourantNb               0.44257             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2778          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71348         0.85283


 TIME FOR THE TIME STEP            10009:        0.76897E+02

===============================================================


 INSTANT    0.100100000E-01   TIME STEP NUMBER           10010
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.119862196E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123622656E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.451403801E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.544298322E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138938029E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      45   0.81157E-03   0.45907E-02 0.20053E+01 
c  Velocity[X]                                      0.14016E-03 
c  Velocity[Y]                                      0.13016E-03 
c  Velocity[Z]                                      0.43204E-02 
c  Pressure     0.36645E-04     131   0.93262E-02   0.25851E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.67858E-08   0.16087E-08 0.99350E-01 
c  r22          0.10850E-01      13   0.54834E-08   0.17787E-08 0.10127E+00 
c  r33          0.21856E-01      16   0.60365E-08   0.12207E-07 0.12686E+00 
c  r12          0.93839E-03      19   0.58474E-08   0.29432E-09 0.60464E+00 
c  r13          0.46667E-02      19   0.73290E-08   0.14549E-08 0.19899E+00 
c  r23          0.39967E-02      19   0.67645E-08   0.12742E-08 0.19854E+00 
c  epsilon      0.10971E+02      11   0.35494E-08   0.93183E-02 0.16196E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.84157E-02 0.43296E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393         0.61346       0.0052536       0.0015072
v  Velocity[Y]            -0.57329          0.5444       0.0030781      0.00087316
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                 -36.44          359.98          87.641          169.82
v  r11                   0.0010597        0.081884        0.013068        0.018283
v  r22                   0.0011101        0.082629        0.013348        0.018643
v  r33                   0.0016342         0.17434        0.027239        0.037201
v  r12                   -0.010664        0.013603     -0.00023371     -0.00030926
v  r13                   -0.045554        0.052795      9.2672e-05       0.0010135
v  r23                   -0.046721        0.051186      3.0007e-05      0.00057433
v  epsilon                0.068582          271.32          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9714e-05       0.0099176      0.00092425       0.0017424
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2781          0.1144         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71348         0.85283


 TIME FOR THE TIME STEP            10010:        0.77647E+02

===============================================================


 INSTANT    0.100110000E-01   TIME STEP NUMBER           10011
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.399543493E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186693628E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.205482066E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.194357124E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.172737910E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81197E-03   0.45799E-02 0.20049E+01 
c  Velocity[X]                                      0.14018E-03 
c  Velocity[Y]                                      0.12966E-03 
c  Velocity[Z]                                      0.43100E-02 
c  Pressure     0.36661E-04     133   0.93326E-02   0.25862E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.68402E-08   0.16249E-08 0.99717E-01 
c  r22          0.10850E-01      13   0.55733E-08   0.17775E-08 0.10097E+00 
c  r33          0.21856E-01      15   0.70992E-08   0.12282E-07 0.12692E+00 
c  r12          0.93839E-03      19   0.56280E-08   0.29122E-09 0.60206E+00 
c  r13          0.46667E-02      19   0.72259E-08   0.14594E-08 0.19884E+00 
c  r23          0.39967E-02      19   0.59377E-08   0.12766E-08 0.19937E+00 
c  epsilon      0.10971E+02      11   0.36279E-08   0.95927E-02 0.16346E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.84567E-02 0.43389E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391          0.6135       0.0052536       0.0015072
v  Velocity[Y]            -0.57338         0.54426       0.0030782      0.00087319
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.413          360.03          87.653          169.86
v  r11                   0.0010597        0.081883        0.013068        0.018283
v  r22                   0.0011101        0.082629        0.013348        0.018643
v  r33                   0.0016343         0.17436        0.027239        0.037201
v  r12                   -0.010664        0.013608     -0.00023371     -0.00030926
v  r13                   -0.045553        0.052795      9.2673e-05       0.0010135
v  r23                    -0.04672        0.051206      3.0008e-05      0.00057433
v  epsilon                0.068582          271.34          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9713e-05       0.0099177      0.00092425       0.0017424
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017901           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85282


 TIME FOR THE TIME STEP            10011:        0.79073E+02

===============================================================


 INSTANT    0.100120000E-01   TIME STEP NUMBER           10012
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.364064042E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.513972850E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.509993117E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.554828099E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.852639302E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      40   0.81236E-03   0.45464E-02 0.19965E+01 
c  Velocity[X]                                      0.13804E-03 
c  Velocity[Y]                                      0.12978E-03 
c  Velocity[Z]                                      0.42786E-02 
c  Pressure     0.36770E-04     132   0.93609E-02   0.25938E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.69538E-08   0.16441E-08 0.10081E+00 
c  r22          0.10850E-01      13   0.53724E-08   0.18267E-08 0.10191E+00 
c  r33          0.21856E-01      16   0.61145E-08   0.12488E-07 0.12780E+00 
c  r12          0.93839E-03      19   0.56341E-08   0.30165E-09 0.61064E+00 
c  r13          0.46667E-02      20   0.63697E-08   0.14926E-08 0.19977E+00 
c  r23          0.39968E-02      19   0.68990E-08   0.12836E-08 0.20040E+00 
c  epsilon      0.10971E+02      11   0.35924E-08   0.97471E-02 0.16484E+00 
c  TempC        0.25716E+06      16   0.15118E-04   0.84081E-02 0.43308E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61351       0.0052536       0.0015073
v  Velocity[Y]            -0.57338         0.54425       0.0030782      0.00087316
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.473          360.02          87.644          169.85
v  r11                   0.0010597        0.081894        0.013068        0.018283
v  r22                   0.0011101        0.082631        0.013348        0.018643
v  r33                   0.0016343         0.17438        0.027239        0.037201
v  r12                    -0.01067        0.013607     -0.00023371     -0.00030926
v  r13                   -0.045555        0.052797      9.2675e-05       0.0010135
v  r23                    -0.04672        0.051194      3.0009e-05      0.00057433
v  epsilon                0.068582          271.36          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9714e-05       0.0099177      0.00092425       0.0017424
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2771          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71348         0.85282


 TIME FOR THE TIME STEP            10012:        0.77071E+02

===============================================================


 INSTANT    0.100130000E-01   TIME STEP NUMBER           10013
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.210520618E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.834169450E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.118291577E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.640638186E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.454370323E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81134E-03   0.45320E-02 0.19951E+01 
c  Velocity[X]                                      0.13899E-03 
c  Velocity[Y]                                      0.13034E-03 
c  Velocity[Z]                                      0.42626E-02 
c  Pressure     0.36107E-04     132   0.91863E-02   0.25470E-01 0.00000E+00 
c  r11          0.10583E-01      14   0.54645E-08   0.16332E-08 0.99554E-01 
c  r22          0.10850E-01      13   0.59563E-08   0.18326E-08 0.10180E+00 
c  r33          0.21856E-01      16   0.56946E-08   0.12534E-07 0.12751E+00 
c  r12          0.93840E-03      19   0.63759E-08   0.29479E-09 0.60577E+00 
c  r13          0.46667E-02      20   0.58885E-08   0.14907E-08 0.20011E+00 
c  r23          0.39968E-02      20   0.61996E-08   0.12689E-08 0.19806E+00 
c  epsilon      0.10971E+02      11   0.34239E-08   0.10155E-01 0.16780E+00 
c  TempC        0.25716E+06      16   0.15110E-04   0.84340E-02 0.43373E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61348       0.0052536       0.0015073
v  Velocity[Y]            -0.57349         0.54446       0.0030782      0.00087316
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                 -36.45          360.03          87.651          169.86
v  r11                   0.0010597        0.081905        0.013068        0.018283
v  r22                   0.0011102        0.082631        0.013348        0.018643
v  r33                   0.0016343         0.17438        0.027239        0.037201
v  r12                   -0.010672         0.01361     -0.00023371     -0.00030926
v  r13                   -0.045555        0.052795      9.2676e-05       0.0010135
v  r23                   -0.046719        0.051183      3.0009e-05      0.00057433
v  epsilon                0.068582          271.39          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9716e-05       0.0099177      0.00092426       0.0017424
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2766         0.11439         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71348         0.85282


 TIME FOR THE TIME STEP            10013:        0.79700E+02

===============================================================


 INSTANT    0.100140000E-01   TIME STEP NUMBER           10014
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173885636E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.215167496E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.408094725E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.143632274E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.141646989E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81214E-03   0.45371E-02 0.19945E+01 
c  Velocity[X]                                      0.13912E-03 
c  Velocity[Y]                                      0.12987E-03 
c  Velocity[Z]                                      0.42681E-02 
c  Pressure     0.36432E-04     132   0.92788E-02   0.25700E-01 0.00000E+00 
c  r11          0.10583E-01      14   0.54684E-08   0.16166E-08 0.99465E-01 
c  r22          0.10850E-01      13   0.61171E-08   0.18085E-08 0.10125E+00 
c  r33          0.21856E-01      15   0.68021E-08   0.12326E-07 0.12674E+00 
c  r12          0.93840E-03      19   0.65123E-08   0.29702E-09 0.60626E+00 
c  r13          0.46667E-02      19   0.71698E-08   0.14717E-08 0.19911E+00 
c  r23          0.39968E-02      20   0.56373E-08   0.12633E-08 0.19813E+00 
c  epsilon      0.10971E+02      11   0.35238E-08   0.97566E-02 0.16514E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.84758E-02 0.43331E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61353       0.0052536       0.0015073
v  Velocity[Y]            -0.57331         0.54417       0.0030781      0.00087316
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.473          360.03          87.656          169.85
v  r11                   0.0010597         0.08191        0.013068        0.018283
v  r22                   0.0011102        0.082631        0.013348        0.018643
v  r33                   0.0016343         0.17436        0.027239        0.037201
v  r12                   -0.010673        0.013608     -0.00023371     -0.00030926
v  r13                   -0.045553        0.052795      9.2678e-05       0.0010135
v  r23                   -0.046718        0.051209      3.0011e-05      0.00057434
v  epsilon                0.068582          271.34          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9716e-05       0.0099178      0.00092426       0.0017424
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017901           5.277          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71348         0.85283


 TIME FOR THE TIME STEP            10014:        0.79452E+02

===============================================================


 INSTANT    0.100150000E-01   TIME STEP NUMBER           10015
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127608203E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.248476202E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.895440319E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.328680065E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.394729806E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81151E-03   0.45381E-02 0.19946E+01 
c  Velocity[X]                                      0.13903E-03 
c  Velocity[Y]                                      0.12885E-03 
c  Velocity[Z]                                      0.42702E-02 
c  Pressure     0.36355E-04     133   0.92680E-02   0.25644E-01 0.00000E+00 
c  r11          0.10583E-01      14   0.51508E-08   0.16531E-08 0.10028E+00 
c  r22          0.10850E-01      13   0.60031E-08   0.18167E-08 0.10174E+00 
c  r33          0.21856E-01      15   0.65497E-08   0.12660E-07 0.12834E+00 
c  r12          0.93840E-03      19   0.63221E-08   0.29964E-09 0.60674E+00 
c  r13          0.46667E-02      20   0.57505E-08   0.14880E-08 0.20022E+00 
c  r23          0.39968E-02      20   0.56248E-08   0.13109E-08 0.20148E+00 
c  epsilon      0.10971E+02      11   0.34641E-08   0.10268E-01 0.17167E+00 
c  TempC        0.25716E+06      16   0.15078E-04   0.84234E-02 0.43291E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61354       0.0052536       0.0015072
v  Velocity[Y]            -0.57337          0.5442       0.0030782      0.00087313
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.389          360.09          87.686           169.9
v  r11                   0.0010597        0.081925        0.013068        0.018283
v  r22                   0.0011102         0.08263        0.013348        0.018643
v  r33                   0.0016343         0.17437        0.027239        0.037201
v  r12                   -0.010676        0.013608     -0.00023371     -0.00030926
v  r13                   -0.045556        0.052794      9.2679e-05       0.0010135
v  r23                   -0.046717        0.051196      3.0012e-05      0.00057434
v  epsilon                0.068582          271.35          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9717e-05       0.0099179      0.00092426       0.0017424
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2772          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71348         0.85282


 TIME FOR THE TIME STEP            10015:        0.79408E+02

===============================================================


 INSTANT    0.100160000E-01   TIME STEP NUMBER           10016
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.304960524E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.104455410E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934908E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.284337814E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.335275441E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.126487388E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81221E-03   0.45588E-02 0.20011E+01 
c  Velocity[X]                                      0.13948E-03 
c  Velocity[Y]                                      0.12970E-03 
c  Velocity[Z]                                      0.42896E-02 
c  Pressure     0.36666E-04     133   0.93357E-02   0.25865E-01 0.00000E+00 
c  r11          0.10583E-01      14   0.52145E-08   0.16116E-08 0.99468E-01 
c  r22          0.10850E-01      13   0.58656E-08   0.18040E-08 0.10138E+00 
c  r33          0.21856E-01      15   0.71394E-08   0.12257E-07 0.12659E+00 
c  r12          0.93840E-03      19   0.62592E-08   0.29701E-09 0.60535E+00 
c  r13          0.46668E-02      19   0.62965E-08   0.14707E-08 0.19902E+00 
c  r23          0.39968E-02      19   0.66349E-08   0.12543E-08 0.19787E+00 
c  epsilon      0.10971E+02      11   0.32906E-08   0.96502E-02 0.16351E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.84037E-02 0.43294E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61349       0.0052536       0.0015072
v  Velocity[Y]            -0.57334         0.54436       0.0030782      0.00087315
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.441          360.06          87.689          169.89
v  r11                   0.0010597        0.081931        0.013068        0.018283
v  r22                   0.0011102        0.082629        0.013348        0.018643
v  r33                   0.0016343         0.17439        0.027239        0.037201
v  r12                   -0.010672        0.013608     -0.00023371     -0.00030926
v  r13                   -0.045554        0.052794      9.2681e-05       0.0010135
v  r23                   -0.046717        0.051189      3.0013e-05      0.00057434
v  epsilon                0.068582          271.38          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9715e-05       0.0099176      0.00092426       0.0017424
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2772          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71348         0.85282


 TIME FOR THE TIME STEP            10016:        0.80502E+02

===============================================================


 INSTANT    0.100170000E-01   TIME STEP NUMBER           10017
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181066297E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151512255E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203384295E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.565362554E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.189114685E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      40   0.81099E-03   0.45516E-02 0.19996E+01 
c  Velocity[X]                                      0.13999E-03 
c  Velocity[Y]                                      0.12970E-03 
c  Velocity[Z]                                      0.42819E-02 
c  Pressure     0.36729E-04     133   0.93396E-02   0.25909E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.68096E-08   0.16233E-08 0.99832E-01 
c  r22          0.10850E-01      13   0.59490E-08   0.17926E-08 0.10117E+00 
c  r33          0.21856E-01      15   0.64615E-08   0.12305E-07 0.12698E+00 
c  r12          0.93840E-03      19   0.58784E-08   0.28840E-09 0.59891E+00 
c  r13          0.46668E-02      19   0.65902E-08   0.14644E-08 0.19897E+00 
c  r23          0.39968E-02      19   0.60308E-08   0.12825E-08 0.19967E+00 
c  epsilon      0.10971E+02      11   0.33103E-08   0.95496E-02 0.16246E+00 
c  TempC        0.25716E+06      16   0.15097E-04   0.83942E-02 0.43248E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61353       0.0052536       0.0015072
v  Velocity[Y]            -0.57341         0.54452       0.0030782      0.00087316
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                 -36.42          360.09          87.682           169.9
v  r11                   0.0010597        0.081941        0.013068        0.018283
v  r22                   0.0011102        0.082626        0.013348        0.018643
v  r33                   0.0016343         0.17438        0.027239        0.037201
v  r12                    -0.01067        0.013603     -0.00023371     -0.00030926
v  r13                   -0.045554        0.052796      9.2681e-05       0.0010135
v  r23                   -0.046717        0.051208      3.0014e-05      0.00057434
v  epsilon                0.068582          271.37          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9714e-05       0.0099176      0.00092426       0.0017424
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2771          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71348         0.85282


 TIME FOR THE TIME STEP            10017:        0.79058E+02

===============================================================


 INSTANT    0.100180000E-01   TIME STEP NUMBER           10018
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.382453393E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.570819162E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.708402332E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.433908869E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.391353791E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      44   0.81256E-03   0.45558E-02 0.19975E+01 
c  Velocity[X]                                      0.13933E-03 
c  Velocity[Y]                                      0.13035E-03 
c  Velocity[Z]                                      0.42861E-02 
c  Pressure     0.36784E-04     131   0.93617E-02   0.25948E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.66393E-08   0.16262E-08 0.99853E-01 
c  r22          0.10850E-01      13   0.56426E-08   0.18257E-08 0.10161E+00 
c  r33          0.21856E-01      15   0.63308E-08   0.12566E-07 0.12782E+00 
c  r12          0.93840E-03      19   0.54587E-08   0.29021E-09 0.60058E+00 
c  r13          0.46668E-02      19   0.69043E-08   0.15014E-08 0.20060E+00 
c  r23          0.39968E-02      19   0.53617E-08   0.12902E-08 0.20031E+00 
c  epsilon      0.10971E+02      11   0.33718E-08   0.10090E-01 0.16707E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.84320E-02 0.43335E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61352       0.0052536       0.0015072
v  Velocity[Y]            -0.57333         0.54435       0.0030781      0.00087313
v  Velocity[Z]               1.565          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.455          360.02          87.659          169.85
v  r11                   0.0010597        0.081942        0.013068        0.018283
v  r22                   0.0011102        0.082626        0.013348        0.018643
v  r33                   0.0016344         0.17435        0.027239        0.037201
v  r12                   -0.010668        0.013604     -0.00023371     -0.00030926
v  r13                   -0.045556        0.052796      9.2684e-05       0.0010135
v  r23                   -0.046718          0.0512      3.0014e-05      0.00057434
v  epsilon                0.068583          271.36          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9712e-05       0.0099177      0.00092426       0.0017424
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2774          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71348         0.85283


 TIME FOR THE TIME STEP            10018:        0.80237E+02

===============================================================


 INSTANT    0.100190000E-01   TIME STEP NUMBER           10019
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.153743335E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.918156887E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.730501639E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.144839611E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140039317E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81111E-03   0.45720E-02 0.20041E+01 
c  Velocity[X]                                      0.13899E-03 
c  Velocity[Y]                                      0.12992E-03 
c  Velocity[Z]                                      0.43031E-02 
c  Pressure     0.36043E-04     132   0.91792E-02   0.25425E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.65761E-08   0.16163E-08 0.99581E-01 
c  r22          0.10850E-01      13   0.51605E-08   0.18022E-08 0.10121E+00 
c  r33          0.21856E-01      15   0.52368E-08   0.12366E-07 0.12678E+00 
c  r12          0.93840E-03      18   0.68290E-08   0.29992E-09 0.61007E+00 
c  r13          0.46668E-02      19   0.70585E-08   0.14993E-08 0.20011E+00 
c  r23          0.39968E-02      19   0.54278E-08   0.12744E-08 0.19892E+00 
c  epsilon      0.10971E+02      11   0.32335E-08   0.97197E-02 0.16422E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.84868E-02 0.43408E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61351       0.0052536       0.0015072
v  Velocity[Y]            -0.57337         0.54433       0.0030782      0.00087313
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                 -36.44          359.98           87.62          169.81
v  r11                   0.0010597        0.081946        0.013068        0.018283
v  r22                   0.0011102        0.082627        0.013349        0.018643
v  r33                   0.0016344         0.17437        0.027239        0.037201
v  r12                   -0.010665        0.013606     -0.00023371     -0.00030926
v  r13                   -0.045554        0.052796      9.2685e-05       0.0010135
v  r23                   -0.046718        0.051196      3.0016e-05      0.00057434
v  epsilon                0.068583          271.35          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9711e-05       0.0099177      0.00092426       0.0017424
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85282


 TIME FOR THE TIME STEP            10019:        0.79931E+02

===============================================================


 INSTANT    0.100200000E-01   TIME STEP NUMBER           10020
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.287213785E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138629392E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.115330101E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.124812529E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.271638272E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81197E-03   0.45192E-02 0.19908E+01 
c  Velocity[X]                                      0.13913E-03 
c  Velocity[Y]                                      0.12927E-03 
c  Velocity[Z]                                      0.42508E-02 
c  Pressure     0.36388E-04     133   0.92670E-02   0.25668E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.61787E-08   0.16066E-08 0.99379E-01 
c  r22          0.10850E-01      13   0.49099E-08   0.17956E-08 0.10094E+00 
c  r33          0.21856E-01      14   0.68928E-08   0.12253E-07 0.12633E+00 
c  r12          0.93840E-03      18   0.65456E-08   0.29542E-09 0.60471E+00 
c  r13          0.46668E-02      20   0.59591E-08   0.14707E-08 0.19869E+00 
c  r23          0.39968E-02      19   0.53025E-08   0.12603E-08 0.19815E+00 
c  epsilon      0.10971E+02      11   0.32954E-08   0.96378E-02 0.16272E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.84416E-02 0.43346E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161987


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61352       0.0052536       0.0015072
v  Velocity[Y]             -0.5733         0.54439       0.0030783      0.00087318
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.463          360.06          87.678          169.88
v  r11                   0.0010597        0.081942        0.013068        0.018283
v  r22                   0.0011102        0.082628        0.013349        0.018643
v  r33                   0.0016344         0.17439        0.027239        0.037201
v  r12                   -0.010662        0.013597     -0.00023371     -0.00030926
v  r13                   -0.045553        0.052796      9.2687e-05       0.0010135
v  r23                   -0.046719        0.051192      3.0017e-05      0.00057434
v  epsilon                0.068583          271.37          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.971e-05       0.0099178      0.00092427       0.0017424
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2782          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71348         0.85283


 TIME FOR THE TIME STEP            10020:        0.79441E+02

===============================================================


 INSTANT    0.100210000E-01   TIME STEP NUMBER           10021
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.384409184E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276415088E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.170888978E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.941548093E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.216339130E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81165E-03   0.45429E-02 0.19955E+01 
c  Velocity[X]                                      0.13954E-03 
c  Velocity[Y]                                      0.13026E-03 
c  Velocity[Z]                                      0.42731E-02 
c  Pressure     0.36591E-04     134   0.93082E-02   0.25812E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.62301E-08   0.16660E-08 0.10089E+00 
c  r22          0.10850E-01      13   0.51339E-08   0.18578E-08 0.10224E+00 
c  r33          0.21856E-01      15   0.52706E-08   0.12818E-07 0.12887E+00 
c  r12          0.93840E-03      18   0.69632E-08   0.30680E-09 0.61319E+00 
c  r13          0.46668E-02      20   0.62437E-08   0.15254E-08 0.20144E+00 
c  r23          0.39968E-02      19   0.57792E-08   0.13198E-08 0.20277E+00 
c  epsilon      0.10971E+02      11   0.34230E-08   0.10358E-01 0.17216E+00 
c  TempC        0.25716E+06      16   0.15099E-04   0.84082E-02 0.43282E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61353       0.0052536       0.0015072
v  Velocity[Y]            -0.57335         0.54449       0.0030783      0.00087322
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.398          360.07          87.668          169.89
v  r11                   0.0010597        0.081945        0.013068        0.018283
v  r22                   0.0011102        0.082629        0.013349        0.018643
v  r33                   0.0016344         0.17438        0.027239        0.037201
v  r12                    -0.01066        0.013597     -0.00023371     -0.00030926
v  r13                   -0.045558        0.052795      9.2688e-05       0.0010135
v  r23                   -0.046718        0.051209      3.0016e-05      0.00057434
v  epsilon                0.068583          271.39          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9709e-05       0.0099178      0.00092427       0.0017424
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2783          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71348         0.85282


 TIME FOR THE TIME STEP            10021:        0.81857E+02

===============================================================


 INSTANT    0.100220000E-01   TIME STEP NUMBER           10022
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151864748E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.242524013E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.260148070E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.476854076E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.467715909E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      40   0.81194E-03   0.45386E-02 0.19953E+01 
c  Velocity[X]                                      0.13885E-03 
c  Velocity[Y]                                      0.13026E-03 
c  Velocity[Z]                                      0.42695E-02 
c  Pressure     0.36088E-04     132   0.91865E-02   0.25457E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57294E-08   0.16230E-08 0.99526E-01 
c  r22          0.10850E-01      13   0.53230E-08   0.18219E-08 0.10221E+00 
c  r33          0.21856E-01      15   0.59823E-08   0.12403E-07 0.12759E+00 
c  r12          0.93840E-03      18   0.66389E-08   0.30141E-09 0.61035E+00 
c  r13          0.46668E-02      20   0.59594E-08   0.14851E-08 0.20036E+00 
c  r23          0.39968E-02      19   0.62702E-08   0.12783E-08 0.19905E+00 
c  epsilon      0.10971E+02      11   0.34731E-08   0.94133E-02 0.16289E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84170E-02 0.43273E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61348       0.0052537       0.0015073
v  Velocity[Y]            -0.57332         0.54426       0.0030783      0.00087317
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                 -36.45          359.94          87.622          169.79
v  r11                   0.0010597        0.081942        0.013068        0.018283
v  r22                   0.0011102        0.082629        0.013349        0.018643
v  r33                   0.0016344         0.17435        0.027239        0.037201
v  r12                   -0.010661        0.013598     -0.00023371     -0.00030926
v  r13                   -0.045554        0.052795      9.2689e-05       0.0010135
v  r23                   -0.046718        0.051197      3.0017e-05      0.00057434
v  epsilon                0.068583          271.34          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9709e-05       0.0099179      0.00092427       0.0017424
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2782          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71348         0.85283


 TIME FOR THE TIME STEP            10022:        0.78042E+02

===============================================================


 INSTANT    0.100230000E-01   TIME STEP NUMBER           10023
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.755308179E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.377279468E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.312010025E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.946219878E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.635583610E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81129E-03   0.45547E-02 0.20005E+01 
c  Velocity[X]                                      0.13952E-03 
c  Velocity[Y]                                      0.12943E-03 
c  Velocity[Z]                                      0.42858E-02 
c  Pressure     0.36743E-04     134   0.93529E-02   0.25918E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59779E-08   0.16405E-08 0.10039E+00 
c  r22          0.10850E-01      13   0.51836E-08   0.17946E-08 0.10126E+00 
c  r33          0.21856E-01      15   0.54461E-08   0.12350E-07 0.12736E+00 
c  r12          0.93840E-03      18   0.62557E-08   0.29475E-09 0.60962E+00 
c  r13          0.46668E-02      19   0.69808E-08   0.14587E-08 0.19945E+00 
c  r23          0.39968E-02      19   0.70612E-08   0.12711E-08 0.19951E+00 
c  epsilon      0.10971E+02      11   0.32800E-08   0.95720E-02 0.16300E+00 
c  TempC        0.25716E+06      16   0.15079E-04   0.85256E-02 0.43578E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61356       0.0052537       0.0015073
v  Velocity[Y]            -0.57329          0.5444       0.0030783       0.0008732
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.432          360.03          87.652          169.86
v  r11                   0.0010597        0.081952        0.013068        0.018283
v  r22                   0.0011103        0.082629        0.013349        0.018643
v  r33                   0.0016344         0.17437        0.027239        0.037201
v  r12                   -0.010664        0.013591     -0.00023371     -0.00030926
v  r13                   -0.045554        0.052795       9.269e-05       0.0010135
v  r23                   -0.046717        0.051181      3.0018e-05      0.00057434
v  epsilon                0.068583          271.36          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9711e-05        0.009918      0.00092427       0.0017424
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2782          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71348         0.85283


 TIME FOR THE TIME STEP            10023:        0.78757E+02

===============================================================


 INSTANT    0.100240000E-01   TIME STEP NUMBER           10024
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.266028667E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.168873154E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.207601726E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.172795499E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183232392E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81262E-03   0.45318E-02 0.19935E+01 
c  Velocity[X]                                      0.13854E-03 
c  Velocity[Y]                                      0.12936E-03 
c  Velocity[Z]                                      0.42639E-02 
c  Pressure     0.36555E-04     132   0.93065E-02   0.25786E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59713E-08   0.16694E-08 0.10091E+00 
c  r22          0.10850E-01      13   0.53452E-08   0.18614E-08 0.10232E+00 
c  r33          0.21856E-01      15   0.52275E-08   0.12799E-07 0.12872E+00 
c  r12          0.93840E-03      18   0.62028E-08   0.30095E-09 0.61196E+00 
c  r13          0.46668E-02      19   0.65438E-08   0.15296E-08 0.20098E+00 
c  r23          0.39968E-02      19   0.64931E-08   0.13039E-08 0.20121E+00 
c  epsilon      0.10971E+02      11   0.34454E-08   0.10142E-01 0.16740E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84367E-02 0.43344E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61353       0.0052538       0.0015073
v  Velocity[Y]             -0.5732         0.54437       0.0030783      0.00087323
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.461          360.05          87.679          169.89
v  r11                   0.0010597        0.081952        0.013068        0.018283
v  r22                   0.0011103         0.08263        0.013349        0.018643
v  r33                   0.0016345         0.17439        0.027239        0.037201
v  r12                   -0.010667        0.013587     -0.00023372     -0.00030926
v  r13                   -0.045557        0.052798      9.2691e-05       0.0010135
v  r23                   -0.046716        0.051201      3.0019e-05      0.00057434
v  epsilon                0.068583          271.37          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.971e-05       0.0099179      0.00092427       0.0017424
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2782          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71348         0.85283


 TIME FOR THE TIME STEP            10024:        0.81705E+02

===============================================================


 INSTANT    0.100250000E-01   TIME STEP NUMBER           10025
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.152463287E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.161224939E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.115422885E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.836617914E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.475064980E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81044E-03   0.45460E-02 0.19979E+01 
c  Velocity[X]                                      0.13919E-03 
c  Velocity[Y]                                      0.12984E-03 
c  Velocity[Z]                                      0.42769E-02 
c  Pressure     0.36526E-04     134   0.92963E-02   0.25765E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55963E-08   0.16545E-08 0.99937E-01 
c  r22          0.10850E-01      13   0.48772E-08   0.18149E-08 0.10144E+00 
c  r33          0.21856E-01      15   0.59073E-08   0.12477E-07 0.12731E+00 
c  r12          0.93840E-03      18   0.56411E-08   0.29398E-09 0.60363E+00 
c  r13          0.46668E-02      20   0.57911E-08   0.14831E-08 0.19935E+00 
c  r23          0.39968E-02      19   0.70299E-08   0.12880E-08 0.19896E+00 
c  epsilon      0.10971E+02      11   0.36287E-08   0.98637E-02 0.16539E+00 
c  TempC        0.25716E+06      16   0.15124E-04   0.83822E-02 0.43155E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385          0.6135       0.0052538       0.0015073
v  Velocity[Y]            -0.57319         0.54443       0.0030783      0.00087323
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.419          360.08           87.68          169.89
v  r11                   0.0010597        0.081953        0.013068        0.018283
v  r22                   0.0011103        0.082626        0.013349        0.018643
v  r33                   0.0016345         0.17437        0.027239        0.037201
v  r12                   -0.010667        0.013585     -0.00023372     -0.00030926
v  r13                   -0.045556        0.052799      9.2692e-05       0.0010135
v  r23                   -0.046716        0.051193      3.0019e-05      0.00057434
v  epsilon                0.068583          271.38          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9711e-05       0.0099177      0.00092427       0.0017424
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017902           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85283


 TIME FOR THE TIME STEP            10025:        0.81368E+02

===============================================================


 INSTANT    0.100260000E-01   TIME STEP NUMBER           10026
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.796450524E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.128938522E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.162869685E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.228506487E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.895052579E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81256E-03   0.45473E-02 0.19978E+01 
c  Velocity[X]                                      0.13977E-03 
c  Velocity[Y]                                      0.13073E-03 
c  Velocity[Z]                                      0.42768E-02 
c  Pressure     0.36895E-04     132   0.93952E-02   0.26026E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57258E-08   0.16610E-08 0.10028E+00 
c  r22          0.10850E-01      13   0.48038E-08   0.18595E-08 0.10223E+00 
c  r33          0.21856E-01      15   0.52652E-08   0.12703E-07 0.12793E+00 
c  r12          0.93840E-03      18   0.57892E-08   0.29658E-09 0.60443E+00 
c  r13          0.46668E-02      19   0.68728E-08   0.15117E-08 0.20050E+00 
c  r23          0.39968E-02      19   0.64433E-08   0.12850E-08 0.19869E+00 
c  epsilon      0.10971E+02      11   0.35160E-08   0.10112E-01 0.16692E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.84748E-02 0.43415E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61354       0.0052538       0.0015073
v  Velocity[Y]            -0.57322         0.54452       0.0030783       0.0008732
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.472          359.99          87.652          169.83
v  r11                   0.0010597        0.081947        0.013068        0.018283
v  r22                   0.0011103        0.082629        0.013349        0.018643
v  r33                   0.0016345         0.17434        0.027239        0.037201
v  r12                   -0.010674        0.013586     -0.00023372     -0.00030926
v  r13                   -0.045554          0.0528      9.2694e-05       0.0010135
v  r23                   -0.046715        0.051187       3.002e-05      0.00057435
v  epsilon                0.068583          271.33          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9712e-05       0.0099176      0.00092427       0.0017424
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2772          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71348         0.85283


 TIME FOR THE TIME STEP            10026:        0.83080E+02

===============================================================


 INSTANT    0.100270000E-01   TIME STEP NUMBER           10027
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.670245051E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.379765246E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.218230384E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.264361923E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.414093406E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11251E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      40   0.81166E-03   0.45533E-02 0.19971E+01 
c  Velocity[X]                                      0.13888E-03 
c  Velocity[Y]                                      0.12946E-03 
c  Velocity[Z]                                      0.42849E-02 
c  Pressure     0.36145E-04     133   0.92051E-02   0.25495E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55455E-08   0.16554E-08 0.10075E+00 
c  r22          0.10850E-01      13   0.47328E-08   0.18112E-08 0.10137E+00 
c  r33          0.21856E-01      14   0.69455E-08   0.12544E-07 0.12801E+00 
c  r12          0.93840E-03      18   0.53148E-08   0.29379E-09 0.60629E+00 
c  r13          0.46668E-02      19   0.57601E-08   0.14904E-08 0.19956E+00 
c  r23          0.39968E-02      19   0.59668E-08   0.12875E-08 0.20020E+00 
c  epsilon      0.10971E+02      11   0.34083E-08   0.10051E-01 0.17102E+00 
c  TempC        0.25716E+06      16   0.15095E-04   0.84333E-02 0.43323E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61353       0.0052538       0.0015073
v  Velocity[Y]            -0.57353         0.54429       0.0030784      0.00087324
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                 -36.39          360.06          87.671          169.88
v  r11                   0.0010598        0.081947        0.013069        0.018283
v  r22                   0.0011103         0.08263        0.013349        0.018643
v  r33                   0.0016345         0.17435        0.027239        0.037201
v  r12                   -0.010677         0.01358     -0.00023372     -0.00030926
v  r13                   -0.045556        0.052797      9.2695e-05       0.0010135
v  r23                   -0.046715        0.051174       3.002e-05      0.00057434
v  epsilon                0.068583          271.33          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9714e-05       0.0099175      0.00092427       0.0017424
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2775          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71348         0.85282


 TIME FOR THE TIME STEP            10027:        0.81005E+02

===============================================================


 INSTANT    0.100280000E-01   TIME STEP NUMBER           10028
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120210749E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.151906927E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.416009698E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.460809754E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.888819453E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81243E-03   0.45444E-02 0.19956E+01 
c  Velocity[X]                                      0.13937E-03 
c  Velocity[Y]                                      0.12902E-03 
c  Velocity[Z]                                      0.42760E-02 
c  Pressure     0.36264E-04     133   0.92356E-02   0.25581E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55929E-08   0.16273E-08 0.99615E-01 
c  r22          0.10850E-01      13   0.48523E-08   0.17824E-08 0.10085E+00 
c  r33          0.21856E-01      15   0.53292E-08   0.12398E-07 0.12683E+00 
c  r12          0.93840E-03      18   0.52007E-08   0.29712E-09 0.60455E+00 
c  r13          0.46668E-02      19   0.65748E-08   0.14752E-08 0.19927E+00 
c  r23          0.39968E-02      19   0.57598E-08   0.12789E-08 0.19863E+00 
c  epsilon      0.10971E+02      11   0.33490E-08   0.98869E-02 0.16563E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.84203E-02 0.43346E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61347       0.0052538       0.0015073
v  Velocity[Y]            -0.57345         0.54442       0.0030783       0.0008732
v  Velocity[Z]              1.5649          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4369          4.3406          4.3632
v  Pressure                -36.431          360.08          87.688          169.89
v  r11                   0.0010598        0.081948        0.013069        0.018283
v  r22                   0.0011103        0.082632        0.013349        0.018643
v  r33                   0.0016345         0.17437        0.027239        0.037201
v  r12                   -0.010679         0.01358     -0.00023372     -0.00030926
v  r13                   -0.045554        0.052797      9.2696e-05       0.0010135
v  r23                   -0.046715        0.051205      3.0021e-05      0.00057435
v  epsilon                0.068584          271.35          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9715e-05       0.0099174      0.00092428       0.0017424
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2766          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71348         0.85282


 TIME FOR THE TIME STEP            10028:        0.81408E+02

===============================================================


 INSTANT    0.100290000E-01   TIME STEP NUMBER           10029
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.134545039E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.260552456E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.676112431E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.493443656E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.318146812E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81161E-03   0.45355E-02 0.19943E+01 
c  Velocity[X]                                      0.13926E-03 
c  Velocity[Y]                                      0.12941E-03 
c  Velocity[Z]                                      0.42669E-02 
c  Pressure     0.36544E-04     132   0.93055E-02   0.25779E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54652E-08   0.16256E-08 0.99373E-01 
c  r22          0.10850E-01      13   0.50743E-08   0.17860E-08 0.10042E+00 
c  r33          0.21856E-01      15   0.59582E-08   0.12232E-07 0.12563E+00 
c  r12          0.93840E-03      18   0.51541E-08   0.29312E-09 0.60337E+00 
c  r13          0.46668E-02      19   0.66975E-08   0.14637E-08 0.19792E+00 
c  r23          0.39968E-02      19   0.64172E-08   0.12587E-08 0.19698E+00 
c  epsilon      0.10971E+02      11   0.35276E-08   0.97364E-02 0.16366E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.84680E-02 0.43388E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61352       0.0052538       0.0015073
v  Velocity[Y]            -0.57349         0.54436       0.0030784      0.00087324
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                 -36.42          360.14          87.703          169.93
v  r11                   0.0010598        0.081953        0.013069        0.018283
v  r22                   0.0011103        0.082632        0.013349        0.018643
v  r33                   0.0016345         0.17435        0.027239        0.037201
v  r12                   -0.010681        0.013576     -0.00023372     -0.00030926
v  r13                   -0.045555        0.052795      9.2699e-05       0.0010135
v  r23                   -0.046715        0.051198      3.0023e-05      0.00057435
v  epsilon                0.068584          271.36          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9717e-05       0.0099174      0.00092428       0.0017424
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2767          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767         0.71348         0.85282


 TIME FOR THE TIME STEP            10029:        0.82258E+02

===============================================================


 INSTANT    0.100300000E-01   TIME STEP NUMBER           10030
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.211352831E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.205030375E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.224506881E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.197924021E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.152930901E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81203E-03   0.45329E-02 0.19928E+01 
c  Velocity[X]                                      0.13811E-03 
c  Velocity[Y]                                      0.12987E-03 
c  Velocity[Z]                                      0.42649E-02 
c  Pressure     0.36285E-04     131   0.92365E-02   0.25595E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52608E-08   0.16189E-08 0.99051E-01 
c  r22          0.10850E-01      13   0.46347E-08   0.18101E-08 0.10081E+00 
c  r33          0.21856E-01      14   0.64075E-08   0.12421E-07 0.12627E+00 
c  r12          0.93840E-03      17   0.66687E-08   0.29104E-09 0.60003E+00 
c  r13          0.46668E-02      19   0.53107E-08   0.14800E-08 0.19808E+00 
c  r23          0.39968E-02      19   0.56786E-08   0.12691E-08 0.19756E+00 
c  epsilon      0.10971E+02      11   0.32955E-08   0.10131E-01 0.16738E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.83677E-02 0.43110E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388          0.6135       0.0052538       0.0015073
v  Velocity[Y]            -0.57346         0.54441       0.0030783      0.00087319
v  Velocity[Z]              1.5649          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5787          5.4369          4.3406          4.3632
v  Pressure                -36.435             360          87.645          169.84
v  r11                   0.0010598        0.081949        0.013069        0.018283
v  r22                   0.0011103        0.082633        0.013349        0.018643
v  r33                   0.0016345         0.17431        0.027239        0.037201
v  r12                    -0.01068        0.013579     -0.00023372     -0.00030926
v  r13                   -0.045557        0.052796      9.2699e-05       0.0010135
v  r23                   -0.046715        0.051194      3.0023e-05      0.00057435
v  epsilon                0.068584          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9716e-05       0.0099176      0.00092428       0.0017424
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2774          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71348         0.85283


 TIME FOR THE TIME STEP            10030:        0.84056E+02

===============================================================


 INSTANT    0.100310000E-01   TIME STEP NUMBER           10031
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.329090100E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319673111E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.303022263E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.401882963E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.438870965E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81098E-03   0.45604E-02 0.20013E+01 
c  Velocity[X]                                      0.13957E-03 
c  Velocity[Y]                                      0.13016E-03 
c  Velocity[Z]                                      0.42906E-02 
c  Pressure     0.36388E-04     133   0.92633E-02   0.25668E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.53401E-08   0.16249E-08 0.99315E-01 
c  r22          0.10850E-01      13   0.47717E-08   0.18079E-08 0.10102E+00 
c  r33          0.21856E-01      14   0.66430E-08   0.12347E-07 0.12647E+00 
c  r12          0.93840E-03      18   0.50284E-08   0.30115E-09 0.60840E+00 
c  r13          0.46668E-02      19   0.60825E-08   0.14683E-08 0.19810E+00 
c  r23          0.39968E-02      19   0.55228E-08   0.12685E-08 0.19762E+00 
c  epsilon      0.10971E+02      11   0.31994E-08   0.99189E-02 0.16577E+00 
c  TempC        0.25716E+06      16   0.15108E-04   0.84443E-02 0.43345E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393         0.61349       0.0052537       0.0015073
v  Velocity[Y]            -0.57349         0.54451       0.0030783      0.00087321
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.401          360.01          87.657          169.85
v  r11                   0.0010598        0.081951        0.013069        0.018283
v  r22                   0.0011103        0.082632        0.013349        0.018643
v  r33                   0.0016345         0.17433        0.027239        0.037201
v  r12                   -0.010676        0.013575     -0.00023372     -0.00030926
v  r13                   -0.045554        0.052794      9.2701e-05       0.0010135
v  r23                   -0.046715        0.051222      3.0024e-05      0.00057435
v  epsilon                0.068584          271.33          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9718e-05       0.0099177      0.00092428       0.0017424
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2779          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71348         0.85282


 TIME FOR THE TIME STEP            10031:        0.85343E+02

===============================================================


 INSTANT    0.100320000E-01   TIME STEP NUMBER           10032
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.401175728E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200830318E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.299921879E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.108581657E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.502164839E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81236E-03   0.45369E-02 0.19948E+01 
c  Velocity[X]                                      0.13894E-03 
c  Velocity[Y]                                      0.12908E-03 
c  Velocity[Z]                                      0.42689E-02 
c  Pressure     0.36585E-04     133   0.93138E-02   0.25808E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50814E-08   0.16279E-08 0.99907E-01 
c  r22          0.10850E-01      13   0.47918E-08   0.18157E-08 0.10111E+00 
c  r33          0.21856E-01      15   0.52660E-08   0.12449E-07 0.12681E+00 
c  r12          0.93840E-03      17   0.69112E-08   0.29780E-09 0.60437E+00 
c  r13          0.46668E-02      18   0.67464E-08   0.15022E-08 0.19891E+00 
c  r23          0.39968E-02      18   0.69451E-08   0.12821E-08 0.19884E+00 
c  epsilon      0.10971E+02      11   0.34020E-08   0.98954E-02 0.16554E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.84306E-02 0.43377E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373          0.6135       0.0052538       0.0015073
v  Velocity[Y]            -0.57345         0.54428       0.0030783      0.00087317
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                 -36.47          360.05          87.672          169.88
v  r11                   0.0010598        0.081946        0.013069        0.018283
v  r22                   0.0011104        0.082634        0.013349        0.018643
v  r33                   0.0016346         0.17437        0.027239        0.037201
v  r12                   -0.010672        0.013577     -0.00023372     -0.00030926
v  r13                   -0.045553        0.052797      9.2702e-05       0.0010135
v  r23                   -0.046715        0.051214      3.0025e-05      0.00057435
v  epsilon                0.068584          271.34          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9718e-05       0.0099176      0.00092428       0.0017424
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017902           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85282


 TIME FOR THE TIME STEP            10032:        0.83310E+02

===============================================================


 INSTANT    0.100330000E-01   TIME STEP NUMBER           10033
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157578525E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.606524256E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.524089348E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.865045315E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100651432E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81209E-03   0.44994E-02 0.19868E+01 
c  Velocity[X]                                      0.13877E-03 
c  Velocity[Y]                                      0.12966E-03 
c  Velocity[Z]                                      0.42310E-02 
c  Pressure     0.36241E-04     132   0.92263E-02   0.25564E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52513E-08   0.16278E-08 0.10035E+00 
c  r22          0.10850E-01      13   0.50261E-08   0.17968E-08 0.10114E+00 
c  r33          0.21856E-01      14   0.67297E-08   0.12323E-07 0.12696E+00 
c  r12          0.93841E-03      18   0.48747E-08   0.29803E-09 0.60641E+00 
c  r13          0.46668E-02      18   0.63010E-08   0.14740E-08 0.19866E+00 
c  r23          0.39968E-02      18   0.66911E-08   0.12752E-08 0.19923E+00 
c  epsilon      0.10971E+02      11   0.33439E-08   0.97231E-02 0.16493E+00 
c  TempC        0.25716E+06      16   0.15105E-04   0.84000E-02 0.43283E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161986


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375          0.6135       0.0052539       0.0015073
v  Velocity[Y]            -0.57358         0.54434       0.0030783       0.0008732
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.443          360.02          87.644          169.85
v  r11                   0.0010598        0.081951        0.013069        0.018283
v  r22                   0.0011104        0.082631        0.013349        0.018644
v  r33                   0.0016346         0.17435        0.027239        0.037201
v  r12                   -0.010671        0.013572     -0.00023372     -0.00030926
v  r13                   -0.045557        0.052798      9.2703e-05       0.0010135
v  r23                   -0.046714        0.051203      3.0025e-05      0.00057435
v  epsilon                0.068584          271.36          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.972e-05       0.0099175      0.00092428       0.0017424
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2785          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71348         0.85283


 TIME FOR THE TIME STEP            10033:        0.81659E+02

===============================================================


 INSTANT    0.100340000E-01   TIME STEP NUMBER           10034
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.187370258E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.356901499E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160069951E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133816309E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201412358E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81242E-03   0.45472E-02 0.19985E+01 
c  Velocity[X]                                      0.13902E-03 
c  Velocity[Y]                                      0.13000E-03 
c  Velocity[Z]                                      0.42782E-02 
c  Pressure     0.36441E-04     133   0.92743E-02   0.25706E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50228E-08   0.16578E-08 0.10049E+00 
c  r22          0.10850E-01      13   0.49261E-08   0.17872E-08 0.10069E+00 
c  r33          0.21856E-01      15   0.53543E-08   0.12461E-07 0.12726E+00 
c  r12          0.93841E-03      17   0.68963E-08   0.30228E-09 0.60962E+00 
c  r13          0.46668E-02      19   0.54762E-08   0.14620E-08 0.19857E+00 
c  r23          0.39968E-02      18   0.68442E-08   0.13026E-08 0.20097E+00 
c  epsilon      0.10971E+02      11   0.34606E-08   0.10132E-01 0.17038E+00 
c  TempC        0.25716E+06      16   0.15165E-04   0.84674E-02 0.43349E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61344       0.0052539       0.0015073
v  Velocity[Y]            -0.57346         0.54451       0.0030783       0.0008732
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.472          360.01          87.646          169.84
v  r11                   0.0010598        0.081956        0.013069        0.018283
v  r22                   0.0011104        0.082632        0.013349        0.018644
v  r33                   0.0016346         0.17433        0.027239        0.037201
v  r12                   -0.010667        0.013574     -0.00023372     -0.00030926
v  r13                   -0.045554        0.052801      9.2704e-05       0.0010135
v  r23                   -0.046713        0.051222      3.0026e-05      0.00057435
v  epsilon                0.068584           271.3          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.972e-05       0.0099175      0.00092428       0.0017424
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2787          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71348         0.85283


 TIME FOR THE TIME STEP            10034:        0.83403E+02

===============================================================


 INSTANT    0.100350000E-01   TIME STEP NUMBER           10035
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.109582334E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.235083450E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.678010587E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.118877604E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184117961E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81146E-03   0.45841E-02 0.20040E+01 
c  Velocity[X]                                      0.13998E-03 
c  Velocity[Y]                                      0.12933E-03 
c  Velocity[Z]                                      0.43148E-02 
c  Pressure     0.36668E-04     134   0.93456E-02   0.25866E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.49513E-08   0.15991E-08 0.99275E-01 
c  r22          0.10850E-01      13   0.49453E-08   0.17573E-08 0.10013E+00 
c  r33          0.21856E-01      15   0.62727E-08   0.12125E-07 0.12597E+00 
c  r12          0.93841E-03      18   0.55211E-08   0.28977E-09 0.60054E+00 
c  r13          0.46668E-02      19   0.56561E-08   0.14363E-08 0.19726E+00 
c  r23          0.39968E-02      18   0.70409E-08   0.12613E-08 0.19782E+00 
c  epsilon      0.10971E+02      11   0.34664E-08   0.95026E-02 0.16208E+00 
c  TempC        0.25716E+06      16   0.15096E-04   0.85055E-02 0.43472E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61351       0.0052538       0.0015073
v  Velocity[Y]            -0.57349          0.5442       0.0030783      0.00087317
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.444          360.11           87.71          169.93
v  r11                   0.0010598        0.081953        0.013069        0.018284
v  r22                   0.0011104        0.082632        0.013349        0.018644
v  r33                   0.0016346         0.17434        0.027239        0.037201
v  r12                   -0.010664        0.013576     -0.00023372     -0.00030926
v  r13                   -0.045553        0.052802      9.2706e-05       0.0010135
v  r23                   -0.046712        0.051211      3.0027e-05      0.00057435
v  epsilon                0.068584          271.31          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9722e-05       0.0099174      0.00092429       0.0017424
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2791          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71348         0.85282


 TIME FOR THE TIME STEP            10035:        0.80856E+02

===============================================================


 INSTANT    0.100360000E-01   TIME STEP NUMBER           10036
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111641058E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.549417349E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129666244E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.261565915E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.679389043E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81310E-03   0.45182E-02 0.19896E+01 
c  Velocity[X]                                      0.13834E-03 
c  Velocity[Y]                                      0.12925E-03 
c  Velocity[Z]                                      0.42507E-02 
c  Pressure     0.36229E-04     133   0.92243E-02   0.25555E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50342E-08   0.16368E-08 0.99636E-01 
c  r22          0.10850E-01      13   0.51654E-08   0.17907E-08 0.10066E+00 
c  r33          0.21856E-01      15   0.59032E-08   0.12368E-07 0.12635E+00 
c  r12          0.93841E-03      18   0.57655E-08   0.29424E-09 0.60405E+00 
c  r13          0.46668E-02      19   0.62544E-08   0.14590E-08 0.19806E+00 
c  r23          0.39968E-02      19   0.53486E-08   0.12931E-08 0.19900E+00 
c  epsilon      0.10971E+02      11   0.33341E-08   0.99877E-02 0.16669E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.83760E-02 0.43212E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61347       0.0052539       0.0015073
v  Velocity[Y]            -0.57332          0.5442       0.0030783      0.00087317
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.416          360.07          87.692           169.9
v  r11                   0.0010598        0.081948        0.013069        0.018284
v  r22                   0.0011104        0.082637        0.013349        0.018644
v  r33                   0.0016346         0.17436        0.027239        0.037201
v  r12                   -0.010671        0.013574     -0.00023372     -0.00030926
v  r13                   -0.045556          0.0528      9.2707e-05       0.0010135
v  r23                   -0.046712        0.051205      3.0028e-05      0.00057435
v  epsilon                0.068584          271.33          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9724e-05       0.0099174      0.00092429       0.0017424
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2799          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8799         0.71348         0.85283


 TIME FOR THE TIME STEP            10036:        0.83089E+02

===============================================================


 INSTANT    0.100370000E-01   TIME STEP NUMBER           10037
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.909656612E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172788940E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.126081589E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.400817257E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.142533095E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81080E-03   0.45325E-02 0.19928E+01 
c  Velocity[X]                                      0.13790E-03 
c  Velocity[Y]                                      0.12956E-03 
c  Velocity[Z]                                      0.42651E-02 
c  Pressure     0.36276E-04     133   0.92398E-02   0.25589E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50596E-08   0.16318E-08 0.99656E-01 
c  r22          0.10850E-01      13   0.50974E-08   0.18025E-08 0.10103E+00 
c  r33          0.21856E-01      15   0.55027E-08   0.12443E-07 0.12694E+00 
c  r12          0.93841E-03      18   0.59650E-08   0.29669E-09 0.60606E+00 
c  r13          0.46668E-02      19   0.56116E-08   0.14883E-08 0.19964E+00 
c  r23          0.39968E-02      19   0.52865E-08   0.12900E-08 0.19915E+00 
c  epsilon      0.10971E+02      11   0.31361E-08   0.99104E-02 0.16545E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84263E-02 0.43342E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61343       0.0052538       0.0015073
v  Velocity[Y]            -0.57334         0.54435       0.0030783      0.00087316
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                  -36.4          360.09          87.698          169.91
v  r11                   0.0010598        0.081951        0.013069        0.018284
v  r22                   0.0011104         0.08264        0.013349        0.018644
v  r33                   0.0016346         0.17434        0.027239        0.037201
v  r12                   -0.010669         0.01358     -0.00023372     -0.00030926
v  r13                   -0.045555        0.052797      9.2708e-05       0.0010135
v  r23                   -0.046712        0.051225      3.0028e-05      0.00057435
v  epsilon                0.068584          271.33          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9726e-05       0.0099174      0.00092429       0.0017424
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2796          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8796         0.71348         0.85282


 TIME FOR THE TIME STEP            10037:        0.83233E+02

===============================================================


 INSTANT    0.100380000E-01   TIME STEP NUMBER           10038
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.116394704E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.544131200E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.101418674E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.506764362E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106108240E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81223E-03   0.45528E-02 0.20008E+01 
c  Velocity[X]                                      0.13959E-03 
c  Velocity[Y]                                      0.13090E-03 
c  Velocity[Z]                                      0.42823E-02 
c  Pressure     0.36652E-04     131   0.93355E-02   0.25855E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50253E-08   0.16298E-08 0.99597E-01 
c  r22          0.10850E-01      13   0.52328E-08   0.17759E-08 0.10050E+00 
c  r33          0.21856E-01      15   0.56544E-08   0.12370E-07 0.12671E+00 
c  r12          0.93841E-03      18   0.51445E-08   0.29665E-09 0.60782E+00 
c  r13          0.46668E-02      19   0.52734E-08   0.14510E-08 0.19781E+00 
c  r23          0.39968E-02      19   0.56356E-08   0.12887E-08 0.19866E+00 
c  epsilon      0.10971E+02      11   0.33878E-08   0.99597E-02 0.16619E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.84426E-02 0.43296E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61347       0.0052539       0.0015073
v  Velocity[Y]            -0.57338         0.54408       0.0030782       0.0008731
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                 -36.47          360.02          87.671          169.86
v  r11                   0.0010598        0.081949        0.013069        0.018284
v  r22                   0.0011104        0.082641        0.013349        0.018644
v  r33                   0.0016347         0.17433        0.027239        0.037201
v  r12                   -0.010668        0.013579     -0.00023372     -0.00030926
v  r13                   -0.045554        0.052796       9.271e-05       0.0010135
v  r23                   -0.046713        0.051211       3.003e-05      0.00057436
v  epsilon                0.068584           271.3          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9726e-05       0.0099176      0.00092429       0.0017424
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2783          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71348         0.85282


 TIME FOR THE TIME STEP            10038:        0.80913E+02

===============================================================


 INSTANT    0.100390000E-01   TIME STEP NUMBER           10039
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.865813485E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237212304E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.259696483E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.179218170E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.418484024E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      45   0.81232E-03   0.45572E-02 0.20004E+01 
c  Velocity[X]                                      0.13907E-03 
c  Velocity[Y]                                      0.12956E-03 
c  Velocity[Z]                                      0.42886E-02 
c  Pressure     0.36447E-04     132   0.92808E-02   0.25710E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.51575E-08   0.16392E-08 0.99698E-01 
c  r22          0.10850E-01      13   0.53322E-08   0.18135E-08 0.10102E+00 
c  r33          0.21856E-01      15   0.52263E-08   0.12495E-07 0.12711E+00 
c  r12          0.93841E-03      18   0.58543E-08   0.29635E-09 0.60860E+00 
c  r13          0.46668E-02      18   0.65746E-08   0.14822E-08 0.19892E+00 
c  r23          0.39968E-02      19   0.53667E-08   0.12798E-08 0.19846E+00 
c  epsilon      0.10971E+02      11   0.34103E-08   0.10019E-01 0.16594E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.84706E-02 0.43394E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61352       0.0052538       0.0015073
v  Velocity[Y]            -0.57352         0.54388       0.0030783      0.00087314
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                 -36.42          360.03          87.652          169.86
v  r11                   0.0010598        0.081959        0.013069        0.018284
v  r22                   0.0011104         0.08264        0.013349        0.018644
v  r33                   0.0016347         0.17434        0.027239        0.037201
v  r12                   -0.010667        0.013582     -0.00023372     -0.00030926
v  r13                   -0.045556        0.052795      9.2711e-05       0.0010135
v  r23                   -0.046713        0.051196      3.0031e-05      0.00057436
v  epsilon                0.068584          271.33          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9726e-05       0.0099178      0.00092429       0.0017424
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85282


 TIME FOR THE TIME STEP            10039:        0.81249E+02

===============================================================


 INSTANT    0.100400000E-01   TIME STEP NUMBER           10040
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.204622486E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.255524427E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.185209453E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.103665365E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.464059069E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40364E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81209E-03   0.45482E-02 0.19963E+01 
c  Velocity[X]                                      0.13959E-03 
c  Velocity[Y]                                      0.12916E-03 
c  Velocity[Z]                                      0.42795E-02 
c  Pressure     0.36492E-04     134   0.92898E-02   0.25742E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.51931E-08   0.16544E-08 0.10016E+00 
c  r22          0.10850E-01      13   0.50463E-08   0.18291E-08 0.10159E+00 
c  r33          0.21856E-01      15   0.53664E-08   0.12697E-07 0.12813E+00 
c  r12          0.93841E-03      18   0.57987E-08   0.29960E-09 0.60796E+00 
c  r13          0.46668E-02      19   0.52347E-08   0.15167E-08 0.20082E+00 
c  r23          0.39968E-02      19   0.58925E-08   0.12987E-08 0.20030E+00 
c  epsilon      0.10971E+02      11   0.33461E-08   0.10590E-01 0.17349E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.84340E-02 0.43338E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61347       0.0052538       0.0015073
v  Velocity[Y]            -0.57337          0.5439       0.0030783      0.00087312
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.437             360          87.652          169.84
v  r11                   0.0010598        0.081964        0.013069        0.018284
v  r22                   0.0011105         0.08264        0.013349        0.018644
v  r33                   0.0016347         0.17437        0.027239        0.037201
v  r12                   -0.010668        0.013582     -0.00023372     -0.00030926
v  r13                   -0.045554        0.052798      9.2713e-05       0.0010135
v  r23                   -0.046714        0.051232      3.0031e-05      0.00057436
v  epsilon                0.068584          271.33          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9723e-05       0.0099179      0.00092429       0.0017424
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2775          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71348         0.85282


 TIME FOR THE TIME STEP            10040:        0.78706E+02

===============================================================


 INSTANT    0.100410000E-01   TIME STEP NUMBER           10041
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200326503E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.493034180E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.306863651E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.292637403E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.451755823E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      40   0.81097E-03   0.45540E-02 0.19991E+01 
c  Velocity[X]                                      0.13956E-03 
c  Velocity[Y]                                      0.12976E-03 
c  Velocity[Z]                                      0.42847E-02 
c  Pressure     0.36527E-04     132   0.93084E-02   0.25767E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.51958E-08   0.16174E-08 0.99353E-01 
c  r22          0.10850E-01      13   0.53676E-08   0.17817E-08 0.10065E+00 
c  r33          0.21856E-01      14   0.68957E-08   0.12218E-07 0.12633E+00 
c  r12          0.93841E-03      18   0.61480E-08   0.29238E-09 0.60529E+00 
c  r13          0.46668E-02      19   0.64089E-08   0.14567E-08 0.19786E+00 
c  r23          0.39968E-02      20   0.63597E-08   0.12646E-08 0.19755E+00 
c  epsilon      0.10971E+02      11   0.32579E-08   0.94666E-02 0.16191E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.84197E-02 0.43329E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61351       0.0052538       0.0015072
v  Velocity[Y]            -0.57341          0.5441       0.0030782      0.00087309
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.437          360.12           87.72          169.94
v  r11                   0.0010598        0.081971        0.013069        0.018284
v  r22                   0.0011105         0.08264        0.013349        0.018644
v  r33                   0.0016347         0.17436        0.027239        0.037201
v  r12                   -0.010668        0.013581     -0.00023372     -0.00030926
v  r13                   -0.045555        0.052798      9.2715e-05       0.0010135
v  r23                   -0.046715        0.051221      3.0032e-05      0.00057436
v  epsilon                0.068585          271.33          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9718e-05        0.009918      0.00092429       0.0017424
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2779          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71348         0.85283


 TIME FOR THE TIME STEP            10041:        0.77263E+02

===============================================================


 INSTANT    0.100420000E-01   TIME STEP NUMBER           10042
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.196681294E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267975446E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.810804360E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108155319E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.326572461E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      44   0.81316E-03   0.45238E-02 0.19918E+01 
c  Velocity[X]                                      0.13842E-03 
c  Velocity[Y]                                      0.12952E-03 
c  Velocity[Z]                                      0.42559E-02 
c  Pressure     0.36591E-04     133   0.93214E-02   0.25812E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.53058E-08   0.16151E-08 0.99283E-01 
c  r22          0.10850E-01      13   0.55413E-08   0.17695E-08 0.10091E+00 
c  r33          0.21856E-01      15   0.53150E-08   0.12228E-07 0.12659E+00 
c  r12          0.93841E-03      18   0.61423E-08   0.29115E-09 0.60265E+00 
c  r13          0.46668E-02      19   0.66515E-08   0.14593E-08 0.19852E+00 
c  r23          0.39968E-02      20   0.65066E-08   0.12762E-08 0.19849E+00 
c  epsilon      0.10971E+02      11   0.32388E-08   0.95107E-02 0.16258E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.84133E-02 0.43280E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162016


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339          0.6135       0.0052538       0.0015073
v  Velocity[Y]            -0.57331          0.5443       0.0030782      0.00087306
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4369          4.3406          4.3632
v  Pressure                -36.442           360.1          87.702          169.91
v  r11                   0.0010598        0.081972        0.013069        0.018284
v  r22                   0.0011105        0.082641        0.013349        0.018644
v  r33                   0.0016347         0.17433         0.02724        0.037201
v  r12                   -0.010666        0.013583     -0.00023372     -0.00030926
v  r13                   -0.045557          0.0528      9.2717e-05       0.0010135
v  r23                   -0.046716        0.051215      3.0033e-05      0.00057436
v  epsilon                0.068585          271.29          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9715e-05        0.009918       0.0009243       0.0017424
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2783          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71348         0.85282


 TIME FOR THE TIME STEP            10042:        0.78221E+02

===============================================================


 INSTANT    0.100430000E-01   TIME STEP NUMBER           10043
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.612744462E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.373933141E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237491273E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.426138579E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.165963328E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81149E-03   0.45768E-02 0.20029E+01 
c  Velocity[X]                                      0.13984E-03 
c  Velocity[Y]                                      0.12991E-03 
c  Velocity[Z]                                      0.43071E-02 
c  Pressure     0.36705E-04     133   0.93455E-02   0.25892E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54958E-08   0.16254E-08 0.99437E-01 
c  r22          0.10850E-01      13   0.57485E-08   0.17915E-08 0.10117E+00 
c  r33          0.21856E-01      15   0.54352E-08   0.12380E-07 0.12701E+00 
c  r12          0.93841E-03      18   0.62101E-08   0.29580E-09 0.60435E+00 
c  r13          0.46668E-02      19   0.67264E-08   0.14584E-08 0.19841E+00 
c  r23          0.39968E-02      20   0.60171E-08   0.12793E-08 0.19883E+00 
c  epsilon      0.10971E+02      11   0.33334E-08   0.97214E-02 0.16451E+00 
c  TempC        0.25716E+06      16   0.15103E-04   0.84420E-02 0.43365E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162017


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61347       0.0052539       0.0015073
v  Velocity[Y]             -0.5734         0.54415       0.0030782      0.00087308
v  Velocity[Z]              1.5649          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5787          5.4369          4.3406          4.3632
v  Pressure                -36.434          360.01          87.654          169.84
v  r11                   0.0010598        0.081975        0.013069        0.018284
v  r22                   0.0011105        0.082641        0.013349        0.018644
v  r33                   0.0016347         0.17434         0.02724        0.037201
v  r12                   -0.010664        0.013581     -0.00023372     -0.00030926
v  r13                   -0.045555        0.052801      9.2718e-05       0.0010135
v  r23                   -0.046716        0.051238      3.0033e-05      0.00057436
v  epsilon                0.068585          271.31          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9713e-05        0.009918       0.0009243       0.0017424
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2787          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71348         0.85283


 TIME FOR THE TIME STEP            10043:        0.77546E+02

===============================================================


 INSTANT    0.100440000E-01   TIME STEP NUMBER           10044
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.219941153E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.243298114E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186425405E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.433099034E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199143252E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81285E-03   0.45178E-02 0.19910E+01 
c  Velocity[X]                                      0.13887E-03 
c  Velocity[Y]                                      0.12934E-03 
c  Velocity[Z]                                      0.42496E-02 
c  Pressure     0.36200E-04     131   0.92139E-02   0.25536E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.61532E-08   0.16486E-08 0.99795E-01 
c  r22          0.10850E-01      13   0.56569E-08   0.18252E-08 0.10147E+00 
c  r33          0.21856E-01      15   0.67245E-08   0.12599E-07 0.12758E+00 
c  r12          0.93841E-03      18   0.62085E-08   0.29508E-09 0.60479E+00 
c  r13          0.46668E-02      20   0.57959E-08   0.14810E-08 0.19950E+00 
c  r23          0.39968E-02      20   0.54819E-08   0.12829E-08 0.19912E+00 
c  epsilon      0.10971E+02      11   0.35450E-08   0.10286E-01 0.16869E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.85032E-02 0.43453E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61352       0.0052539       0.0015073
v  Velocity[Y]             -0.5734         0.54425       0.0030782      0.00087305
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.471          360.06          87.679          169.88
v  r11                   0.0010598        0.081975        0.013069        0.018284
v  r22                   0.0011105        0.082642        0.013349        0.018644
v  r33                   0.0016347         0.17438         0.02724        0.037201
v  r12                   -0.010657        0.013585     -0.00023372     -0.00030926
v  r13                   -0.045553        0.052803      9.2719e-05       0.0010135
v  r23                   -0.046717        0.051227      3.0035e-05      0.00057436
v  epsilon                0.068585          271.32          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9711e-05       0.0099179       0.0009243       0.0017424
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2789          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71348         0.85282


 TIME FOR THE TIME STEP            10044:        0.81148E+02

===============================================================


 INSTANT    0.100450000E-01   TIME STEP NUMBER           10045
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154877645E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.356383932E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155012191E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.212370168E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.738871507E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      44   0.81206E-03   0.45351E-02 0.19936E+01 
c  Velocity[X]                                      0.13862E-03 
c  Velocity[Y]                                      0.12980E-03 
c  Velocity[Z]                                      0.42667E-02 
c  Pressure     0.36555E-04     132   0.93073E-02   0.25786E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60657E-08   0.16099E-08 0.99089E-01 
c  r22          0.10850E-01      13   0.60566E-08   0.17951E-08 0.10098E+00 
c  r33          0.21856E-01      15   0.61952E-08   0.12358E-07 0.12678E+00 
c  r12          0.93841E-03      18   0.66659E-08   0.29353E-09 0.60124E+00 
c  r13          0.46668E-02      19   0.75729E-08   0.14932E-08 0.19932E+00 
c  r23          0.39968E-02      19   0.72856E-08   0.12784E-08 0.19812E+00 
c  epsilon      0.10971E+02      11   0.34812E-08   0.97337E-02 0.16333E+00 
c  TempC        0.25716E+06      16   0.15093E-04   0.83692E-02 0.43160E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384          0.6135       0.0052539       0.0015073
v  Velocity[Y]            -0.57359          0.5444       0.0030783      0.00087308
v  Velocity[Z]               1.565          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4369          4.3406          4.3632
v  Pressure                -36.395          360.03          87.637          169.85
v  r11                   0.0010598        0.081967        0.013069        0.018284
v  r22                   0.0011105        0.082639        0.013349        0.018644
v  r33                   0.0016348         0.17435         0.02724        0.037201
v  r12                   -0.010652        0.013585     -0.00023372     -0.00030926
v  r13                   -0.045558        0.052805      9.2719e-05       0.0010135
v  r23                   -0.046718        0.051231      3.0035e-05      0.00057436
v  epsilon                0.068585          271.33          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.971e-05       0.0099179       0.0009243       0.0017424
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2784          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71348         0.85283


 TIME FOR THE TIME STEP            10045:        0.80124E+02

===============================================================


 INSTANT    0.100460000E-01   TIME STEP NUMBER           10046
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.663138789E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190298616E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.200225712E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.151015267E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.215645782E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81159E-03   0.45444E-02 0.19987E+01 
c  Velocity[X]                                      0.13905E-03 
c  Velocity[Y]                                      0.13043E-03 
c  Velocity[Z]                                      0.42749E-02 
c  Pressure     0.36507E-04     131   0.92969E-02   0.25752E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50619E-08   0.16334E-08 0.10016E+00 
c  r22          0.10850E-01      13   0.54428E-08   0.17842E-08 0.10136E+00 
c  r33          0.21856E-01      15   0.57809E-08   0.12380E-07 0.12787E+00 
c  r12          0.93841E-03      18   0.57716E-08   0.29680E-09 0.60971E+00 
c  r13          0.46668E-02      19   0.65172E-08   0.14552E-08 0.19952E+00 
c  r23          0.39968E-02      19   0.71702E-08   0.12884E-08 0.20106E+00 
c  epsilon      0.10971E+02      11   0.32433E-08   0.97614E-02 0.16824E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83980E-02 0.43261E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61348       0.0052539       0.0015073
v  Velocity[Y]            -0.57348         0.54408       0.0030783      0.00087309
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.452          360.01          87.671          169.85
v  r11                   0.0010598         0.08196        0.013069        0.018284
v  r22                   0.0011105         0.08264        0.013349        0.018644
v  r33                   0.0016348         0.17433         0.02724        0.037201
v  r12                   -0.010655        0.013582     -0.00023372     -0.00030926
v  r13                   -0.045555        0.052804      9.2721e-05       0.0010135
v  r23                   -0.046718        0.051226      3.0036e-05      0.00057436
v  epsilon                0.068585          271.27          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.971e-05        0.009918       0.0009243       0.0017424
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2783          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71348         0.85283


 TIME FOR THE TIME STEP            10046:        0.79503E+02

===============================================================


 INSTANT    0.100470000E-01   TIME STEP NUMBER           10047
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.194488864E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.241645983E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.540517743E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.633980156E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.114270121E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81132E-03   0.45270E-02 0.19959E+01 
c  Velocity[X]                                      0.13949E-03 
c  Velocity[Y]                                      0.12927E-03 
c  Velocity[Z]                                      0.42582E-02 
c  Pressure     0.36390E-04     133   0.92583E-02   0.25670E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55446E-08   0.16092E-08 0.99307E-01 
c  r22          0.10850E-01      13   0.54023E-08   0.18234E-08 0.10144E+00 
c  r33          0.21856E-01      15   0.71085E-08   0.12363E-07 0.12704E+00 
c  r12          0.93841E-03      18   0.59126E-08   0.28810E-09 0.60229E+00 
c  r13          0.46668E-02      19   0.73193E-08   0.14812E-08 0.19968E+00 
c  r23          0.39968E-02      19   0.68972E-08   0.12478E-08 0.19792E+00 
c  epsilon      0.10971E+02      11   0.32826E-08   0.98155E-02 0.16419E+00 
c  TempC        0.25716E+06      16   0.15101E-04   0.84701E-02 0.43421E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63368          0.6135       0.0052539       0.0015073
v  Velocity[Y]            -0.57363         0.54413       0.0030783      0.00087311
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.443           360.1          87.709          169.92
v  r11                   0.0010598        0.081958        0.013069        0.018284
v  r22                   0.0011105        0.082642        0.013349        0.018644
v  r33                   0.0016348         0.17434         0.02724        0.037201
v  r12                   -0.010657        0.013578     -0.00023372     -0.00030926
v  r13                   -0.045554        0.052802      9.2721e-05       0.0010135
v  r23                   -0.046718        0.051253      3.0037e-05      0.00057436
v  epsilon                0.068585          271.29          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9712e-05       0.0099181       0.0009243       0.0017424
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2782          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71348         0.85282


 TIME FOR THE TIME STEP            10047:        0.80150E+02

===============================================================


 INSTANT    0.100480000E-01   TIME STEP NUMBER           10048
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160949633E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.223020188E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.532448013E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.161109692E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.897454772E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21889E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81353E-03   0.45419E-02 0.19945E+01 
c  Velocity[X]                                      0.13887E-03 
c  Velocity[Y]                                      0.12866E-03 
c  Velocity[Z]                                      0.42744E-02 
c  Pressure     0.36658E-04     133   0.93307E-02   0.25860E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59296E-08   0.16539E-08 0.10012E+00 
c  r22          0.10850E-01      13   0.53821E-08   0.17902E-08 0.10110E+00 
c  r33          0.21856E-01      15   0.59897E-08   0.12484E-07 0.12762E+00 
c  r12          0.93841E-03      18   0.58673E-08   0.29185E-09 0.60226E+00 
c  r13          0.46668E-02      19   0.53730E-08   0.14801E-08 0.19962E+00 
c  r23          0.39968E-02      19   0.65153E-08   0.13040E-08 0.20035E+00 
c  epsilon      0.10971E+02      11   0.32612E-08   0.98864E-02 0.16491E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.83991E-02 0.43304E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61348       0.0052539       0.0015073
v  Velocity[Y]            -0.57361         0.54426       0.0030783      0.00087313
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.438             360          87.633          169.83
v  r11                   0.0010598         0.08196        0.013069        0.018284
v  r22                   0.0011105        0.082642        0.013349        0.018644
v  r33                   0.0016348         0.17437         0.02724        0.037201
v  r12                   -0.010663        0.013582     -0.00023372     -0.00030926
v  r13                   -0.045557        0.052803      9.2722e-05       0.0010135
v  r23                   -0.046718        0.051244      3.0038e-05      0.00057436
v  epsilon                0.068585          271.31          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.971e-05       0.0099181       0.0009243       0.0017424
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2779          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71348         0.85282


 TIME FOR THE TIME STEP            10048:        0.77610E+02

===============================================================


 INSTANT    0.100490000E-01   TIME STEP NUMBER           10049
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.676764778E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.131017517E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.760457167E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.450396876E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.274184186E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81163E-03   0.45498E-02 0.19988E+01 
c  Velocity[X]                                      0.13928E-03 
c  Velocity[Y]                                      0.13060E-03 
c  Velocity[Z]                                      0.42800E-02 
c  Pressure     0.36591E-04     132   0.93213E-02   0.25812E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57323E-08   0.16293E-08 0.99593E-01 
c  r22          0.10850E-01      13   0.55383E-08   0.18229E-08 0.10192E+00 
c  r33          0.21856E-01      14   0.71360E-08   0.12505E-07 0.12792E+00 
c  r12          0.93841E-03      18   0.64690E-08   0.29804E-09 0.60712E+00 
c  r13          0.46668E-02      18   0.73296E-08   0.14969E-08 0.20060E+00 
c  r23          0.39968E-02      19   0.53878E-08   0.12779E-08 0.19879E+00 
c  epsilon      0.10971E+02      11   0.31432E-08   0.99311E-02 0.16503E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.84848E-02 0.43425E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61347       0.0052539       0.0015073
v  Velocity[Y]            -0.57355         0.54442       0.0030784      0.00087314
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.403          360.05          87.661          169.87
v  r11                   0.0010598        0.081958        0.013069        0.018284
v  r22                   0.0011105        0.082642        0.013349        0.018644
v  r33                   0.0016348         0.17436         0.02724        0.037201
v  r12                   -0.010663        0.013582     -0.00023372     -0.00030926
v  r13                   -0.045556        0.052802      9.2723e-05       0.0010135
v  r23                   -0.046718        0.051228      3.0039e-05      0.00057436
v  epsilon                0.068585          271.32          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9711e-05       0.0099181       0.0009243       0.0017424
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85282


 TIME FOR THE TIME STEP            10049:        0.79721E+02

===============================================================


 INSTANT    0.100500000E-01   TIME STEP NUMBER           10050
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.228991317E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.165840910E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.379724187E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.259505074E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.188246990E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40363E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81186E-03   0.45631E-02 0.19999E+01 
c  Velocity[X]                                      0.14040E-03 
c  Velocity[Y]                                      0.13050E-03 
c  Velocity[Z]                                      0.42922E-02 
c  Pressure     0.36055E-04     131   0.91851E-02   0.25433E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.56083E-08   0.16415E-08 0.99944E-01 
c  r22          0.10850E-01      13   0.53366E-08   0.18420E-08 0.10198E+00 
c  r33          0.21856E-01      15   0.55682E-08   0.12673E-07 0.12824E+00 
c  r12          0.93841E-03      18   0.61181E-08   0.29728E-09 0.60554E+00 
c  r13          0.46668E-02      18   0.71575E-08   0.15162E-08 0.20120E+00 
c  r23          0.39968E-02      19   0.54599E-08   0.12883E-08 0.19947E+00 
c  epsilon      0.10971E+02      11   0.32914E-08   0.10264E-01 0.16726E+00 
c  TempC        0.25716E+06      16   0.15124E-04   0.84609E-02 0.43336E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61351       0.0052539       0.0015073
v  Velocity[Y]            -0.57352         0.54411       0.0030783      0.00087309
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.404          360.06          87.688          169.88
v  r11                   0.0010598        0.081955        0.013069        0.018284
v  r22                   0.0011106        0.082641        0.013349        0.018644
v  r33                   0.0016348         0.17434         0.02724        0.037201
v  r12                   -0.010663        0.013579     -0.00023372     -0.00030926
v  r13                   -0.045554        0.052801      9.2725e-05       0.0010135
v  r23                   -0.046718        0.051239      3.0041e-05      0.00057437
v  epsilon                0.068585          271.28          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9709e-05       0.0099181      0.00092431       0.0017424
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017903           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85283


 TIME FOR THE TIME STEP            10050:        0.79339E+02

===============================================================


 INSTANT    0.100510000E-01   TIME STEP NUMBER           10051
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.278124884E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221856105E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.313424156E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.829117848E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.167350129E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81146E-03   0.45301E-02 0.19941E+01 
c  Velocity[X]                                      0.13877E-03 
c  Velocity[Y]                                      0.12905E-03 
c  Velocity[Z]                                      0.42623E-02 
c  Pressure     0.36257E-04     132   0.92305E-02   0.25576E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55424E-08   0.16127E-08 0.99907E-01 
c  r22          0.10850E-01      13   0.50271E-08   0.17733E-08 0.10096E+00 
c  r33          0.21856E-01      15   0.57765E-08   0.12187E-07 0.12720E+00 
c  r12          0.93841E-03      18   0.55237E-08   0.29004E-09 0.60468E+00 
c  r13          0.46668E-02      18   0.69808E-08   0.14774E-08 0.20014E+00 
c  r23          0.39968E-02      19   0.59270E-08   0.12570E-08 0.19859E+00 
c  epsilon      0.10971E+02      11   0.32244E-08   0.92821E-02 0.16021E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.84299E-02 0.43328E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61352       0.0052539       0.0015072
v  Velocity[Y]            -0.57366         0.54413       0.0030784      0.00087311
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.406          360.06          87.683          169.89
v  r11                   0.0010598        0.081952        0.013069        0.018284
v  r22                   0.0011106        0.082636        0.013349        0.018644
v  r33                   0.0016348         0.17435         0.02724        0.037201
v  r12                   -0.010661        0.013574     -0.00023372     -0.00030926
v  r13                   -0.045557        0.052801      9.2726e-05       0.0010135
v  r23                   -0.046718        0.051231      3.0041e-05      0.00057436
v  epsilon                0.068585          271.32          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9711e-05        0.009918      0.00092431       0.0017424
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2772          0.1144         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71349         0.85283


 TIME FOR THE TIME STEP            10051:        0.80467E+02

===============================================================


 INSTANT    0.100520000E-01   TIME STEP NUMBER           10052
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201362864E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.167387821E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.178177172E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.180461910E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319377323E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      44   0.81194E-03   0.45394E-02 0.19943E+01 
c  Velocity[X]                                      0.13953E-03 
c  Velocity[Y]                                      0.12965E-03 
c  Velocity[Z]                                      0.42702E-02 
c  Pressure     0.36282E-04     131   0.92374E-02   0.25593E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.58716E-08   0.16076E-08 0.99205E-01 
c  r22          0.10850E-01      13   0.48518E-08   0.18043E-08 0.10083E+00 
c  r33          0.21856E-01      15   0.54509E-08   0.12301E-07 0.12649E+00 
c  r12          0.93841E-03      18   0.51015E-08   0.29365E-09 0.60459E+00 
c  r13          0.46668E-02      18   0.66749E-08   0.14879E-08 0.19903E+00 
c  r23          0.39968E-02      19   0.53369E-08   0.12695E-08 0.19852E+00 
c  epsilon      0.10971E+02      11   0.32812E-08   0.97440E-02 0.16454E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.83863E-02 0.43254E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61347       0.0052539       0.0015072
v  Velocity[Y]            -0.57353         0.54428       0.0030784      0.00087309
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.438          360.05          87.683          169.88
v  r11                   0.0010598         0.08195        0.013069        0.018284
v  r22                   0.0011106        0.082639        0.013349        0.018644
v  r33                   0.0016348         0.17438         0.02724        0.037201
v  r12                   -0.010659        0.013578     -0.00023372     -0.00030926
v  r13                   -0.045554        0.052805      9.2727e-05       0.0010135
v  r23                   -0.046717        0.051225      3.0042e-05      0.00057437
v  epsilon                0.068585          271.34          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9713e-05       0.0099178      0.00092431       0.0017424
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017903           5.277          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71348         0.85283


 TIME FOR THE TIME STEP            10052:        0.79363E+02

===============================================================


 INSTANT    0.100530000E-01   TIME STEP NUMBER           10053
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.337407190E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.233361072E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229819658E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.412667815E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.969116440E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      44   0.81208E-03   0.45411E-02 0.19939E+01 
c  Velocity[X]                                      0.13926E-03 
c  Velocity[Y]                                      0.13014E-03 
c  Velocity[Z]                                      0.42717E-02 
c  Pressure     0.36531E-04     131   0.93039E-02   0.25769E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54982E-08   0.16704E-08 0.10119E+00 
c  r22          0.10850E-01      13   0.49054E-08   0.17752E-08 0.10082E+00 
c  r33          0.21856E-01      15   0.55489E-08   0.12462E-07 0.12814E+00 
c  r12          0.93841E-03      18   0.50923E-08   0.29698E-09 0.60875E+00 
c  r13          0.46668E-02      18   0.61496E-08   0.14705E-08 0.19959E+00 
c  r23          0.39968E-02      19   0.51214E-08   0.13314E-08 0.20387E+00 
c  epsilon      0.10971E+02      11   0.33255E-08   0.99626E-02 0.16996E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.84497E-02 0.43394E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61349       0.0052538       0.0015072
v  Velocity[Y]            -0.57369         0.54406       0.0030784      0.00087311
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                 -36.41          360.05          87.676          169.89
v  r11                   0.0010598        0.081945        0.013069        0.018284
v  r22                   0.0011106        0.082642        0.013349        0.018644
v  r33                   0.0016349         0.17437         0.02724        0.037201
v  r12                    -0.01066        0.013584     -0.00023372     -0.00030926
v  r13                   -0.045555        0.052804      9.2728e-05       0.0010135
v  r23                   -0.046716        0.051242      3.0043e-05      0.00057437
v  epsilon                0.068585          271.36          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9713e-05       0.0099179      0.00092431       0.0017424
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2772          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71348         0.85282


 TIME FOR THE TIME STEP            10053:        0.80660E+02

===============================================================


 INSTANT    0.100540000E-01   TIME STEP NUMBER           10054
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.265146965E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.650226028E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138196092E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.698346785E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.772071463E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81242E-03   0.45336E-02 0.19939E+01 
c  Velocity[X]                                      0.13870E-03 
c  Velocity[Y]                                      0.12932E-03 
c  Velocity[Z]                                      0.42656E-02 
c  Pressure     0.36399E-04     133   0.92698E-02   0.25676E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.49497E-08   0.16130E-08 0.99508E-01 
c  r22          0.10850E-01      13   0.51205E-08   0.17807E-08 0.10073E+00 
c  r33          0.21856E-01      15   0.56201E-08   0.12229E-07 0.12683E+00 
c  r12          0.93842E-03      18   0.54526E-08   0.29480E-09 0.60374E+00 
c  r13          0.46668E-02      18   0.69831E-08   0.14394E-08 0.19762E+00 
c  r23          0.39968E-02      19   0.51951E-08   0.12625E-08 0.19859E+00 
c  epsilon      0.10971E+02      11   0.33625E-08   0.94729E-02 0.16277E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.84287E-02 0.43241E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338         0.61347       0.0052539       0.0015072
v  Velocity[Y]            -0.57352         0.54417       0.0030783      0.00087309
v  Velocity[Z]              1.5651          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4369          4.3406          4.3632
v  Pressure                -36.441          360.02           87.68          169.87
v  r11                   0.0010599        0.081946        0.013069        0.018284
v  r22                   0.0011106        0.082644        0.013349        0.018644
v  r33                   0.0016349         0.17434         0.02724        0.037201
v  r12                   -0.010669        0.013586     -0.00023373     -0.00030927
v  r13                   -0.045557        0.052804      9.2729e-05       0.0010135
v  r23                   -0.046715        0.051228      3.0043e-05      0.00057437
v  epsilon                0.068585          271.33          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9712e-05        0.009918      0.00092431       0.0017424
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017903           5.277          0.1144         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71348         0.85283


 TIME FOR THE TIME STEP            10054:        0.77659E+02

===============================================================


 INSTANT    0.100550000E-01   TIME STEP NUMBER           10055
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136572435E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.325731656E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.365450442E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285244104E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.448474611E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81190E-03   0.45508E-02 0.19990E+01 
c  Velocity[X]                                      0.13963E-03 
c  Velocity[Y]                                      0.12962E-03 
c  Velocity[Z]                                      0.42816E-02 
c  Pressure     0.36147E-04     131   0.92096E-02   0.25498E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.51773E-08   0.15990E-08 0.99272E-01 
c  r22          0.10850E-01      13   0.52026E-08   0.17994E-08 0.10080E+00 
c  r33          0.21856E-01      15   0.55178E-08   0.12338E-07 0.12667E+00 
c  r12          0.93842E-03      18   0.60577E-08   0.29758E-09 0.60486E+00 
c  r13          0.46668E-02      18   0.65778E-08   0.14922E-08 0.19957E+00 
c  r23          0.39968E-02      18   0.68293E-08   0.12675E-08 0.19790E+00 
c  epsilon      0.10971E+02      11   0.34243E-08   0.96959E-02 0.16260E+00 
c  TempC        0.25716E+06      16   0.15096E-04   0.84475E-02 0.43345E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61347       0.0052539       0.0015072
v  Velocity[Y]            -0.57365         0.54435       0.0030785      0.00087314
v  Velocity[Z]               1.565          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4369          4.3406          4.3632
v  Pressure                -36.387          360.03          87.671          169.88
v  r11                   0.0010599        0.081939        0.013069        0.018284
v  r22                   0.0011106        0.082645        0.013349        0.018644
v  r33                   0.0016349         0.17435         0.02724        0.037201
v  r12                   -0.010668         0.01359     -0.00023372     -0.00030926
v  r13                   -0.045554        0.052803      9.2731e-05       0.0010135
v  r23                   -0.046714        0.051219      3.0045e-05      0.00057437
v  epsilon                0.068586          271.33          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9715e-05       0.0099179      0.00092431       0.0017424
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85283


 TIME FOR THE TIME STEP            10055:        0.80457E+02

===============================================================


 INSTANT    0.100560000E-01   TIME STEP NUMBER           10056
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.381641110E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.607627472E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.396600608E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.192967941E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.214161210E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81183E-03   0.45490E-02 0.19969E+01 
c  Velocity[X]                                      0.13926E-03 
c  Velocity[Y]                                      0.12995E-03 
c  Velocity[Z]                                      0.42797E-02 
c  Pressure     0.36953E-04     133   0.94020E-02   0.26066E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.51249E-08   0.16572E-08 0.10046E+00 
c  r22          0.10850E-01      13   0.48925E-08   0.17993E-08 0.10095E+00 
c  r33          0.21856E-01      15   0.54561E-08   0.12560E-07 0.12780E+00 
c  r12          0.93842E-03      18   0.55939E-08   0.30129E-09 0.60735E+00 
c  r13          0.46668E-02      18   0.67102E-08   0.15129E-08 0.20059E+00 
c  r23          0.39968E-02      19   0.55870E-08   0.12963E-08 0.20052E+00 
c  epsilon      0.10971E+02      11   0.33616E-08   0.99081E-02 0.16505E+00 
c  TempC        0.25716E+06      16   0.15167E-04   0.84407E-02 0.43359E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61345       0.0052539       0.0015072
v  Velocity[Y]            -0.57364         0.54407       0.0030784      0.00087309
v  Velocity[Z]               1.565          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4369          4.3406          4.3632
v  Pressure                -36.452          360.06          87.686          169.89
v  r11                   0.0010599        0.081931        0.013069        0.018284
v  r22                   0.0011106        0.082645        0.013349        0.018644
v  r33                   0.0016349         0.17439         0.02724        0.037201
v  r12                   -0.010663         0.01359     -0.00023373     -0.00030927
v  r13                   -0.045553        0.052802      9.2732e-05       0.0010135
v  r23                   -0.046712        0.051201      3.0046e-05      0.00057437
v  epsilon                0.068586          271.33          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9715e-05       0.0099178      0.00092431       0.0017424
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2775          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71348         0.85282


 TIME FOR THE TIME STEP            10056:        0.80219E+02

===============================================================


 INSTANT    0.100570000E-01   TIME STEP NUMBER           10057
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.192886402E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.855433274E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.251582419E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191936174E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.129167455E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81249E-03   0.45485E-02 0.19971E+01 
c  Velocity[X]                                      0.13868E-03 
c  Velocity[Y]                                      0.12963E-03 
c  Velocity[Z]                                      0.42802E-02 
c  Pressure     0.36431E-04     133   0.92738E-02   0.25698E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52124E-08   0.16775E-08 0.10092E+00 
c  r22          0.10850E-01      13   0.50101E-08   0.18119E-08 0.10123E+00 
c  r33          0.21856E-01      15   0.57999E-08   0.12598E-07 0.12800E+00 
c  r12          0.93842E-03      18   0.60877E-08   0.30087E-09 0.60828E+00 
c  r13          0.46668E-02      18   0.70876E-08   0.14786E-08 0.19900E+00 
c  r23          0.39968E-02      19   0.55828E-08   0.13203E-08 0.20205E+00 
c  epsilon      0.10971E+02      11   0.32218E-08   0.97264E-02 0.16477E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.84065E-02 0.43264E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338         0.61347       0.0052539       0.0015072
v  Velocity[Y]            -0.57365         0.54407       0.0030784      0.00087311
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.395          360.08          87.682           169.9
v  r11                   0.0010599        0.081925        0.013069        0.018284
v  r22                   0.0011106        0.082644        0.013349        0.018644
v  r33                   0.0016349         0.17436         0.02724        0.037201
v  r12                   -0.010659        0.013587     -0.00023373     -0.00030927
v  r13                   -0.045557        0.052803      9.2734e-05       0.0010135
v  r23                   -0.046712        0.051219      3.0048e-05      0.00057437
v  epsilon                0.068586          271.35          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9717e-05       0.0099178      0.00092432       0.0017424
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2773          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71348         0.85282


 TIME FOR THE TIME STEP            10057:        0.78509E+02

===============================================================


 INSTANT    0.100580000E-01   TIME STEP NUMBER           10058
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.185321066E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209679953E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283211776E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.893961114E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.180931570E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81174E-03   0.45606E-02 0.20015E+01 
c  Velocity[X]                                      0.13905E-03 
c  Velocity[Y]                                      0.12960E-03 
c  Velocity[Z]                                      0.42919E-02 
c  Pressure     0.36799E-04     134   0.93668E-02   0.25959E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52050E-08   0.16737E-08 0.10114E+00 
c  r22          0.10850E-01      13   0.53144E-08   0.18292E-08 0.10191E+00 
c  r33          0.21856E-01      15   0.62929E-08   0.12644E-07 0.12860E+00 
c  r12          0.93842E-03      18   0.57599E-08   0.30226E-09 0.60840E+00 
c  r13          0.46668E-02      19   0.54391E-08   0.14961E-08 0.20023E+00 
c  r23          0.39968E-02      19   0.63155E-08   0.13112E-08 0.20196E+00 
c  epsilon      0.10971E+02      11   0.34871E-08   0.96014E-02 0.16350E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.84668E-02 0.43423E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61345       0.0052539       0.0015072
v  Velocity[Y]            -0.57364         0.54421       0.0030784       0.0008731
v  Velocity[Z]              1.5652          5.4369          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4369          4.3406          4.3632
v  Pressure                -36.464          360.02          87.672          169.86
v  r11                   0.0010599        0.081919        0.013069        0.018284
v  r22                   0.0011106         0.08264        0.013349        0.018644
v  r33                   0.0016349         0.17434         0.02724        0.037201
v  r12                   -0.010659        0.013585     -0.00023373     -0.00030926
v  r13                   -0.045554        0.052806      9.2736e-05       0.0010135
v  r23                   -0.046711        0.051211      3.0049e-05      0.00057437
v  epsilon                0.068586          271.31          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9718e-05       0.0099178      0.00092432       0.0017424
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017903           5.277          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71348         0.85283


 TIME FOR THE TIME STEP            10058:        0.78767E+02

===============================================================


 INSTANT    0.100590000E-01   TIME STEP NUMBER           10059
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.175627474E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153585363E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.219164208E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.186975378E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.250277104E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81180E-03   0.45460E-02 0.19987E+01 
c  Velocity[X]                                      0.13958E-03 
c  Velocity[Y]                                      0.13029E-03 
c  Velocity[Z]                                      0.42761E-02 
c  Pressure     0.36321E-04     134   0.92471E-02   0.25622E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.56717E-08   0.16456E-08 0.99972E-01 
c  r22          0.10850E-01      13   0.52778E-08   0.17935E-08 0.10078E+00 
c  r33          0.21856E-01      15   0.56413E-08   0.12491E-07 0.12736E+00 
c  r12          0.93842E-03      18   0.57704E-08   0.29884E-09 0.60703E+00 
c  r13          0.46668E-02      19   0.55688E-08   0.14778E-08 0.19896E+00 
c  r23          0.39968E-02      19   0.63582E-08   0.12959E-08 0.20035E+00 
c  epsilon      0.10971E+02      11   0.35031E-08   0.99842E-02 0.16851E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.84622E-02 0.43344E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61345       0.0052539       0.0015072
v  Velocity[Y]            -0.57358         0.54426       0.0030784      0.00087315
v  Velocity[Z]              1.5652           5.437          4.3388          4.3625
v  ǁVelocityǁ                1.579           5.437          4.3406          4.3632
v  Pressure                -36.422          360.05          87.673          169.88
v  r11                   0.0010599        0.081917        0.013069        0.018284
v  r22                   0.0011106        0.082641        0.013349        0.018644
v  r33                   0.0016349         0.17436         0.02724        0.037201
v  r12                   -0.010659        0.013587     -0.00023373     -0.00030926
v  r13                   -0.045554        0.052805      9.2736e-05       0.0010135
v  r23                    -0.04671        0.051197      3.0049e-05      0.00057437
v  epsilon                0.068586          271.32          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9723e-05       0.0099179      0.00092432       0.0017424
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2773          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71348         0.85283


 TIME FOR THE TIME STEP            10059:        0.79299E+02

===============================================================


 INSTANT    0.100600000E-01   TIME STEP NUMBER           10060
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.334227332E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.990921122E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.442491785E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.131714243E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.726309078E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81231E-03   0.45276E-02 0.19919E+01 
c  Velocity[X]                                      0.13859E-03 
c  Velocity[Y]                                      0.12926E-03 
c  Velocity[Z]                                      0.42598E-02 
c  Pressure     0.36298E-04     131   0.92370E-02   0.25605E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55623E-08   0.16224E-08 0.99731E-01 
c  r22          0.10850E-01      13   0.53093E-08   0.18079E-08 0.10124E+00 
c  r33          0.21856E-01      15   0.59082E-08   0.12394E-07 0.12722E+00 
c  r12          0.93842E-03      18   0.64132E-08   0.29558E-09 0.60249E+00 
c  r13          0.46668E-02      18   0.68919E-08   0.14657E-08 0.19845E+00 
c  r23          0.39968E-02      19   0.71106E-08   0.12648E-08 0.19862E+00 
c  epsilon      0.10971E+02      11   0.34448E-08   0.97310E-02 0.16363E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.83368E-02 0.43099E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61348       0.0052539       0.0015073
v  Velocity[Y]            -0.57358         0.54406       0.0030784      0.00087312
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.448           360.1          87.684           169.9
v  r11                   0.0010599        0.081911        0.013069        0.018284
v  r22                   0.0011107        0.082641        0.013349        0.018644
v  r33                   0.0016349         0.17437         0.02724        0.037201
v  r12                   -0.010662        0.013587     -0.00023373     -0.00030927
v  r13                   -0.045557        0.052801      9.2737e-05       0.0010135
v  r23                    -0.04671        0.051227      3.0051e-05      0.00057437
v  epsilon                0.068586          271.32          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9726e-05        0.009918      0.00092432       0.0017424
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2771          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71348         0.85282


 TIME FOR THE TIME STEP            10060:        0.74354E+02

===============================================================


 INSTANT    0.100610000E-01   TIME STEP NUMBER           10061
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.508419708E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.741261457E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.164537780E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.195345948E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.782520186E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81167E-03   0.45557E-02 0.19965E+01 
c  Velocity[X]                                      0.13933E-03 
c  Velocity[Y]                                      0.12933E-03 
c  Velocity[Z]                                      0.42870E-02 
c  Pressure     0.36694E-04     133   0.93408E-02   0.25885E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.49500E-08   0.16332E-08 0.99985E-01 
c  r22          0.10850E-01      13   0.56450E-08   0.18184E-08 0.10146E+00 
c  r33          0.21856E-01      15   0.73078E-08   0.12493E-07 0.12747E+00 
c  r12          0.93842E-03      18   0.66254E-08   0.30000E-09 0.60390E+00 
c  r13          0.46668E-02      19   0.59162E-08   0.15020E-08 0.20009E+00 
c  r23          0.39968E-02      20   0.58774E-08   0.12905E-08 0.19983E+00 
c  epsilon      0.10971E+02      11   0.35357E-08   0.97995E-02 0.16304E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.84675E-02 0.43427E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369         0.61346        0.005254       0.0015073
v  Velocity[Y]            -0.57355         0.54416       0.0030784      0.00087312
v  Velocity[Z]              1.5654          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4369          4.3406          4.3632
v  Pressure                -36.435          360.02          87.661          169.86
v  r11                   0.0010599        0.081911        0.013069        0.018284
v  r22                   0.0011107         0.08264        0.013349        0.018644
v  r33                   0.0016349         0.17435         0.02724        0.037201
v  r12                   -0.010661        0.013588     -0.00023373     -0.00030926
v  r13                   -0.045556        0.052799      9.2739e-05       0.0010135
v  r23                    -0.04671         0.05122      3.0052e-05      0.00057437
v  epsilon                0.068586          271.32          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.973e-05        0.009918      0.00092432       0.0017424
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85283


 TIME FOR THE TIME STEP            10061:        0.78405E+02

===============================================================


 INSTANT    0.100620000E-01   TIME STEP NUMBER           10062
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.147380844E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.128862150E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.139843011E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.132040118E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.288367058E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81216E-03   0.45551E-02 0.19993E+01 
c  Velocity[X]                                      0.13924E-03 
c  Velocity[Y]                                      0.12946E-03 
c  Velocity[Z]                                      0.42864E-02 
c  Pressure     0.36626E-04     133   0.93244E-02   0.25837E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50834E-08   0.16208E-08 0.99728E-01 
c  r22          0.10850E-01      13   0.51383E-08   0.18204E-08 0.10158E+00 
c  r33          0.21856E-01      15   0.55540E-08   0.12414E-07 0.12731E+00 
c  r12          0.93842E-03      18   0.63348E-08   0.29526E-09 0.60144E+00 
c  r13          0.46668E-02      19   0.56570E-08   0.14953E-08 0.19985E+00 
c  r23          0.39968E-02      19   0.70016E-08   0.12627E-08 0.19812E+00 
c  epsilon      0.10971E+02      11   0.33987E-08   0.97886E-02 0.16489E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.84850E-02 0.43456E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61347        0.005254       0.0015073
v  Velocity[Y]            -0.57353         0.54386       0.0030784      0.00087309
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.436          359.99          87.649          169.83
v  r11                   0.0010599        0.081914        0.013069        0.018284
v  r22                   0.0011107        0.082641        0.013349        0.018644
v  r33                    0.001635         0.17433         0.02724        0.037201
v  r12                   -0.010658        0.013587     -0.00023373     -0.00030926
v  r13                   -0.045554        0.052801       9.274e-05       0.0010135
v  r23                   -0.046709        0.051208      3.0053e-05      0.00057437
v  epsilon                0.068586          271.26          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9731e-05       0.0099179      0.00092432       0.0017424
v  CourantNb               0.44266             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2779          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71348         0.85282


 TIME FOR THE TIME STEP            10062:        0.79894E+02

===============================================================


 INSTANT    0.100630000E-01   TIME STEP NUMBER           10063
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.878964049E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.238019827E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188711712E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.804462259E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.119913326E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81216E-03   0.45363E-02 0.19959E+01 
c  Velocity[X]                                      0.13883E-03 
c  Velocity[Y]                                      0.12981E-03 
c  Velocity[Z]                                      0.42677E-02 
c  Pressure     0.36363E-04     133   0.92603E-02   0.25650E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.51531E-08   0.16329E-08 0.10034E+00 
c  r22          0.10850E-01      13   0.54044E-08   0.18001E-08 0.10098E+00 
c  r33          0.21856E-01      15   0.61232E-08   0.12423E-07 0.12724E+00 
c  r12          0.93842E-03      18   0.66382E-08   0.29326E-09 0.60291E+00 
c  r13          0.46668E-02      19   0.72728E-08   0.14794E-08 0.19877E+00 
c  r23          0.39968E-02      19   0.68431E-08   0.12724E-08 0.19896E+00 
c  epsilon      0.10971E+02      11   0.33348E-08   0.10002E-01 0.16627E+00 
c  TempC        0.25716E+06      16   0.15082E-04   0.84312E-02 0.43334E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338          0.6135        0.005254       0.0015073
v  Velocity[Y]            -0.57353         0.54388       0.0030785      0.00087312
v  Velocity[Z]              1.5653           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5791           5.437          4.3406          4.3632
v  Pressure                -36.392          360.04          87.661          169.87
v  r11                   0.0010599        0.081916        0.013069        0.018284
v  r22                   0.0011107        0.082642        0.013349        0.018644
v  r33                    0.001635         0.17434         0.02724        0.037201
v  r12                   -0.010656        0.013584     -0.00023373     -0.00030926
v  r13                   -0.045557        0.052799      9.2741e-05       0.0010135
v  r23                    -0.04671        0.051197      3.0054e-05      0.00057437
v  epsilon                0.068586          271.28          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9735e-05       0.0099177      0.00092432       0.0017424
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017903           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85282


 TIME FOR THE TIME STEP            10063:        0.78732E+02

===============================================================


 INSTANT    0.100640000E-01   TIME STEP NUMBER           10064
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.238155610E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.236458207E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.147977491E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.247124550E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.276690661E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81216E-03   0.45547E-02 0.19986E+01 
c  Velocity[X]                                      0.13969E-03 
c  Velocity[Y]                                      0.12959E-03 
c  Velocity[Z]                                      0.42854E-02 
c  Pressure     0.36345E-04     131   0.92542E-02   0.25639E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.53964E-08   0.16317E-08 0.10008E+00 
c  r22          0.10850E-01      13   0.59658E-08   0.18204E-08 0.10115E+00 
c  r33          0.21856E-01      15   0.57399E-08   0.12435E-07 0.12706E+00 
c  r12          0.93842E-03      19   0.55231E-08   0.29380E-09 0.60267E+00 
c  r13          0.46668E-02      19   0.64991E-08   0.14770E-08 0.19917E+00 
c  r23          0.39968E-02      19   0.73319E-08   0.12467E-08 0.19828E+00 
c  epsilon      0.10971E+02      11   0.32790E-08   0.10074E-01 0.16712E+00 
c  TempC        0.25716E+06      16   0.15171E-04   0.84720E-02 0.43416E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61344        0.005254       0.0015073
v  Velocity[Y]            -0.57343         0.54403       0.0030785      0.00087312
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.437          360.05          87.674          169.88
v  r11                   0.0010599        0.081911        0.013069        0.018284
v  r22                   0.0011107         0.08264        0.013349        0.018644
v  r33                    0.001635         0.17437         0.02724        0.037201
v  r12                   -0.010657        0.013584     -0.00023373     -0.00030926
v  r13                   -0.045554        0.052799      9.2742e-05       0.0010135
v  r23                   -0.046711        0.051233      3.0054e-05      0.00057437
v  epsilon                0.068586          271.29          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9735e-05       0.0099177      0.00092433       0.0017424
v  CourantNb               0.44266             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2785          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71348         0.85283


 TIME FOR THE TIME STEP            10064:        0.79037E+02

===============================================================


 INSTANT    0.100650000E-01   TIME STEP NUMBER           10065
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141498910E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.750963431E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.817810816E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.197151769E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.156214312E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81047E-03   0.45566E-02 0.19993E+01 
c  Velocity[X]                                      0.13954E-03 
c  Velocity[Y]                                      0.13000E-03 
c  Velocity[Z]                                      0.42871E-02 
c  Pressure     0.36447E-04     132   0.92793E-02   0.25710E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54547E-08   0.16797E-08 0.10121E+00 
c  r22          0.10850E-01      13   0.61355E-08   0.18359E-08 0.10209E+00 
c  r33          0.21856E-01      15   0.57613E-08   0.12713E-07 0.12884E+00 
c  r12          0.93842E-03      19   0.57996E-08   0.30180E-09 0.60700E+00 
c  r13          0.46668E-02      19   0.66319E-08   0.14916E-08 0.20054E+00 
c  r23          0.39968E-02      19   0.72205E-08   0.13220E-08 0.20373E+00 
c  epsilon      0.10971E+02      11   0.34321E-08   0.10239E-01 0.17164E+00 
c  TempC        0.25716E+06      16   0.15110E-04   0.84265E-02 0.43299E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61347        0.005254       0.0015073
v  Velocity[Y]            -0.57352         0.54422       0.0030785      0.00087309
v  Velocity[Z]              1.5657           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5794           5.437          4.3406          4.3632
v  Pressure                -36.449          360.09           87.69          169.91
v  r11                   0.0010599        0.081909        0.013069        0.018284
v  r22                   0.0011107        0.082639        0.013349        0.018644
v  r33                    0.001635         0.17435         0.02724        0.037201
v  r12                   -0.010656        0.013587     -0.00023373     -0.00030926
v  r13                   -0.045556        0.052798      9.2744e-05       0.0010135
v  r23                   -0.046711        0.051233      3.0055e-05      0.00057437
v  epsilon                0.068587          271.31          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9735e-05       0.0099178      0.00092433       0.0017424
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2786          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71348         0.85282


 TIME FOR THE TIME STEP            10065:        0.81379E+02

===============================================================


 INSTANT    0.100660000E-01   TIME STEP NUMBER           10066
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.549846675E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.146737492E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.218590345E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.133849618E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.626573430E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81308E-03   0.45288E-02 0.19938E+01 
c  Velocity[X]                                      0.13885E-03 
c  Velocity[Y]                                      0.12974E-03 
c  Velocity[Z]                                      0.42602E-02 
c  Pressure     0.36585E-04     132   0.93092E-02   0.25807E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52277E-08   0.16510E-08 0.10055E+00 
c  r22          0.10850E-01      13   0.59344E-08   0.18239E-08 0.10187E+00 
c  r33          0.21856E-01      15   0.69299E-08   0.12567E-07 0.12791E+00 
c  r12          0.93842E-03      19   0.60643E-08   0.29689E-09 0.60498E+00 
c  r13          0.46668E-02      19   0.69758E-08   0.14858E-08 0.20033E+00 
c  r23          0.39968E-02      19   0.63470E-08   0.13035E-08 0.20091E+00 
c  epsilon      0.10971E+02      11   0.35522E-08   0.99460E-02 0.16614E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.83914E-02 0.43222E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61347        0.005254       0.0015073
v  Velocity[Y]            -0.57341         0.54388       0.0030785      0.00087309
v  Velocity[Z]              1.5655          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4369          4.3406          4.3632
v  Pressure                -36.446          360.05          87.692          169.89
v  r11                   0.0010599        0.081908        0.013069        0.018284
v  r22                   0.0011107         0.08264        0.013349        0.018644
v  r33                    0.001635         0.17432         0.02724        0.037202
v  r12                   -0.010658        0.013581     -0.00023373     -0.00030927
v  r13                   -0.045558        0.052799      9.2744e-05       0.0010135
v  r23                   -0.046712        0.051215      3.0055e-05      0.00057437
v  epsilon                0.068587          271.29          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9734e-05       0.0099177      0.00092433       0.0017424
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2786          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71348         0.85282


 TIME FOR THE TIME STEP            10066:        0.77952E+02

===============================================================


 INSTANT    0.100670000E-01   TIME STEP NUMBER           10067
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.271546818E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.781081907E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.126458171E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935032E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276968273E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.170659064E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935015E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81219E-03   0.45519E-02 0.19989E+01 
c  Velocity[X]                                      0.13911E-03 
c  Velocity[Y]                                      0.12980E-03 
c  Velocity[Z]                                      0.42830E-02 
c  Pressure     0.36575E-04     133   0.93160E-02   0.25800E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.48191E-08   0.16374E-08 0.10010E+00 
c  r22          0.10850E-01      13   0.53498E-08   0.18155E-08 0.10161E+00 
c  r33          0.21856E-01      15   0.57115E-08   0.12407E-07 0.12723E+00 
c  r12          0.93842E-03      18   0.71990E-08   0.29525E-09 0.60619E+00 
c  r13          0.46668E-02      19   0.57874E-08   0.14832E-08 0.19965E+00 
c  r23          0.39968E-02      19   0.59025E-08   0.12792E-08 0.19911E+00 
c  epsilon      0.10971E+02      11   0.34172E-08   0.96785E-02 0.16322E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.84364E-02 0.43322E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61349        0.005254       0.0015073
v  Velocity[Y]            -0.57348         0.54391       0.0030786      0.00087314
v  Velocity[Z]              1.5655           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5793           5.437          4.3406          4.3632
v  Pressure                -36.396          360.03          87.653          169.86
v  r11                   0.0010599        0.081911        0.013069        0.018284
v  r22                   0.0011107        0.082635        0.013349        0.018644
v  r33                    0.001635         0.17434         0.02724        0.037202
v  r12                   -0.010657        0.013577     -0.00023373     -0.00030926
v  r13                   -0.045556          0.0528      9.2745e-05       0.0010135
v  r23                   -0.046713        0.051237      3.0056e-05      0.00057437
v  epsilon                0.068587           271.3          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9736e-05       0.0099176      0.00092433       0.0017424
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2784          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71348         0.85283


 TIME FOR THE TIME STEP            10067:        0.81116E+02

===============================================================


 INSTANT    0.100680000E-01   TIME STEP NUMBER           10068
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.683972329E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.157086034E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.526241724E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.463735174E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232573032E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81211E-03   0.45299E-02 0.19939E+01 
c  Velocity[X]                                      0.13987E-03 
c  Velocity[Y]                                      0.12936E-03 
c  Velocity[Z]                                      0.42607E-02 
c  Pressure     0.36323E-04     131   0.92511E-02   0.25622E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50529E-08   0.15992E-08 0.99602E-01 
c  r22          0.10850E-01      13   0.52648E-08   0.18061E-08 0.10143E+00 
c  r33          0.21856E-01      15   0.62700E-08   0.12229E-07 0.12681E+00 
c  r12          0.93842E-03      19   0.54226E-08   0.30112E-09 0.60945E+00 
c  r13          0.46668E-02      19   0.66239E-08   0.14797E-08 0.19999E+00 
c  r23          0.39968E-02      19   0.67497E-08   0.12491E-08 0.19793E+00 
c  epsilon      0.10971E+02      11   0.33475E-08   0.94192E-02 0.16157E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.85018E-02 0.43461E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61349       0.0052541       0.0015073
v  Velocity[Y]            -0.57339         0.54409       0.0030785      0.00087311
v  Velocity[Z]              1.5656          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4369          4.3406          4.3632
v  Pressure                -36.485          359.99          87.622          169.82
v  r11                   0.0010599        0.081918        0.013069        0.018284
v  r22                   0.0011107        0.082636        0.013349        0.018644
v  r33                    0.001635         0.17436         0.02724        0.037202
v  r12                   -0.010654        0.013581     -0.00023373     -0.00030927
v  r13                   -0.045554          0.0528      9.2747e-05       0.0010135
v  r23                   -0.046714        0.051216      3.0058e-05      0.00057437
v  epsilon                0.068587          271.34          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9737e-05       0.0099175      0.00092433       0.0017424
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2781          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71349         0.85283


 TIME FOR THE TIME STEP            10068:        0.80878E+02

===============================================================


 INSTANT    0.100690000E-01   TIME STEP NUMBER           10069
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.191422540E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.506673863E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.514469755E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.987266884E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.315482675E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81236E-03   0.45160E-02 0.19897E+01 
c  Velocity[X]                                      0.13793E-03 
c  Velocity[Y]                                      0.12877E-03 
c  Velocity[Z]                                      0.42493E-02 
c  Pressure     0.36335E-04     132   0.92511E-02   0.25631E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55027E-08   0.16339E-08 0.10060E+00 
c  r22          0.10850E-01      13   0.53055E-08   0.17844E-08 0.10127E+00 
c  r33          0.21856E-01      15   0.57947E-08   0.12231E-07 0.12716E+00 
c  r12          0.93842E-03      18   0.71044E-08   0.29666E-09 0.60570E+00 
c  r13          0.46668E-02      19   0.61014E-08   0.14676E-08 0.19904E+00 
c  r23          0.39969E-02      19   0.57516E-08   0.12819E-08 0.20090E+00 
c  epsilon      0.10971E+02      11   0.32606E-08   0.92688E-02 0.16137E+00 
c  TempC        0.25716E+06      16   0.15122E-04   0.84084E-02 0.43306E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61349       0.0052541       0.0015073
v  Velocity[Y]            -0.57337         0.54391       0.0030786      0.00087316
v  Velocity[Z]              1.5656           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5794           5.437          4.3406          4.3632
v  Pressure                 -36.45          360.05          87.658          169.87
v  r11                   0.0010599        0.081915        0.013069        0.018284
v  r22                   0.0011107        0.082637        0.013349        0.018644
v  r33                    0.001635         0.17434         0.02724        0.037202
v  r12                   -0.010659        0.013585     -0.00023373     -0.00030927
v  r13                   -0.045558        0.052799      9.2747e-05       0.0010135
v  r23                   -0.046715        0.051205      3.0058e-05      0.00057437
v  epsilon                0.068587          271.36          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9738e-05       0.0099176      0.00092433       0.0017424
v  CourantNb               0.44256             0.6         0.59908         0.59839
v  FourierNb             0.0017903           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85283


 TIME FOR THE TIME STEP            10069:        0.80268E+02

===============================================================


 INSTANT    0.100700000E-01   TIME STEP NUMBER           10070
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.236014260E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.381261151E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.271035237E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.296405248E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.131261465E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81187E-03   0.45261E-02 0.19943E+01 
c  Velocity[X]                                      0.13933E-03 
c  Velocity[Y]                                      0.12954E-03 
c  Velocity[Z]                                      0.42572E-02 
c  Pressure     0.36060E-04     131   0.91772E-02   0.25436E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.51842E-08   0.16250E-08 0.99896E-01 
c  r22          0.10850E-01      13   0.54120E-08   0.18026E-08 0.10153E+00 
c  r33          0.21856E-01      15   0.55122E-08   0.12412E-07 0.12754E+00 
c  r12          0.93842E-03      19   0.53395E-08   0.29515E-09 0.60412E+00 
c  r13          0.46668E-02      19   0.62457E-08   0.14854E-08 0.20059E+00 
c  r23          0.39969E-02      19   0.58367E-08   0.12811E-08 0.20001E+00 
c  epsilon      0.10971E+02      11   0.33630E-08   0.97448E-02 0.16425E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.83624E-02 0.43135E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61348        0.005254       0.0015073
v  Velocity[Y]            -0.57338         0.54405       0.0030785      0.00087311
v  Velocity[Z]              1.5653          5.4369          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4369          4.3406          4.3632
v  Pressure                -36.467          359.99          87.644          169.83
v  r11                   0.0010599        0.081915        0.013069        0.018284
v  r22                   0.0011107        0.082638        0.013349        0.018644
v  r33                    0.001635         0.17432         0.02724        0.037202
v  r12                   -0.010655        0.013587     -0.00023373     -0.00030927
v  r13                   -0.045555          0.0528      9.2748e-05       0.0010135
v  r23                   -0.046715          0.0512      3.0058e-05      0.00057437
v  epsilon                0.068587          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9739e-05       0.0099177      0.00092433       0.0017424
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2784          0.1144         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71348         0.85283


 TIME FOR THE TIME STEP            10070:        0.80967E+02

===============================================================


 INSTANT    0.100710000E-01   TIME STEP NUMBER           10071
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227855116E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.138432356E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.291119736E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.397714506E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122984567E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81090E-03   0.45581E-02 0.20008E+01 
c  Velocity[X]                                      0.14023E-03 
c  Velocity[Y]                                      0.12942E-03 
c  Velocity[Z]                                      0.42885E-02 
c  Pressure     0.36771E-04     133   0.93564E-02   0.25938E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.51532E-08   0.16414E-08 0.10051E+00 
c  r22          0.10850E-01      13   0.53744E-08   0.17972E-08 0.10165E+00 
c  r33          0.21856E-01      15   0.62228E-08   0.12467E-07 0.12828E+00 
c  r12          0.93842E-03      18   0.68591E-08   0.29177E-09 0.60287E+00 
c  r13          0.46668E-02      19   0.68225E-08   0.14797E-08 0.20036E+00 
c  r23          0.39969E-02      19   0.60103E-08   0.12925E-08 0.20116E+00 
c  epsilon      0.10971E+02      11   0.34890E-08   0.99190E-02 0.16883E+00 
c  TempC        0.25716E+06      16   0.15085E-04   0.84889E-02 0.43460E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379          0.6135        0.005254       0.0015073
v  Velocity[Y]            -0.57349         0.54405       0.0030787      0.00087318
v  Velocity[Z]              1.5655           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5792           5.437          4.3406          4.3632
v  Pressure                -36.445          360.11          87.723          169.94
v  r11                   0.0010599        0.081916        0.013069        0.018284
v  r22                   0.0011107        0.082639        0.013349        0.018644
v  r33                    0.001635         0.17434         0.02724        0.037202
v  r12                   -0.010654        0.013586     -0.00023373     -0.00030927
v  r13                   -0.045554        0.052801      9.2748e-05       0.0010135
v  r23                   -0.046716        0.051227      3.0058e-05      0.00057437
v  epsilon                0.068587          271.33          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9738e-05       0.0099175      0.00092433       0.0017424
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017903           5.279          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71348         0.85282


 TIME FOR THE TIME STEP            10071:        0.77207E+02

===============================================================


 INSTANT    0.100720000E-01   TIME STEP NUMBER           10072
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.592109624E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.217773724E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162112824E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.246275197E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111492384E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81300E-03   0.45189E-02 0.19896E+01 
c  Velocity[X]                                      0.13818E-03 
c  Velocity[Y]                                      0.12954E-03 
c  Velocity[Z]                                      0.42512E-02 
c  Pressure     0.36646E-04     133   0.93317E-02   0.25850E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52124E-08   0.16140E-08 0.99748E-01 
c  r22          0.10850E-01      13   0.51454E-08   0.18265E-08 0.10198E+00 
c  r33          0.21856E-01      15   0.54758E-08   0.12367E-07 0.12730E+00 
c  r12          0.93842E-03      18   0.63573E-08   0.29579E-09 0.60570E+00 
c  r13          0.46668E-02      19   0.55655E-08   0.14972E-08 0.20051E+00 
c  r23          0.39969E-02      19   0.61592E-08   0.12592E-08 0.19835E+00 
c  epsilon      0.10971E+02      11   0.33843E-08   0.97619E-02 0.16487E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84183E-02 0.43300E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61351       0.0052541       0.0015074
v  Velocity[Y]            -0.57338         0.54409       0.0030786      0.00087315
v  Velocity[Z]              1.5655           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5793           5.437          4.3406          4.3632
v  Pressure                -36.472          360.03          87.649          169.86
v  r11                   0.0010599        0.081916        0.013069        0.018284
v  r22                   0.0011107         0.08264        0.013349        0.018644
v  r33                    0.001635         0.17436         0.02724        0.037202
v  r12                   -0.010653        0.013589     -0.00023373     -0.00030927
v  r13                   -0.045557        0.052803      9.2749e-05       0.0010135
v  r23                   -0.046716        0.051219      3.0059e-05      0.00057437
v  epsilon                0.068588          271.36          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9738e-05       0.0099175      0.00092434       0.0017424
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2791          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71348         0.85283


 TIME FOR THE TIME STEP            10072:        0.74799E+02

===============================================================


 INSTANT    0.100730000E-01   TIME STEP NUMBER           10073
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183184986E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.746933907E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.317259786E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935016E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.666235464E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.204648339E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81186E-03   0.45297E-02 0.19933E+01 
c  Velocity[X]                                      0.13952E-03 
c  Velocity[Y]                                      0.12956E-03 
c  Velocity[Z]                                      0.42607E-02 
c  Pressure     0.36320E-04     132   0.92475E-02   0.25619E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50744E-08   0.16181E-08 0.99349E-01 
c  r22          0.10850E-01      13   0.51753E-08   0.17888E-08 0.10089E+00 
c  r33          0.21856E-01      15   0.58543E-08   0.12295E-07 0.12657E+00 
c  r12          0.93842E-03      18   0.59692E-08   0.29921E-09 0.60709E+00 
c  r13          0.46668E-02      19   0.58854E-08   0.14899E-08 0.19990E+00 
c  r23          0.39969E-02      19   0.66911E-08   0.12744E-08 0.19841E+00 
c  epsilon      0.10971E+02      11   0.34314E-08   0.96746E-02 0.16261E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.84405E-02 0.43361E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61348       0.0052542       0.0015074
v  Velocity[Y]            -0.57349         0.54419       0.0030787      0.00087317
v  Velocity[Z]              1.5656           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5793           5.437          4.3406          4.3632
v  Pressure                -36.445          359.99          87.614          169.82
v  r11                   0.0010599        0.081919        0.013069        0.018284
v  r22                   0.0011108        0.082637        0.013349        0.018644
v  r33                   0.0016351         0.17439         0.02724        0.037202
v  r12                   -0.010659        0.013594     -0.00023373     -0.00030926
v  r13                   -0.045556        0.052806      9.2751e-05       0.0010135
v  r23                   -0.046716        0.051206       3.006e-05      0.00057437
v  epsilon                0.068588          271.38          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9737e-05       0.0099174      0.00092434       0.0017424
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2782          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71348         0.85282


 TIME FOR THE TIME STEP            10073:        0.78458E+02

===============================================================


 INSTANT    0.100740000E-01   TIME STEP NUMBER           10074
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.417860830E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.856849863E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.115329073E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111996685E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.234296080E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81166E-03   0.45708E-02 0.20035E+01 
c  Velocity[X]                                      0.14006E-03 
c  Velocity[Y]                                      0.13007E-03 
c  Velocity[Z]                                      0.43006E-02 
c  Pressure     0.36431E-04     132   0.92853E-02   0.25698E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.48474E-08   0.16134E-08 0.10003E+00 
c  r22          0.10850E-01      13   0.50939E-08   0.17735E-08 0.10092E+00 
c  r33          0.21856E-01      15   0.62532E-08   0.12145E-07 0.12699E+00 
c  r12          0.93842E-03      18   0.59275E-08   0.29501E-09 0.60648E+00 
c  r13          0.46668E-02      19   0.61517E-08   0.14526E-08 0.19864E+00 
c  r23          0.39969E-02      19   0.68236E-08   0.12710E-08 0.19929E+00 
c  epsilon      0.10971E+02      11   0.33568E-08   0.92860E-02 0.16119E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84601E-02 0.43361E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61347       0.0052542       0.0015074
v  Velocity[Y]            -0.57345         0.54399       0.0030786      0.00087317
v  Velocity[Z]              1.5656           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5794           5.437          4.3406          4.3632
v  Pressure                -36.459             360          87.656          169.84
v  r11                   0.0010599        0.081918        0.013069        0.018284
v  r22                   0.0011108         0.08264        0.013349        0.018644
v  r33                   0.0016351         0.17437         0.02724        0.037202
v  r12                   -0.010663        0.013595     -0.00023373     -0.00030926
v  r13                   -0.045554        0.052809      9.2752e-05       0.0010135
v  r23                   -0.046716        0.051193       3.006e-05      0.00057437
v  epsilon                0.068588          271.36          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9734e-05       0.0099175      0.00092434       0.0017424
v  CourantNb               0.44258             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2776          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71348         0.85283


 TIME FOR THE TIME STEP            10074:        0.78179E+02

===============================================================


 INSTANT    0.100750000E-01   TIME STEP NUMBER           10075
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.864610929E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.196319298E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130254242E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935019E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182357351E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.113002213E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81191E-03   0.44993E-02 0.19874E+01 
c  Velocity[X]                                      0.13829E-03 
c  Velocity[Y]                                      0.12929E-03 
c  Velocity[Z]                                      0.42317E-02 
c  Pressure     0.36314E-04     131   0.92507E-02   0.25616E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50750E-08   0.16060E-08 0.99223E-01 
c  r22          0.10850E-01      13   0.50268E-08   0.18011E-08 0.10097E+00 
c  r33          0.21856E-01      15   0.51609E-08   0.12346E-07 0.12704E+00 
c  r12          0.93842E-03      18   0.54895E-08   0.29236E-09 0.59983E+00 
c  r13          0.46668E-02      19   0.56293E-08   0.14779E-08 0.19927E+00 
c  r23          0.39969E-02      19   0.60484E-08   0.12595E-08 0.19822E+00 
c  epsilon      0.10971E+02      11   0.33891E-08   0.98391E-02 0.16621E+00 
c  TempC        0.25716E+06      16   0.15093E-04   0.83887E-02 0.43196E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61352       0.0052542       0.0015074
v  Velocity[Y]             -0.5735         0.54406       0.0030787      0.00087318
v  Velocity[Z]              1.5657           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5795           5.437          4.3406          4.3632
v  Pressure                -36.425          360.03          87.642          169.85
v  r11                   0.0010599        0.081917        0.013069        0.018284
v  r22                   0.0011108        0.082645        0.013349        0.018644
v  r33                   0.0016351         0.17433         0.02724        0.037202
v  r12                   -0.010663        0.013595     -0.00023373     -0.00030927
v  r13                   -0.045556        0.052807      9.2752e-05       0.0010135
v  r23                   -0.046715         0.05123      3.0061e-05      0.00057437
v  epsilon                0.068588          271.33          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9731e-05       0.0099175      0.00092434       0.0017424
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85282


 TIME FOR THE TIME STEP            10075:        0.78046E+02

===============================================================


 INSTANT    0.100760000E-01   TIME STEP NUMBER           10076
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.543418848E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.500897479E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934898E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.958976366E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136708553E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151686091E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81231E-03   0.45685E-02 0.20033E+01 
c  Velocity[X]                                      0.13881E-03 
c  Velocity[Y]                                      0.12994E-03 
c  Velocity[Z]                                      0.42997E-02 
c  Pressure     0.36709E-04     133   0.93426E-02   0.25895E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.49656E-08   0.16330E-08 0.99646E-01 
c  r22          0.10850E-01      13   0.51274E-08   0.18402E-08 0.10180E+00 
c  r33          0.21856E-01      15   0.53314E-08   0.12559E-07 0.12750E+00 
c  r12          0.93843E-03      18   0.53462E-08   0.30932E-09 0.61071E+00 
c  r13          0.46668E-02      19   0.59060E-08   0.15207E-08 0.20067E+00 
c  r23          0.39969E-02      19   0.58538E-08   0.12924E-08 0.19954E+00 
c  epsilon      0.10971E+02      11   0.32128E-08   0.98730E-02 0.16364E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.84583E-02 0.43428E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61346       0.0052541       0.0015073
v  Velocity[Y]            -0.57351         0.54418       0.0030787      0.00087317
v  Velocity[Z]              1.5654           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5792           5.437          4.3406          4.3632
v  Pressure                -36.457          360.05          87.684          169.88
v  r11                   0.0010599         0.08192        0.013069        0.018284
v  r22                   0.0011108        0.082648        0.013349        0.018644
v  r33                   0.0016351         0.17435         0.02724        0.037202
v  r12                   -0.010659        0.013596     -0.00023373     -0.00030927
v  r13                   -0.045554        0.052808      9.2753e-05       0.0010135
v  r23                   -0.046715        0.051227      3.0062e-05      0.00057437
v  epsilon                0.068588          271.35          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9731e-05       0.0099177      0.00092434       0.0017424
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017902           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85282


 TIME FOR THE TIME STEP            10076:        0.81484E+02

===============================================================


 INSTANT    0.100770000E-01   TIME STEP NUMBER           10077
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.244449172E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.250533869E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169451025E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.295114054E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.872052131E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81196E-03   0.45389E-02 0.19948E+01 
c  Velocity[X]                                      0.13864E-03 
c  Velocity[Y]                                      0.12877E-03 
c  Velocity[Z]                                      0.42715E-02 
c  Pressure     0.36033E-04     133   0.91739E-02   0.25417E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54669E-08   0.16534E-08 0.10038E+00 
c  r22          0.10850E-01      13   0.52025E-08   0.18164E-08 0.10155E+00 
c  r33          0.21856E-01      15   0.56132E-08   0.12580E-07 0.12807E+00 
c  r12          0.93843E-03      18   0.59665E-08   0.29904E-09 0.60541E+00 
c  r13          0.46668E-02      19   0.62766E-08   0.14991E-08 0.20070E+00 
c  r23          0.39969E-02      19   0.57745E-08   0.13085E-08 0.20140E+00 
c  epsilon      0.10971E+02      11   0.32206E-08   0.10055E-01 0.16931E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.84453E-02 0.43396E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61347       0.0052541       0.0015073
v  Velocity[Y]            -0.57359         0.54404       0.0030787      0.00087317
v  Velocity[Z]              1.5654           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5792           5.437          4.3406          4.3632
v  Pressure                -36.445          360.11          87.689          169.92
v  r11                   0.0010599        0.081916        0.013069        0.018284
v  r22                   0.0011108        0.082652        0.013349        0.018644
v  r33                   0.0016351         0.17438         0.02724        0.037202
v  r12                    -0.01066        0.013596     -0.00023373     -0.00030926
v  r13                   -0.045556        0.052808      9.2754e-05       0.0010135
v  r23                   -0.046715        0.051216      3.0063e-05      0.00057437
v  epsilon                0.068589          271.38          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9731e-05       0.0099179      0.00092434       0.0017424
v  CourantNb               0.44259             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2782          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71348         0.85283


 TIME FOR THE TIME STEP            10077:        0.77369E+02

===============================================================


 INSTANT    0.100780000E-01   TIME STEP NUMBER           10078
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100882663E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.112862241E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.518480383E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.532763222E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.196137826E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81290E-03   0.45263E-02 0.19918E+01 
c  Velocity[X]                                      0.13903E-03 
c  Velocity[Y]                                      0.12997E-03 
c  Velocity[Z]                                      0.42573E-02 
c  Pressure     0.36678E-04     132   0.93427E-02   0.25872E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.53511E-08   0.16425E-08 0.99849E-01 
c  r22          0.10850E-01      13   0.52201E-08   0.18042E-08 0.10107E+00 
c  r33          0.21856E-01      15   0.58655E-08   0.12400E-07 0.12693E+00 
c  r12          0.93843E-03      18   0.51441E-08   0.29399E-09 0.60219E+00 
c  r13          0.46668E-02      19   0.63143E-08   0.14698E-08 0.19861E+00 
c  r23          0.39969E-02      19   0.66003E-08   0.12768E-08 0.19869E+00 
c  epsilon      0.10971E+02      11   0.31864E-08   0.96380E-02 0.16371E+00 
c  TempC        0.25716E+06      16   0.15114E-04   0.84002E-02 0.43190E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61352       0.0052541       0.0015074
v  Velocity[Y]            -0.57354         0.54406       0.0030787       0.0008732
v  Velocity[Z]              1.5652           5.437          4.3388          4.3625
v  ǁVelocityǁ                1.579           5.437          4.3406          4.3632
v  Pressure                -36.493          360.04          87.664          169.87
v  r11                   0.0010599        0.081916        0.013069        0.018284
v  r22                   0.0011108        0.082655        0.013349        0.018644
v  r33                   0.0016351         0.17434         0.02724        0.037202
v  r12                   -0.010661        0.013597     -0.00023373     -0.00030927
v  r13                   -0.045558        0.052811      9.2755e-05       0.0010135
v  r23                   -0.046715        0.051235      3.0064e-05      0.00057438
v  epsilon                0.068589          271.37          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9732e-05       0.0099179      0.00092434       0.0017424
v  CourantNb               0.44258             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2781          0.1144         0.25442
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71348         0.85282


 TIME FOR THE TIME STEP            10078:        0.80922E+02

===============================================================


 INSTANT    0.100790000E-01   TIME STEP NUMBER           10079
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.633161891E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.382079191E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319550301E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.437835680E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.473027726E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81222E-03   0.45511E-02 0.20002E+01 
c  Velocity[X]                                      0.13977E-03 
c  Velocity[Y]                                      0.12964E-03 
c  Velocity[Z]                                      0.42817E-02 
c  Pressure     0.36514E-04     134   0.92927E-02   0.25757E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.49962E-08   0.16301E-08 0.10003E+00 
c  r22          0.10850E-01      13   0.53415E-08   0.18421E-08 0.10188E+00 
c  r33          0.21856E-01      15   0.55635E-08   0.12532E-07 0.12756E+00 
c  r12          0.93843E-03      18   0.54039E-08   0.30835E-09 0.61200E+00 
c  r13          0.46668E-02      19   0.60594E-08   0.15145E-08 0.20087E+00 
c  r23          0.39969E-02      19   0.60666E-08   0.12763E-08 0.19908E+00 
c  epsilon      0.10971E+02      11   0.33565E-08   0.98128E-02 0.16423E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.85049E-02 0.43506E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61349       0.0052541       0.0015074
v  Velocity[Y]            -0.57355         0.54414       0.0030787      0.00087321
v  Velocity[Z]              1.5653           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5791           5.437          4.3406          4.3632
v  Pressure                -36.421          360.05          87.663          169.87
v  r11                   0.0010599        0.081917        0.013069        0.018284
v  r22                   0.0011108        0.082652        0.013349        0.018644
v  r33                   0.0016351         0.17432         0.02724        0.037202
v  r12                   -0.010661        0.013598     -0.00023373     -0.00030927
v  r13                   -0.045556        0.052813      9.2756e-05       0.0010135
v  r23                   -0.046715        0.051217      3.0065e-05      0.00057438
v  epsilon                0.068589          271.32          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9734e-05       0.0099178      0.00092434       0.0017424
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2778          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71348         0.85282


 TIME FOR THE TIME STEP            10079:        0.80326E+02

===============================================================


 INSTANT    0.100800000E-01   TIME STEP NUMBER           10080
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186371308E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110839800E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.113276481E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.197084890E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.871873219E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81258E-03   0.45605E-02 0.19997E+01 
c  Velocity[X]                                      0.13948E-03 
c  Velocity[Y]                                      0.12984E-03 
c  Velocity[Z]                                      0.42912E-02 
c  Pressure     0.36405E-04     133   0.92703E-02   0.25680E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.49487E-08   0.16522E-08 0.10038E+00 
c  r22          0.10850E-01      13   0.50210E-08   0.18065E-08 0.10158E+00 
c  r33          0.21856E-01      15   0.54117E-08   0.12497E-07 0.12767E+00 
c  r12          0.93843E-03      18   0.54327E-08   0.30237E-09 0.60659E+00 
c  r13          0.46668E-02      19   0.61760E-08   0.14734E-08 0.19930E+00 
c  r23          0.39969E-02      19   0.59434E-08   0.12929E-08 0.20049E+00 
c  epsilon      0.10971E+02      11   0.33507E-08   0.98474E-02 0.16608E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.83959E-02 0.43241E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339          0.6135       0.0052542       0.0015074
v  Velocity[Y]            -0.57349         0.54429       0.0030786      0.00087317
v  Velocity[Z]              1.5653           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5791           5.437          4.3406          4.3632
v  Pressure                -36.438          359.98          87.628          169.81
v  r11                   0.0010599        0.081914        0.013069        0.018284
v  r22                   0.0011108        0.082655        0.013349        0.018644
v  r33                   0.0016351         0.17433         0.02724        0.037202
v  r12                   -0.010663        0.013596     -0.00023373     -0.00030927
v  r13                   -0.045554        0.052816      9.2757e-05       0.0010135
v  r23                   -0.046715        0.051192      3.0066e-05      0.00057438
v  epsilon                0.068589          271.32          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9735e-05       0.0099178      0.00092435       0.0017424
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2783          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71348         0.85282


 TIME FOR THE TIME STEP            10080:        0.79207E+02

===============================================================


 INSTANT    0.100810000E-01   TIME STEP NUMBER           10081
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.506865498E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.193993914E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.970413335E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.193846697E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.949467794E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40362E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81125E-03   0.45263E-02 0.19933E+01 
c  Velocity[X]                                      0.13803E-03 
c  Velocity[Y]                                      0.13058E-03 
c  Velocity[Z]                                      0.42577E-02 
c  Pressure     0.35989E-04     133   0.91629E-02   0.25387E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52119E-08   0.16329E-08 0.99875E-01 
c  r22          0.10850E-01      13   0.49607E-08   0.18324E-08 0.10193E+00 
c  r33          0.21856E-01      15   0.59829E-08   0.12454E-07 0.12725E+00 
c  r12          0.93843E-03      18   0.55348E-08   0.29892E-09 0.60631E+00 
c  r13          0.46668E-02      20   0.62600E-08   0.14985E-08 0.20032E+00 
c  r23          0.39969E-02      19   0.68098E-08   0.12718E-08 0.19880E+00 
c  epsilon      0.10971E+02      11   0.33534E-08   0.99232E-02 0.16717E+00 
c  TempC        0.25716E+06      16   0.15107E-04   0.83697E-02 0.43209E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61353       0.0052543       0.0015074
v  Velocity[Y]             -0.5736         0.54414       0.0030787      0.00087321
v  Velocity[Z]              1.5653           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5791           5.437          4.3406          4.3632
v  Pressure                -36.442          360.02          87.632          169.84
v  r11                   0.0010599        0.081914        0.013069        0.018284
v  r22                   0.0011108        0.082657        0.013349        0.018644
v  r33                   0.0016351         0.17434         0.02724        0.037202
v  r12                   -0.010661        0.013601     -0.00023373     -0.00030927
v  r13                   -0.045558        0.052815      9.2759e-05       0.0010135
v  r23                   -0.046715        0.051217      3.0067e-05      0.00057438
v  epsilon                0.068589          271.36          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9738e-05       0.0099177      0.00092435       0.0017424
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2793          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8793         0.71348         0.85282


 TIME FOR THE TIME STEP            10081:        0.79175E+02

===============================================================


 INSTANT    0.100820000E-01   TIME STEP NUMBER           10082
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.193780931E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.292406178E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.322551859E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106125275E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.139936792E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81134E-03   0.45266E-02 0.19934E+01 
c  Velocity[X]                                      0.13852E-03 
c  Velocity[Y]                                      0.12934E-03 
c  Velocity[Z]                                      0.42587E-02 
c  Pressure     0.36554E-04     133   0.93152E-02   0.25785E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.56455E-08   0.16227E-08 0.99714E-01 
c  r22          0.10850E-01      13   0.48762E-08   0.17924E-08 0.10104E+00 
c  r33          0.21856E-01      14   0.70477E-08   0.12290E-07 0.12676E+00 
c  r12          0.93843E-03      18   0.56819E-08   0.29722E-09 0.60402E+00 
c  r13          0.46668E-02      18   0.70969E-08   0.14697E-08 0.19891E+00 
c  r23          0.39969E-02      19   0.63151E-08   0.12603E-08 0.19814E+00 
c  epsilon      0.10971E+02      11   0.31553E-08   0.94576E-02 0.16319E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.84602E-02 0.43377E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61348       0.0052542       0.0015074
v  Velocity[Y]            -0.57342         0.54409       0.0030787      0.00087319
v  Velocity[Z]              1.5654           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5792           5.437          4.3406          4.3632
v  Pressure                -36.462          359.98          87.635          169.82
v  r11                   0.0010599        0.081913        0.013069        0.018284
v  r22                   0.0011108        0.082658        0.013349        0.018644
v  r33                   0.0016351         0.17438         0.02724        0.037202
v  r12                   -0.010659        0.013596     -0.00023373     -0.00030927
v  r13                   -0.045556        0.052815       9.276e-05       0.0010135
v  r23                   -0.046714         0.05121      3.0068e-05      0.00057438
v  epsilon                0.068589          271.34          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9739e-05       0.0099176      0.00092435       0.0017424
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2787          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71348         0.85283


 TIME FOR THE TIME STEP            10082:        0.79392E+02

===============================================================


 INSTANT    0.100830000E-01   TIME STEP NUMBER           10083
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.198728575E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.937318709E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.360457487E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.386734146E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.124680006E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81241E-03   0.45312E-02 0.19933E+01 
c  Velocity[X]                                      0.13971E-03 
c  Velocity[Y]                                      0.12867E-03 
c  Velocity[Z]                                      0.42629E-02 
c  Pressure     0.36200E-04     133   0.92225E-02   0.25535E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59062E-08   0.16824E-08 0.10092E+00 
c  r22          0.10850E-01      13   0.48863E-08   0.18153E-08 0.10119E+00 
c  r33          0.21856E-01      15   0.54129E-08   0.12764E-07 0.12861E+00 
c  r12          0.93843E-03      18   0.59749E-08   0.30395E-09 0.60836E+00 
c  r13          0.46669E-02      19   0.57950E-08   0.15012E-08 0.20082E+00 
c  r23          0.39969E-02      19   0.62845E-08   0.13354E-08 0.20301E+00 
c  epsilon      0.10971E+02      11   0.31897E-08   0.10227E-01 0.17145E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.85126E-02 0.43502E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61352       0.0052542       0.0015074
v  Velocity[Y]            -0.57349         0.54418       0.0030787      0.00087323
v  Velocity[Z]              1.5653           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5791           5.437          4.3406          4.3632
v  Pressure                -36.413          360.04          87.651          169.86
v  r11                   0.0010599        0.081911        0.013069        0.018284
v  r22                   0.0011108        0.082658        0.013349        0.018644
v  r33                   0.0016351         0.17436         0.02724        0.037202
v  r12                   -0.010661        0.013592     -0.00023373     -0.00030927
v  r13                   -0.045555        0.052813      9.2761e-05       0.0010135
v  r23                   -0.046714        0.051197      3.0069e-05      0.00057438
v  epsilon                 0.06859          271.33          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9742e-05       0.0099179      0.00092435       0.0017424
v  CourantNb               0.44258             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2789          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71348         0.85283


 TIME FOR THE TIME STEP            10083:        0.79918E+02

===============================================================


 INSTANT    0.100840000E-01   TIME STEP NUMBER           10084
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.596336110E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.490940226E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934900E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178761743E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.211786008E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.918194789E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81248E-03   0.45374E-02 0.19929E+01 
c  Velocity[X]                                      0.13848E-03 
c  Velocity[Y]                                      0.12902E-03 
c  Velocity[Z]                                      0.42699E-02 
c  Pressure     0.36711E-04     133   0.93464E-02   0.25896E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60841E-08   0.16577E-08 0.10027E+00 
c  r22          0.10850E-01      13   0.53862E-08   0.18165E-08 0.10106E+00 
c  r33          0.21856E-01      15   0.61867E-08   0.12526E-07 0.12721E+00 
c  r12          0.93843E-03      18   0.68783E-08   0.29515E-09 0.60113E+00 
c  r13          0.46669E-02      19   0.60419E-08   0.14839E-08 0.19920E+00 
c  r23          0.39969E-02      19   0.66057E-08   0.12767E-08 0.19824E+00 
c  epsilon      0.10971E+02      11   0.33176E-08   0.99926E-02 0.16679E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.84670E-02 0.43448E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61354       0.0052542       0.0015074
v  Velocity[Y]            -0.57347         0.54433       0.0030787      0.00087322
v  Velocity[Z]              1.5652           5.437          4.3388          4.3625
v  ǁVelocityǁ                1.579           5.437          4.3406          4.3632
v  Pressure                -36.484          360.07          87.673          169.89
v  r11                   0.0010599        0.081912        0.013069        0.018284
v  r22                   0.0011108        0.082657        0.013349        0.018644
v  r33                   0.0016351         0.17433         0.02724        0.037202
v  r12                   -0.010661        0.013584     -0.00023373     -0.00030927
v  r13                   -0.045558        0.052814      9.2762e-05       0.0010135
v  r23                   -0.046714        0.051224       3.007e-05      0.00057438
v  epsilon                 0.06859          271.31          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9746e-05       0.0099181      0.00092435       0.0017424
v  CourantNb               0.44265             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2793          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8793         0.71348         0.85283


 TIME FOR THE TIME STEP            10084:        0.79885E+02

===============================================================


 INSTANT    0.100850000E-01   TIME STEP NUMBER           10085
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.261014518E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.146040248E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.149903106E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935012E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.154990721E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.290473999E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69804E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81077E-03   0.45724E-02 0.20019E+01 
c  Velocity[X]                                      0.13908E-03 
c  Velocity[Y]                                      0.12908E-03 
c  Velocity[Z]                                      0.43043E-02 
c  Pressure     0.36206E-04     131   0.92227E-02   0.25539E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.66540E-08   0.16201E-08 0.98875E-01 
c  r22          0.10850E-01      13   0.51305E-08   0.18213E-08 0.10120E+00 
c  r33          0.21856E-01      15   0.53147E-08   0.12532E-07 0.12713E+00 
c  r12          0.93843E-03      18   0.68031E-08   0.30182E-09 0.60585E+00 
c  r13          0.46669E-02      19   0.60281E-08   0.14929E-08 0.19977E+00 
c  r23          0.39969E-02      19   0.69703E-08   0.12823E-08 0.19792E+00 
c  epsilon      0.10971E+02      11   0.34479E-08   0.10031E-01 0.16596E+00 
c  TempC        0.25716E+06      16   0.15100E-04   0.83980E-02 0.43232E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393          0.6135       0.0052542       0.0015074
v  Velocity[Y]             -0.5735         0.54412       0.0030788      0.00087328
v  Velocity[Z]              1.5654           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5792           5.437          4.3406          4.3632
v  Pressure                -36.436          360.02          87.632          169.84
v  r11                   0.0010599        0.081913        0.013069        0.018284
v  r22                   0.0011108        0.082655        0.013349        0.018644
v  r33                   0.0016351         0.17435         0.02724        0.037202
v  r12                   -0.010663        0.013592     -0.00023373     -0.00030927
v  r13                   -0.045557        0.052811      9.2762e-05       0.0010135
v  r23                   -0.046714        0.051213      3.0071e-05      0.00057438
v  epsilon                 0.06859          271.31          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9749e-05       0.0099182      0.00092435       0.0017424
v  CourantNb               0.44263             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2793          0.1144         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8793         0.71349         0.85283


 TIME FOR THE TIME STEP            10085:        0.79241E+02

===============================================================


 INSTANT    0.100860000E-01   TIME STEP NUMBER           10086
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.352295522E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.288134203E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.265623397E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.236571233E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.202041618E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81315E-03   0.45162E-02 0.19914E+01 
c  Velocity[X]                                      0.13937E-03 
c  Velocity[Y]                                      0.12992E-03 
c  Velocity[Z]                                      0.42469E-02 
c  Pressure     0.36510E-04     133   0.92963E-02   0.25753E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.68004E-08   0.16406E-08 0.99454E-01 
c  r22          0.10850E-01      13   0.54557E-08   0.18395E-08 0.10116E+00 
c  r33          0.21856E-01      16   0.61132E-08   0.12610E-07 0.12702E+00 
c  r12          0.93843E-03      18   0.70084E-08   0.29759E-09 0.60357E+00 
c  r13          0.46669E-02      20   0.72376E-08   0.15181E-08 0.19961E+00 
c  r23          0.39969E-02      19   0.64689E-08   0.12812E-08 0.19870E+00 
c  epsilon      0.10971E+02      11   0.35731E-08   0.10293E-01 0.16902E+00 
c  TempC        0.25716E+06      16   0.15120E-04   0.84160E-02 0.43256E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61351       0.0052543       0.0015074
v  Velocity[Y]            -0.57345         0.54425       0.0030787      0.00087321
v  Velocity[Z]              1.5655           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5793           5.437          4.3406          4.3632
v  Pressure                 -36.46          360.01          87.653          169.84
v  r11                   0.0010599        0.081913        0.013069        0.018284
v  r22                   0.0011108        0.082651        0.013349        0.018644
v  r33                   0.0016351         0.17437         0.02724        0.037202
v  r12                   -0.010665        0.013587     -0.00023373     -0.00030927
v  r13                   -0.045555        0.052812      9.2764e-05       0.0010135
v  r23                   -0.046714        0.051198      3.0072e-05      0.00057438
v  epsilon                 0.06859          271.33          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9755e-05       0.0099178      0.00092435       0.0017424
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2786          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71348         0.85282


 TIME FOR THE TIME STEP            10086:        0.80662E+02

===============================================================


 INSTANT    0.100870000E-01   TIME STEP NUMBER           10087
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.367380565E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.210224990E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.255123363E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209067206E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107689519E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69803E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      45   0.81259E-03   0.45276E-02 0.19932E+01 
c  Velocity[X]                                      0.13808E-03 
c  Velocity[Y]                                      0.12957E-03 
c  Velocity[Z]                                      0.42599E-02 
c  Pressure     0.36409E-04     133   0.92648E-02   0.25683E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.67436E-08   0.16423E-08 0.99752E-01 
c  r22          0.10850E-01      13   0.59140E-08   0.18222E-08 0.10104E+00 
c  r33          0.21856E-01      16   0.63063E-08   0.12443E-07 0.12685E+00 
c  r12          0.93843E-03      19   0.57460E-08   0.30138E-09 0.60700E+00 
c  r13          0.46669E-02      20   0.71629E-08   0.14899E-08 0.19854E+00 
c  r23          0.39969E-02      19   0.58575E-08   0.12916E-08 0.19936E+00 
c  epsilon      0.10971E+02      11   0.36271E-08   0.96940E-02 0.16544E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.84339E-02 0.43337E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61355       0.0052543       0.0015074
v  Velocity[Y]            -0.57358         0.54442       0.0030788      0.00087326
v  Velocity[Z]              1.5655           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5793           5.437          4.3406          4.3632
v  Pressure                -36.412          360.09          87.691          169.91
v  r11                   0.0010599         0.08191        0.013069        0.018284
v  r22                   0.0011108        0.082651        0.013349        0.018644
v  r33                   0.0016351         0.17434         0.02724        0.037202
v  r12                   -0.010664        0.013587     -0.00023373     -0.00030927
v  r13                   -0.045558         0.05281      9.2765e-05       0.0010135
v  r23                   -0.046714        0.051187      3.0073e-05      0.00057438
v  epsilon                 0.06859          271.35          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9761e-05       0.0099177      0.00092436       0.0017424
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2784          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71348         0.85282


 TIME FOR THE TIME STEP            10087:        0.80308E+02

===============================================================


 INSTANT    0.100880000E-01   TIME STEP NUMBER           10088
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116285837E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.711199587E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127292227E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.628693080E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.101878103E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81186E-03   0.45615E-02 0.19965E+01 
c  Velocity[X]                                      0.13855E-03 
c  Velocity[Y]                                      0.12906E-03 
c  Velocity[Z]                                      0.42939E-02 
c  Pressure     0.37072E-04     132   0.94388E-02   0.26150E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.63131E-08   0.16477E-08 0.99833E-01 
c  r22          0.10850E-01      13   0.58086E-08   0.18387E-08 0.10144E+00 
c  r33          0.21856E-01      15   0.69097E-08   0.12605E-07 0.12763E+00 
c  r12          0.93843E-03      19   0.55266E-08   0.30238E-09 0.60498E+00 
c  r13          0.46669E-02      20   0.62112E-08   0.15037E-08 0.19956E+00 
c  r23          0.39969E-02      19   0.63600E-08   0.12839E-08 0.19925E+00 
c  epsilon      0.10971E+02      11   0.34939E-08   0.98109E-02 0.16572E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.84599E-02 0.43402E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63395          0.6135       0.0052543       0.0015074
v  Velocity[Y]            -0.57347         0.54424       0.0030787      0.00087324
v  Velocity[Z]              1.5655           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5793           5.437          4.3406          4.3632
v  Pressure                -36.454          359.99          87.636          169.83
v  r11                   0.0010599        0.081905        0.013069        0.018284
v  r22                   0.0011109        0.082651        0.013349        0.018644
v  r33                   0.0016351         0.17431        0.027241        0.037202
v  r12                    -0.01067        0.013585     -0.00023373     -0.00030927
v  r13                   -0.045556        0.052809      9.2766e-05       0.0010135
v  r23                   -0.046714        0.051223      3.0073e-05      0.00057438
v  epsilon                0.068591          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9763e-05       0.0099178      0.00092436       0.0017424
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2785         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71349         0.85283


 TIME FOR THE TIME STEP            10088:        0.80121E+02

===============================================================


 INSTANT    0.100890000E-01   TIME STEP NUMBER           10089
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.213965281E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.274930710E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129407214E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.121264005E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.690008417E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81149E-03   0.45545E-02 0.19989E+01 
c  Velocity[X]                                      0.13921E-03 
c  Velocity[Y]                                      0.12885E-03 
c  Velocity[Z]                                      0.42864E-02 
c  Pressure     0.36354E-04     133   0.92497E-02   0.25645E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.64681E-08   0.16855E-08 0.10076E+00 
c  r22          0.10850E-01      13   0.63607E-08   0.18247E-08 0.10163E+00 
c  r33          0.21856E-01      15   0.60331E-08   0.12707E-07 0.12874E+00 
c  r12          0.93843E-03      19   0.57680E-08   0.30081E-09 0.60481E+00 
c  r13          0.46669E-02      20   0.59820E-08   0.14963E-08 0.20040E+00 
c  r23          0.39969E-02      19   0.65040E-08   0.13170E-08 0.20222E+00 
c  epsilon      0.10971E+02      11   0.33254E-08   0.10246E-01 0.17124E+00 
c  TempC        0.25716E+06      16   0.15122E-04   0.84432E-02 0.43359E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61353       0.0052542       0.0015074
v  Velocity[Y]            -0.57361         0.54418       0.0030788      0.00087329
v  Velocity[Z]              1.5652           5.437          4.3388          4.3625
v  ǁVelocityǁ                1.579           5.437          4.3406          4.3632
v  Pressure                -36.436          360.04          87.658          169.87
v  r11                   0.0010599        0.081901        0.013069        0.018284
v  r22                   0.0011109        0.082651        0.013349        0.018644
v  r33                   0.0016351         0.17432        0.027241        0.037202
v  r12                   -0.010668        0.013594     -0.00023373     -0.00030927
v  r13                   -0.045557        0.052809      9.2767e-05       0.0010135
v  r23                   -0.046714        0.051225      3.0074e-05      0.00057438
v  epsilon                0.068591           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9764e-05       0.0099176      0.00092436       0.0017424
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2779          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71348         0.85283


 TIME FOR THE TIME STEP            10089:        0.82242E+02

===============================================================


 INSTANT    0.100900000E-01   TIME STEP NUMBER           10090
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161886161E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.297435931E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.236013101E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200464109E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.142491479E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      44   0.81317E-03   0.45293E-02 0.19935E+01 
c  Velocity[X]                                      0.13867E-03 
c  Velocity[Y]                                      0.12994E-03 
c  Velocity[Z]                                      0.42607E-02 
c  Pressure     0.36640E-04     133   0.93354E-02   0.25846E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.69704E-08   0.16463E-08 0.99485E-01 
c  r22          0.10850E-01      13   0.63684E-08   0.18282E-08 0.10159E+00 
c  r33          0.21856E-01      15   0.65727E-08   0.12598E-07 0.12742E+00 
c  r12          0.93843E-03      18   0.70100E-08   0.29783E-09 0.60142E+00 
c  r13          0.46669E-02      20   0.56643E-08   0.14967E-08 0.19958E+00 
c  r23          0.39969E-02      19   0.63059E-08   0.12921E-08 0.19886E+00 
c  epsilon      0.10971E+02      11   0.32554E-08   0.10102E-01 0.16608E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.83529E-02 0.43116E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61354       0.0052543       0.0015074
v  Velocity[Y]            -0.57359         0.54424       0.0030788      0.00087327
v  Velocity[Z]              1.5654           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5792           5.437          4.3406          4.3632
v  Pressure                -36.491             360          87.643          169.84
v  r11                   0.0010599        0.081898        0.013069        0.018284
v  r22                   0.0011109        0.082651        0.013349        0.018644
v  r33                   0.0016351         0.17434        0.027241        0.037202
v  r12                   -0.010666        0.013594     -0.00023373     -0.00030927
v  r13                   -0.045559        0.052809      9.2767e-05       0.0010135
v  r23                   -0.046714        0.051215      3.0074e-05      0.00057438
v  epsilon                0.068591          271.32          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9767e-05       0.0099173      0.00092436       0.0017424
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85283


 TIME FOR THE TIME STEP            10090:        0.81150E+02

===============================================================


 INSTANT    0.100910000E-01   TIME STEP NUMBER           10091
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153915587E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.433214131E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.598598597E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227195727E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.197911552E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81204E-03   0.45565E-02 0.19984E+01 
c  Velocity[X]                                      0.13903E-03 
c  Velocity[Y]                                      0.12985E-03 
c  Velocity[Z]                                      0.42876E-02 
c  Pressure     0.36446E-04     131   0.92778E-02   0.25709E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.68884E-08   0.16151E-08 0.99058E-01 
c  r22          0.10850E-01      13   0.62110E-08   0.18031E-08 0.10084E+00 
c  r33          0.21856E-01      15   0.67824E-08   0.12372E-07 0.12665E+00 
c  r12          0.93843E-03      18   0.69975E-08   0.29427E-09 0.60072E+00 
c  r13          0.46669E-02      19   0.66393E-08   0.14926E-08 0.19915E+00 
c  r23          0.39969E-02      20   0.56949E-08   0.12720E-08 0.19823E+00 
c  epsilon      0.10971E+02      11   0.32973E-08   0.95827E-02 0.16198E+00 
c  TempC        0.25716E+06      16   0.15120E-04   0.84447E-02 0.43361E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61352       0.0052543       0.0015074
v  Velocity[Y]            -0.57362         0.54434       0.0030788      0.00087328
v  Velocity[Z]              1.5651           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5789           5.437          4.3406          4.3632
v  Pressure                -36.429          360.02          87.654          169.85
v  r11                   0.0010599        0.081899        0.013069        0.018284
v  r22                   0.0011109         0.08265        0.013349        0.018644
v  r33                   0.0016351         0.17433        0.027241        0.037202
v  r12                   -0.010661        0.013593     -0.00023373     -0.00030927
v  r13                   -0.045557        0.052807      9.2769e-05       0.0010135
v  r23                   -0.046713         0.05124      3.0075e-05      0.00057438
v  epsilon                0.068591          271.33          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9769e-05       0.0099175      0.00092436       0.0017424
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2776          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71348         0.85283


 TIME FOR THE TIME STEP            10091:        0.83334E+02

===============================================================


 INSTANT    0.100920000E-01   TIME STEP NUMBER           10092
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.265840462E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.544063497E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.734655887E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157656343E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166985382E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81226E-03   0.45546E-02 0.19969E+01 
c  Velocity[X]                                      0.13885E-03 
c  Velocity[Y]                                      0.12934E-03 
c  Velocity[Z]                                      0.42864E-02 
c  Pressure     0.36364E-04     131   0.92552E-02   0.25651E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.62878E-08   0.16336E-08 0.99829E-01 
c  r22          0.10850E-01      13   0.57160E-08   0.18147E-08 0.10116E+00 
c  r33          0.21856E-01      15   0.69136E-08   0.12417E-07 0.12700E+00 
c  r12          0.93843E-03      18   0.68894E-08   0.29453E-09 0.60273E+00 
c  r13          0.46669E-02      19   0.61916E-08   0.14981E-08 0.19969E+00 
c  r23          0.39969E-02      19   0.61600E-08   0.12678E-08 0.19826E+00 
c  epsilon      0.10971E+02      11   0.33929E-08   0.98107E-02 0.16481E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.85016E-02 0.43498E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61353       0.0052543       0.0015074
v  Velocity[Y]            -0.57354         0.54414       0.0030788      0.00087327
v  Velocity[Z]              1.5652           5.437          4.3388          4.3625
v  ǁVelocityǁ                1.579           5.437          4.3406          4.3632
v  Pressure                -36.448          360.06           87.68          169.89
v  r11                   0.0010599        0.081914        0.013069        0.018284
v  r22                   0.0011109         0.08265        0.013349        0.018644
v  r33                   0.0016351         0.17431        0.027241        0.037202
v  r12                   -0.010663        0.013595     -0.00023373     -0.00030927
v  r13                   -0.045556        0.052809      9.2769e-05       0.0010135
v  r23                   -0.046712        0.051229      3.0077e-05      0.00057438
v  epsilon                0.068592          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.977e-05       0.0099177      0.00092436       0.0017424
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85282


 TIME FOR THE TIME STEP            10092:        0.80454E+02

===============================================================


 INSTANT    0.100930000E-01   TIME STEP NUMBER           10093
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239905114E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.282372066E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.500749975E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.117149106E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.635443156E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81211E-03   0.44980E-02 0.19869E+01 
c  Velocity[X]                                      0.13779E-03 
c  Velocity[Y]                                      0.12827E-03 
c  Velocity[Z]                                      0.42319E-02 
c  Pressure     0.36219E-04     132   0.92132E-02   0.25549E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.62976E-08   0.16341E-08 0.99748E-01 
c  r22          0.10850E-01      13   0.55624E-08   0.18239E-08 0.10125E+00 
c  r33          0.21856E-01      15   0.64536E-08   0.12459E-07 0.12696E+00 
c  r12          0.93843E-03      18   0.71699E-08   0.29980E-09 0.60519E+00 
c  r13          0.46669E-02      19   0.70151E-08   0.14906E-08 0.19914E+00 
c  r23          0.39969E-02      19   0.69204E-08   0.12700E-08 0.19833E+00 
c  epsilon      0.10971E+02      11   0.34958E-08   0.98987E-02 0.16504E+00 
c  TempC        0.25716E+06      16   0.15106E-04   0.84277E-02 0.43320E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61356       0.0052543       0.0015074
v  Velocity[Y]            -0.57346         0.54425       0.0030789      0.00087328
v  Velocity[Z]              1.5655           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4371          4.3406          4.3632
v  Pressure                -36.419          360.07          87.679           169.9
v  r11                   0.0010599        0.081923        0.013069        0.018284
v  r22                   0.0011109        0.082647        0.013349        0.018644
v  r33                   0.0016352         0.17432        0.027241        0.037202
v  r12                   -0.010663        0.013598     -0.00023373     -0.00030927
v  r13                    -0.04556         0.05281      9.2771e-05       0.0010135
v  r23                    -0.04671        0.051221      3.0078e-05      0.00057438
v  epsilon                0.068592          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9772e-05       0.0099178      0.00092436       0.0017424
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2779          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71348         0.85283


 TIME FOR THE TIME STEP            10093:        0.78909E+02

===============================================================


 INSTANT    0.100940000E-01   TIME STEP NUMBER           10094
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.595852813E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.837399298E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.602471901E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.310669447E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.473721751E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81198E-03   0.45590E-02 0.20012E+01 
c  Velocity[X]                                      0.13855E-03 
c  Velocity[Y]                                      0.12933E-03 
c  Velocity[Z]                                      0.42911E-02 
c  Pressure     0.36683E-04     133   0.93396E-02   0.25876E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.65341E-08   0.16196E-08 0.99082E-01 
c  r22          0.10850E-01      13   0.55232E-08   0.18288E-08 0.10155E+00 
c  r33          0.21856E-01      15   0.68842E-08   0.12437E-07 0.12681E+00 
c  r12          0.93844E-03      18   0.70198E-08   0.29831E-09 0.60428E+00 
c  r13          0.46669E-02      20   0.54862E-08   0.14974E-08 0.19979E+00 
c  r23          0.39969E-02      19   0.66994E-08   0.12680E-08 0.19793E+00 
c  epsilon      0.10971E+02      11   0.34909E-08   0.97942E-02 0.16424E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.84707E-02 0.43381E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61353       0.0052543       0.0015073
v  Velocity[Y]            -0.57338         0.54441       0.0030788      0.00087325
v  Velocity[Z]              1.5652          5.4371          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4371          4.3406          4.3632
v  Pressure                -36.439          359.93            87.6          169.77
v  r11                   0.0010599        0.081927        0.013069        0.018284
v  r22                   0.0011109        0.082647        0.013349        0.018644
v  r33                   0.0016352         0.17435        0.027241        0.037202
v  r12                    -0.01066        0.013597     -0.00023374     -0.00030927
v  r13                   -0.045557         0.05281      9.2772e-05       0.0010136
v  r23                   -0.046709        0.051249      3.0079e-05      0.00057438
v  epsilon                0.068592           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9777e-05        0.009918      0.00092436       0.0017424
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2784          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71348         0.85283


 TIME FOR THE TIME STEP            10094:        0.81299E+02

===============================================================


 INSTANT    0.100950000E-01   TIME STEP NUMBER           10095
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.316695078E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120818427E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.583131561E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.809801594E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.330688498E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81197E-03   0.45525E-02 0.19982E+01 
c  Velocity[X]                                      0.13961E-03 
c  Velocity[Y]                                      0.12894E-03 
c  Velocity[Z]                                      0.42840E-02 
c  Pressure     0.36155E-04     134   0.92009E-02   0.25504E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.65439E-08   0.16761E-08 0.10047E+00 
c  r22          0.10850E-01      13   0.55092E-08   0.18167E-08 0.10112E+00 
c  r33          0.21856E-01      15   0.58027E-08   0.12600E-07 0.12755E+00 
c  r12          0.93844E-03      19   0.53901E-08   0.29992E-09 0.60546E+00 
c  r13          0.46669E-02      19   0.73720E-08   0.14724E-08 0.19909E+00 
c  r23          0.39969E-02      19   0.72695E-08   0.13254E-08 0.20149E+00 
c  epsilon      0.10971E+02      11   0.34410E-08   0.10262E-01 0.17166E+00 
c  TempC        0.25716E+06      16   0.15102E-04   0.84578E-02 0.43396E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61354       0.0052542       0.0015073
v  Velocity[Y]            -0.57343          0.5441       0.0030788      0.00087323
v  Velocity[Z]              1.5653          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4371          4.3406          4.3632
v  Pressure                -36.409          360.14          87.719          169.95
v  r11                   0.0010599        0.081922        0.013069        0.018284
v  r22                   0.0011109        0.082648        0.013349        0.018644
v  r33                   0.0016352         0.17434        0.027241        0.037202
v  r12                   -0.010664        0.013602     -0.00023374     -0.00030927
v  r13                   -0.045556        0.052809      9.2773e-05       0.0010136
v  r23                   -0.046708        0.051238      3.0079e-05      0.00057439
v  epsilon                0.068592           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9781e-05       0.0099177      0.00092437       0.0017424
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2783          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71348         0.85282


 TIME FOR THE TIME STEP            10095:        0.80995E+02

===============================================================


 INSTANT    0.100960000E-01   TIME STEP NUMBER           10096
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153527797E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.266127832E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.319172504E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157702325E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.951177744E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81204E-03   0.45153E-02 0.19904E+01 
c  Velocity[X]                                      0.13850E-03 
c  Velocity[Y]                                      0.13032E-03 
c  Velocity[Z]                                      0.42465E-02 
c  Pressure     0.36968E-04     132   0.94147E-02   0.26078E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59605E-08   0.16456E-08 0.99536E-01 
c  r22          0.10850E-01      13   0.53092E-08   0.18550E-08 0.10181E+00 
c  r33          0.21856E-01      15   0.62488E-08   0.12592E-07 0.12689E+00 
c  r12          0.93844E-03      18   0.69383E-08   0.30108E-09 0.60611E+00 
c  r13          0.46669E-02      19   0.69894E-08   0.15079E-08 0.19935E+00 
c  r23          0.39969E-02      20   0.57200E-08   0.12820E-08 0.19784E+00 
c  epsilon      0.10971E+02      11   0.34610E-08   0.10150E-01 0.16665E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.83754E-02 0.43216E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63396         0.61354       0.0052542       0.0015073
v  Velocity[Y]            -0.57346         0.54413       0.0030788      0.00087326
v  Velocity[Z]              1.5654          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4371          4.3406          4.3632
v  Pressure                -36.464          360.03          87.659          169.86
v  r11                   0.0010599        0.081929        0.013069        0.018284
v  r22                   0.0011109        0.082647        0.013349        0.018644
v  r33                   0.0016352          0.1743        0.027241        0.037202
v  r12                   -0.010662        0.013596     -0.00023374     -0.00030927
v  r13                   -0.045559        0.052806      9.2774e-05       0.0010136
v  r23                   -0.046707         0.05122       3.008e-05      0.00057439
v  epsilon                0.068593          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9784e-05       0.0099175      0.00092437       0.0017424
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2778          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71348         0.85283


 TIME FOR THE TIME STEP            10096:        0.79463E+02

===============================================================


 INSTANT    0.100970000E-01   TIME STEP NUMBER           10097
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.220084228E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.323523124E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.204287415E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.618218625E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172578009E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81186E-03   0.45347E-02 0.19949E+01 
c  Velocity[X]                                      0.13935E-03 
c  Velocity[Y]                                      0.12991E-03 
c  Velocity[Z]                                      0.42654E-02 
c  Pressure     0.36398E-04     133   0.92601E-02   0.25675E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.70973E-08   0.16566E-08 0.99803E-01 
c  r22          0.10850E-01      13   0.58294E-08   0.18496E-08 0.10166E+00 
c  r33          0.21856E-01      15   0.70772E-08   0.12662E-07 0.12767E+00 
c  r12          0.93844E-03      19   0.54102E-08   0.31271E-09 0.61540E+00 
c  r13          0.46669E-02      20   0.58026E-08   0.15117E-08 0.20028E+00 
c  r23          0.39969E-02      20   0.58860E-08   0.13126E-08 0.20141E+00 
c  epsilon      0.10971E+02      11   0.35097E-08   0.97445E-02 0.16287E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83904E-02 0.43244E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63396         0.61351       0.0052542       0.0015073
v  Velocity[Y]            -0.57359         0.54424       0.0030789      0.00087328
v  Velocity[Z]              1.5654          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4371          4.3406          4.3632
v  Pressure                -36.406          359.99          87.621          169.82
v  r11                   0.0010599        0.081935        0.013069        0.018284
v  r22                   0.0011109        0.082647        0.013349        0.018644
v  r33                   0.0016352         0.17432        0.027241        0.037202
v  r12                   -0.010658        0.013599     -0.00023374     -0.00030927
v  r13                   -0.045558        0.052806      9.2775e-05       0.0010136
v  r23                   -0.046706        0.051242      3.0081e-05      0.00057439
v  epsilon                0.068593          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9786e-05       0.0099176      0.00092437       0.0017424
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2778          0.1144         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71348         0.85283


 TIME FOR THE TIME STEP            10097:        0.77314E+02

===============================================================


 INSTANT    0.100980000E-01   TIME STEP NUMBER           10098
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.949902197E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.213027824E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.343767372E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.337797294E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154834165E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81249E-03   0.45351E-02 0.19945E+01 
c  Velocity[X]                                      0.13979E-03 
c  Velocity[Y]                                      0.12986E-03 
c  Velocity[Z]                                      0.42654E-02 
c  Pressure     0.36392E-04     131   0.92688E-02   0.25670E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.69198E-08   0.16778E-08 0.10069E+00 
c  r22          0.10850E-01      13   0.58380E-08   0.18420E-08 0.10199E+00 
c  r33          0.21856E-01      16   0.59084E-08   0.12639E-07 0.12816E+00 
c  r12          0.93844E-03      19   0.54003E-08   0.30303E-09 0.60856E+00 
c  r13          0.46669E-02      20   0.61429E-08   0.14994E-08 0.20018E+00 
c  r23          0.39969E-02      19   0.69303E-08   0.13086E-08 0.20081E+00 
c  epsilon      0.10971E+02      11   0.36955E-08   0.96397E-02 0.16378E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.85133E-02 0.43464E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63399         0.61352       0.0052543       0.0015073
v  Velocity[Y]            -0.57363         0.54445       0.0030788      0.00087319
v  Velocity[Z]              1.5656          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4371          4.3406          4.3632
v  Pressure                -36.459          360.09          87.698          169.91
v  r11                   0.0010599        0.081935        0.013069        0.018284
v  r22                   0.0011109        0.082647        0.013349        0.018644
v  r33                   0.0016352         0.17434        0.027241        0.037202
v  r12                   -0.010657        0.013595     -0.00023374     -0.00030927
v  r13                   -0.045557        0.052809      9.2776e-05       0.0010136
v  r23                   -0.046706        0.051233      3.0081e-05      0.00057438
v  epsilon                0.068593          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9786e-05       0.0099177      0.00092437       0.0017424
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017901           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85283


 TIME FOR THE TIME STEP            10098:        0.75821E+02

===============================================================


 INSTANT    0.100990000E-01   TIME STEP NUMBER           10099
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.303000668E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.428780749E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.491383576E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.176347720E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160395764E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81227E-03   0.45326E-02 0.19945E+01 
c  Velocity[X]                                      0.13888E-03 
c  Velocity[Y]                                      0.12967E-03 
c  Velocity[Z]                                      0.42640E-02 
c  Pressure     0.36429E-04     133   0.92714E-02   0.25696E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.69805E-08   0.16949E-08 0.10099E+00 
c  r22          0.10850E-01      13   0.57527E-08   0.18919E-08 0.10281E+00 
c  r33          0.21856E-01      15   0.71752E-08   0.12923E-07 0.12889E+00 
c  r12          0.93844E-03      19   0.54988E-08   0.30597E-09 0.61094E+00 
c  r13          0.46669E-02      19   0.72520E-08   0.15152E-08 0.20042E+00 
c  r23          0.39969E-02      19   0.57666E-08   0.13083E-08 0.20081E+00 
c  epsilon      0.10971E+02      11   0.35011E-08   0.10217E-01 0.16936E+00 
c  TempC        0.25716E+06      16   0.15124E-04   0.84506E-02 0.43401E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61354       0.0052542       0.0015073
v  Velocity[Y]            -0.57364         0.54414       0.0030788      0.00087324
v  Velocity[Z]              1.5653          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4371          4.3406          4.3632
v  Pressure                -36.397          360.04           87.65          169.85
v  r11                   0.0010599        0.081934        0.013069        0.018284
v  r22                   0.0011109        0.082649        0.013349        0.018644
v  r33                   0.0016352         0.17432        0.027241        0.037202
v  r12                   -0.010657        0.013603     -0.00023374     -0.00030927
v  r13                    -0.04556        0.052808      9.2776e-05       0.0010136
v  r23                   -0.046706        0.051216      3.0082e-05      0.00057438
v  epsilon                0.068594          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9789e-05       0.0099177      0.00092437       0.0017424
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85283


 TIME FOR THE TIME STEP            10099:        0.79166E+02

===============================================================


 INSTANT    0.101000000E-01   TIME STEP NUMBER           10100
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.832843867E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.176755869E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934906E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.167830672E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.279724670E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934912E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.279922907E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69802E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      40   0.81164E-03   0.45513E-02 0.19991E+01 
c  Velocity[X]                                      0.13930E-03 
c  Velocity[Y]                                      0.12909E-03 
c  Velocity[Z]                                      0.42829E-02 
c  Pressure     0.36624E-04     133   0.93250E-02   0.25834E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.67608E-08   0.16619E-08 0.99920E-01 
c  r22          0.10850E-01      13   0.57257E-08   0.18441E-08 0.10205E+00 
c  r33          0.21856E-01      15   0.65038E-08   0.12684E-07 0.12788E+00 
c  r12          0.93844E-03      18   0.66928E-08   0.30627E-09 0.60987E+00 
c  r13          0.46669E-02      19   0.64999E-08   0.15075E-08 0.20104E+00 
c  r23          0.39969E-02      19   0.59855E-08   0.13131E-08 0.20055E+00 
c  epsilon      0.10971E+02      11   0.32765E-08   0.10169E-01 0.16771E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.83784E-02 0.43188E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397          0.6135       0.0052542       0.0015072
v  Velocity[Y]            -0.57357         0.54416       0.0030788      0.00087321
v  Velocity[Z]              1.5654          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4371          4.3406          4.3632
v  Pressure                -36.456          360.04          87.687          169.88
v  r11                   0.0010599        0.081928        0.013069        0.018284
v  r22                   0.0011109        0.082649        0.013349        0.018644
v  r33                   0.0016352          0.1743        0.027241        0.037202
v  r12                   -0.010657        0.013601     -0.00023374     -0.00030927
v  r13                   -0.045557        0.052808      9.2777e-05       0.0010136
v  r23                   -0.046707        0.051235      3.0083e-05      0.00057439
v  epsilon                0.068594          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9794e-05       0.0099177      0.00092437       0.0017424
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017901           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85283


 TIME FOR THE TIME STEP            10100:        0.79897E+02

===============================================================


 INSTANT    0.101010000E-01   TIME STEP NUMBER           10101
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.341340282E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.648996537E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.142949954E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200716214E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.266279996E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81256E-03   0.45413E-02 0.19983E+01 
c  Velocity[X]                                      0.13891E-03 
c  Velocity[Y]                                      0.13058E-03 
c  Velocity[Z]                                      0.42718E-02 
c  Pressure     0.36804E-04     131   0.93681E-02   0.25962E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.65450E-08   0.16851E-08 0.10133E+00 
c  r22          0.10850E-01      13   0.53963E-08   0.18646E-08 0.10287E+00 
c  r33          0.21857E-01      15   0.62178E-08   0.12776E-07 0.12935E+00 
c  r12          0.93844E-03      18   0.61842E-08   0.30417E-09 0.61266E+00 
c  r13          0.46669E-02      19   0.57114E-08   0.14956E-08 0.20100E+00 
c  r23          0.39969E-02      19   0.62456E-08   0.13141E-08 0.20275E+00 
c  epsilon      0.10971E+02      11   0.32544E-08   0.10072E-01 0.17053E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84134E-02 0.43304E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63396         0.61354       0.0052542       0.0015073
v  Velocity[Y]            -0.57365         0.54435       0.0030788      0.00087323
v  Velocity[Z]              1.5653          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4371          4.3406          4.3632
v  Pressure                -36.408          360.12          87.711          169.93
v  r11                   0.0010599        0.081932        0.013069        0.018284
v  r22                   0.0011109        0.082644        0.013349        0.018644
v  r33                   0.0016352         0.17431        0.027241        0.037202
v  r12                   -0.010658        0.013598     -0.00023374     -0.00030927
v  r13                   -0.045558        0.052808      9.2778e-05       0.0010136
v  r23                   -0.046707        0.051223      3.0084e-05      0.00057439
v  epsilon                0.068594          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9797e-05       0.0099178      0.00092437       0.0017424
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2772          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71348         0.85282


 TIME FOR THE TIME STEP            10101:        0.78138E+02

===============================================================


 INSTANT    0.101020000E-01   TIME STEP NUMBER           10102
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.662386714E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.734406321E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283806008E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162920590E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.286001212E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69801E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81237E-03   0.45611E-02 0.19991E+01 
c  Velocity[X]                                      0.13829E-03 
c  Velocity[Y]                                      0.13007E-03 
c  Velocity[Z]                                      0.42927E-02 
c  Pressure     0.36575E-04     133   0.93160E-02   0.25799E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.66626E-08   0.16435E-08 0.99604E-01 
c  r22          0.10850E-01      13   0.54695E-08   0.18640E-08 0.10211E+00 
c  r33          0.21857E-01      16   0.59363E-08   0.12657E-07 0.12765E+00 
c  r12          0.93844E-03      18   0.64674E-08   0.30207E-09 0.60697E+00 
c  r13          0.46669E-02      19   0.63684E-08   0.15182E-08 0.20052E+00 
c  r23          0.39969E-02      19   0.62504E-08   0.12804E-08 0.19873E+00 
c  epsilon      0.10971E+02      11   0.35397E-08   0.10040E-01 0.16597E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.83829E-02 0.43169E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61357       0.0052542       0.0015073
v  Velocity[Y]            -0.57356         0.54419       0.0030788      0.00087324
v  Velocity[Z]              1.5653          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4371          4.3406          4.3632
v  Pressure                -36.438           360.1          87.708          169.92
v  r11                   0.0010599        0.081935        0.013069        0.018284
v  r22                    0.001111        0.082646        0.013349        0.018644
v  r33                   0.0016352         0.17434        0.027241        0.037202
v  r12                   -0.010663        0.013603     -0.00023374     -0.00030927
v  r13                    -0.04556         0.05281      9.2779e-05       0.0010136
v  r23                   -0.046708        0.051218      3.0085e-05      0.00057439
v  epsilon                0.068595          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9799e-05       0.0099178      0.00092438       0.0017424
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2766          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71349         0.85283


 TIME FOR THE TIME STEP            10102:        0.80240E+02

===============================================================


 INSTANT    0.101030000E-01   TIME STEP NUMBER           10103
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.475481357E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160182517E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.354950964E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935020E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.126640946E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.287564917E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69800E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81290E-03   0.45387E-02 0.19964E+01 
c  Velocity[X]                                      0.13900E-03 
c  Velocity[Y]                                      0.12965E-03 
c  Velocity[Z]                                      0.42701E-02 
c  Pressure     0.36140E-04     133   0.92025E-02   0.25493E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.64882E-08   0.16486E-08 0.10029E+00 
c  r22          0.10850E-01      13   0.53292E-08   0.18606E-08 0.10263E+00 
c  r33          0.21857E-01      15   0.67211E-08   0.12662E-07 0.12831E+00 
c  r12          0.93844E-03      18   0.62267E-08   0.30621E-09 0.61328E+00 
c  r13          0.46669E-02      19   0.65046E-08   0.15077E-08 0.20071E+00 
c  r23          0.39969E-02      19   0.60815E-08   0.12991E-08 0.20085E+00 
c  epsilon      0.10971E+02      11   0.35534E-08   0.97126E-02 0.16471E+00 
c  TempC        0.25716E+06      16   0.15090E-04   0.84727E-02 0.43430E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61353       0.0052542       0.0015073
v  Velocity[Y]             -0.5735         0.54429       0.0030788      0.00087322
v  Velocity[Z]              1.5657          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4371          4.3406          4.3632
v  Pressure                -36.391          360.01          87.649          169.84
v  r11                   0.0010599        0.081943        0.013069        0.018284
v  r22                    0.001111        0.082647        0.013349        0.018644
v  r33                   0.0016352         0.17433        0.027241        0.037202
v  r12                   -0.010664        0.013605     -0.00023374     -0.00030927
v  r13                   -0.045558        0.052807       9.278e-05       0.0010136
v  r23                   -0.046708        0.051242      3.0087e-05      0.00057439
v  epsilon                0.068595          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9805e-05       0.0099178      0.00092438       0.0017424
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2766          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71348         0.85282


 TIME FOR THE TIME STEP            10103:        0.74794E+02

===============================================================


 INSTANT    0.101040000E-01   TIME STEP NUMBER           10104
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.329152572E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.385506072E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.902866682E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.405507991E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.266203989E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81148E-03   0.45671E-02 0.20007E+01 
c  Velocity[X]                                      0.14016E-03 
c  Velocity[Y]                                      0.12966E-03 
c  Velocity[Z]                                      0.42973E-02 
c  Pressure     0.36662E-04     133   0.93367E-02   0.25862E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60560E-08   0.16407E-08 0.99959E-01 
c  r22          0.10850E-01      13   0.50990E-08   0.18341E-08 0.10176E+00 
c  r33          0.21857E-01      15   0.52932E-08   0.12583E-07 0.12771E+00 
c  r12          0.93844E-03      18   0.61824E-08   0.30322E-09 0.61134E+00 
c  r13          0.46669E-02      19   0.60232E-08   0.14887E-08 0.19987E+00 
c  r23          0.39969E-02      19   0.60229E-08   0.12685E-08 0.19883E+00 
c  epsilon      0.10971E+02      11   0.34499E-08   0.10169E-01 0.16822E+00 
c  TempC        0.25716E+06      16   0.15180E-04   0.84814E-02 0.43438E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63395         0.61357       0.0052543       0.0015073
v  Velocity[Y]            -0.57342          0.5443       0.0030788      0.00087321
v  Velocity[Z]              1.5656           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5793           5.437          4.3406          4.3632
v  Pressure                -36.449          360.07           87.69          169.89
v  r11                   0.0010599        0.081946        0.013069        0.018284
v  r22                    0.001111        0.082648        0.013349        0.018644
v  r33                   0.0016352         0.17431        0.027241        0.037202
v  r12                   -0.010664          0.0136     -0.00023374     -0.00030927
v  r13                   -0.045557        0.052807       9.278e-05       0.0010136
v  r23                   -0.046709        0.051227      3.0088e-05      0.00057439
v  epsilon                0.068595          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9808e-05       0.0099177      0.00092438       0.0017424
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2771          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71348         0.85282


 TIME FOR THE TIME STEP            10104:        0.78217E+02

===============================================================


 INSTANT    0.101050000E-01   TIME STEP NUMBER           10105
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.273399930E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209758061E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.135602119E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.345315422E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.538724268E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21888E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      40   0.81159E-03   0.45297E-02 0.19906E+01 
c  Velocity[X]                                      0.13871E-03 
c  Velocity[Y]                                      0.12889E-03 
c  Velocity[Z]                                      0.42621E-02 
c  Pressure     0.36449E-04     132   0.92780E-02   0.25711E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59992E-08   0.16597E-08 0.10078E+00 
c  r22          0.10850E-01      13   0.52039E-08   0.18285E-08 0.10182E+00 
c  r33          0.21857E-01      15   0.54966E-08   0.12574E-07 0.12798E+00 
c  r12          0.93844E-03      18   0.62578E-08   0.29533E-09 0.60655E+00 
c  r13          0.46669E-02      19   0.69278E-08   0.15035E-08 0.20062E+00 
c  r23          0.39969E-02      19   0.52115E-08   0.12891E-08 0.20062E+00 
c  epsilon      0.10971E+02      11   0.33374E-08   0.98972E-02 0.16492E+00 
c  TempC        0.25716E+06      16   0.15107E-04   0.84256E-02 0.43314E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162016


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61357       0.0052543       0.0015073
v  Velocity[Y]             -0.5736         0.54433       0.0030788      0.00087321
v  Velocity[Z]              1.5658          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4371          4.3406          4.3632
v  Pressure                -36.398          360.07           87.67          169.89
v  r11                   0.0010599        0.081943        0.013069        0.018284
v  r22                    0.001111        0.082649        0.013349        0.018644
v  r33                   0.0016352         0.17432        0.027241        0.037202
v  r12                   -0.010666        0.013601     -0.00023374     -0.00030927
v  r13                   -0.045561        0.052805      9.2781e-05       0.0010136
v  r23                    -0.04671         0.05121      3.0089e-05      0.00057439
v  epsilon                0.068596          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9811e-05       0.0099176      0.00092438       0.0017424
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85282


 TIME FOR THE TIME STEP            10105:        0.79610E+02

===============================================================


 INSTANT    0.101060000E-01   TIME STEP NUMBER           10106
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.182151188E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.396399089E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934918E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.638241597E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.206339437E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.560037401E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40361E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81264E-03   0.45419E-02 0.19963E+01 
c  Velocity[X]                                      0.13888E-03 
c  Velocity[Y]                                      0.13003E-03 
c  Velocity[Z]                                      0.42730E-02 
c  Pressure     0.36509E-04     133   0.93014E-02   0.25753E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57952E-08   0.16070E-08 0.99319E-01 
c  r22          0.10850E-01      13   0.50360E-08   0.18102E-08 0.10147E+00 
c  r33          0.21857E-01      14   0.70539E-08   0.12320E-07 0.12675E+00 
c  r12          0.93844E-03      18   0.68070E-08   0.29831E-09 0.60540E+00 
c  r13          0.46669E-02      19   0.59352E-08   0.14918E-08 0.20002E+00 
c  r23          0.39969E-02      19   0.51059E-08   0.12786E-08 0.19879E+00 
c  epsilon      0.10971E+02      11   0.33323E-08   0.94799E-02 0.16227E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.84384E-02 0.43359E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61355       0.0052542       0.0015073
v  Velocity[Y]            -0.57351          0.5444       0.0030788      0.00087319
v  Velocity[Z]              1.5659           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5796           5.437          4.3406          4.3632
v  Pressure                -36.453          359.99          87.649          169.83
v  r11                   0.0010599        0.081942        0.013069        0.018284
v  r22                    0.001111         0.08265        0.013349        0.018644
v  r33                   0.0016352         0.17434        0.027241        0.037202
v  r12                   -0.010667        0.013599     -0.00023374     -0.00030927
v  r13                   -0.045558        0.052808      9.2782e-05       0.0010136
v  r23                    -0.04671        0.051235      3.0089e-05      0.00057439
v  epsilon                0.068596          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9814e-05       0.0099176      0.00092438       0.0017424
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2783          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71349         0.85283


 TIME FOR THE TIME STEP            10106:        0.77989E+02

===============================================================


 INSTANT    0.101070000E-01   TIME STEP NUMBER           10107
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.441621981E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.228588706E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.498800468E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172336052E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107371975E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81186E-03   0.45641E-02 0.20001E+01 
c  Velocity[X]                                      0.13922E-03 
c  Velocity[Y]                                      0.12856E-03 
c  Velocity[Z]                                      0.42963E-02 
c  Pressure     0.36577E-04     133   0.93092E-02   0.25801E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54292E-08   0.16518E-08 0.10030E+00 
c  r22          0.10850E-01      13   0.49931E-08   0.18077E-08 0.10107E+00 
c  r33          0.21857E-01      14   0.68906E-08   0.12501E-07 0.12742E+00 
c  r12          0.93844E-03      18   0.63084E-08   0.29886E-09 0.60655E+00 
c  r13          0.46669E-02      18   0.71718E-08   0.14692E-08 0.19869E+00 
c  r23          0.39969E-02      18   0.68682E-08   0.12892E-08 0.20010E+00 
c  epsilon      0.10971E+02      11   0.32067E-08   0.10023E-01 0.16969E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.84635E-02 0.43374E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162015


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61364       0.0052542       0.0015073
v  Velocity[Y]             -0.5736         0.54422       0.0030788      0.00087321
v  Velocity[Z]              1.5654           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5792           5.437          4.3406          4.3632
v  Pressure                -36.424          360.06          87.681          169.89
v  r11                   0.0010599        0.081938        0.013069        0.018284
v  r22                    0.001111         0.08265        0.013349        0.018644
v  r33                   0.0016352         0.17432        0.027241        0.037202
v  r12                   -0.010674          0.0136     -0.00023374     -0.00030927
v  r13                   -0.045557        0.052806      9.2783e-05       0.0010136
v  r23                    -0.04671        0.051219      3.0091e-05      0.00057439
v  epsilon                0.068597          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9819e-05       0.0099177      0.00092438       0.0017424
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2788          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71348         0.85282


 TIME FOR THE TIME STEP            10107:        0.77289E+02

===============================================================


 INSTANT    0.101080000E-01   TIME STEP NUMBER           10108
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.295439702E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.215107691E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.234163448E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.381312272E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.190680307E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81320E-03   0.45015E-02 0.19873E+01 
c  Velocity[X]                                      0.13846E-03 
c  Velocity[Y]                                      0.12912E-03 
c  Velocity[Z]                                      0.42339E-02 
c  Pressure     0.36252E-04     132   0.92316E-02   0.25572E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.50334E-08   0.16278E-08 0.99517E-01 
c  r22          0.10850E-01      13   0.50520E-08   0.18030E-08 0.10094E+00 
c  r33          0.21857E-01      15   0.56474E-08   0.12391E-07 0.12661E+00 
c  r12          0.93844E-03      18   0.60951E-08   0.29235E-09 0.59985E+00 
c  r13          0.46669E-02      19   0.54708E-08   0.14792E-08 0.19873E+00 
c  r23          0.39969E-02      19   0.53560E-08   0.12712E-08 0.19811E+00 
c  epsilon      0.10971E+02      11   0.33329E-08   0.98632E-02 0.16538E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.83966E-02 0.43211E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61362       0.0052542       0.0015073
v  Velocity[Y]            -0.57359         0.54434       0.0030788      0.00087321
v  Velocity[Z]              1.5656           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5794           5.437          4.3406          4.3632
v  Pressure                -36.427          360.04           87.66          169.87
v  r11                   0.0010599        0.081927        0.013069        0.018284
v  r22                    0.001111         0.08265        0.013349        0.018644
v  r33                   0.0016352         0.17428        0.027241        0.037202
v  r12                   -0.010673        0.013601     -0.00023374     -0.00030927
v  r13                    -0.04556        0.052806      9.2785e-05       0.0010136
v  r23                   -0.046711        0.051205      3.0092e-05      0.00057439
v  epsilon                0.068597          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9821e-05       0.0099178      0.00092438       0.0017424
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2787          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71348         0.85282


 TIME FOR THE TIME STEP            10108:        0.77267E+02

===============================================================


 INSTANT    0.101090000E-01   TIME STEP NUMBER           10109
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.460100622E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172222159E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168042510E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.250651008E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.987745898E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81145E-03   0.45441E-02 0.19964E+01 
c  Velocity[X]                                      0.13872E-03 
c  Velocity[Y]                                      0.13011E-03 
c  Velocity[Z]                                      0.42753E-02 
c  Pressure     0.36438E-04     135   0.92787E-02   0.25703E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59232E-08   0.16257E-08 0.98935E-01 
c  r22          0.10850E-01      13   0.52849E-08   0.18198E-08 0.10086E+00 
c  r33          0.21857E-01      14   0.70459E-08   0.12482E-07 0.12638E+00 
c  r12          0.93844E-03      18   0.69229E-08   0.29698E-09 0.60191E+00 
c  r13          0.46669E-02      19   0.64000E-08   0.15016E-08 0.19847E+00 
c  r23          0.39969E-02      19   0.65837E-08   0.12863E-08 0.19899E+00 
c  epsilon      0.10971E+02      11   0.34460E-08   0.99205E-02 0.16421E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84409E-02 0.43346E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61356       0.0052543       0.0015073
v  Velocity[Y]            -0.57359         0.54432       0.0030789      0.00087325
v  Velocity[Z]              1.5656           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5794           5.437          4.3406          4.3632
v  Pressure                -36.417          360.04          87.656          169.86
v  r11                   0.0010599        0.081925        0.013069        0.018284
v  r22                    0.001111        0.082645        0.013349        0.018644
v  r33                   0.0016352          0.1743        0.027241        0.037202
v  r12                   -0.010671        0.013599     -0.00023374     -0.00030927
v  r13                   -0.045559        0.052808      9.2786e-05       0.0010136
v  r23                   -0.046711        0.051224      3.0093e-05      0.00057439
v  epsilon                0.068598          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9825e-05       0.0099178      0.00092438       0.0017424
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2791          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71348         0.85282


 TIME FOR THE TIME STEP            10109:        0.81783E+02

===============================================================


 INSTANT    0.101100000E-01   TIME STEP NUMBER           10110
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115354635E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.908104472E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.198513358E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.159764459E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.425992681E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      40   0.81220E-03   0.45767E-02 0.20029E+01 
c  Velocity[X]                                      0.14045E-03 
c  Velocity[Y]                                      0.13019E-03 
c  Velocity[Z]                                      0.43061E-02 
c  Pressure     0.36519E-04     131   0.92992E-02   0.25760E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.56684E-08   0.16248E-08 0.99130E-01 
c  r22          0.10850E-01      13   0.53338E-08   0.18041E-08 0.10089E+00 
c  r33          0.21857E-01      14   0.67641E-08   0.12397E-07 0.12642E+00 
c  r12          0.93844E-03      18   0.63730E-08   0.29887E-09 0.60406E+00 
c  r13          0.46669E-02      19   0.63681E-08   0.14769E-08 0.19878E+00 
c  r23          0.39969E-02      19   0.52457E-08   0.12810E-08 0.19847E+00 
c  epsilon      0.10971E+02      11   0.34628E-08   0.98759E-02 0.16456E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.84455E-02 0.43354E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61361       0.0052542       0.0015073
v  Velocity[Y]            -0.57354         0.54441       0.0030788      0.00087321
v  Velocity[Z]              1.5656           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5794           5.437          4.3406          4.3632
v  Pressure                -36.459          360.05          87.684          169.88
v  r11                   0.0010599        0.081924        0.013069        0.018284
v  r22                    0.001111        0.082647        0.013349        0.018644
v  r33                   0.0016352         0.17433        0.027241        0.037202
v  r12                   -0.010667        0.013594     -0.00023374     -0.00030927
v  r13                   -0.045557        0.052808      9.2787e-05       0.0010136
v  r23                    -0.04671        0.051205      3.0094e-05      0.00057439
v  epsilon                0.068598          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.983e-05       0.0099179      0.00092439       0.0017424
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2788          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71349         0.85283


 TIME FOR THE TIME STEP            10110:        0.81124E+02

===============================================================


 INSTANT    0.101110000E-01   TIME STEP NUMBER           10111
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.366117721E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.865463182E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.552730739E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935022E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294714457E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.125478126E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81272E-03   0.45398E-02 0.19966E+01 
c  Velocity[X]                                      0.13898E-03 
c  Velocity[Y]                                      0.12962E-03 
c  Velocity[Z]                                      0.42712E-02 
c  Pressure     0.36848E-04     134   0.93815E-02   0.25992E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57307E-08   0.16474E-08 0.10003E+00 
c  r22          0.10850E-01      13   0.50254E-08   0.18274E-08 0.10129E+00 
c  r33          0.21857E-01      15   0.54644E-08   0.12453E-07 0.12681E+00 
c  r12          0.93844E-03      18   0.60704E-08   0.29475E-09 0.60406E+00 
c  r13          0.46669E-02      20   0.59679E-08   0.14805E-08 0.19835E+00 
c  r23          0.39969E-02      19   0.53589E-08   0.12758E-08 0.19861E+00 
c  epsilon      0.10971E+02      11   0.34500E-08   0.98855E-02 0.16574E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.84525E-02 0.43399E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61362       0.0052543       0.0015073
v  Velocity[Y]            -0.57344         0.54451       0.0030789      0.00087324
v  Velocity[Z]              1.5657           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5795           5.437          4.3406          4.3632
v  Pressure                -36.398          360.04          87.654          169.87
v  r11                   0.0010599        0.081928        0.013069        0.018284
v  r22                    0.001111        0.082648        0.013349        0.018644
v  r33                   0.0016352          0.1743        0.027241        0.037202
v  r12                   -0.010667        0.013604     -0.00023374     -0.00030927
v  r13                    -0.04556        0.052806      9.2788e-05       0.0010136
v  r23                    -0.04671        0.051184      3.0095e-05      0.00057439
v  epsilon                0.068599          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9832e-05       0.0099179      0.00092439       0.0017424
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb               0.00179           5.279          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71348         0.85283


 TIME FOR THE TIME STEP            10111:        0.82173E+02

===============================================================


 INSTANT    0.101120000E-01   TIME STEP NUMBER           10112
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.916977655E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.426667986E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.117975028E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130860981E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195058531E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81257E-03   0.45355E-02 0.19942E+01 
c  Velocity[X]                                      0.13881E-03 
c  Velocity[Y]                                      0.12956E-03 
c  Velocity[Z]                                      0.42671E-02 
c  Pressure     0.36502E-04     131   0.92912E-02   0.25748E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.63966E-08   0.16383E-08 0.99383E-01 
c  r22          0.10850E-01      13   0.51605E-08   0.17957E-08 0.10089E+00 
c  r33          0.21857E-01      14   0.71090E-08   0.12349E-07 0.12631E+00 
c  r12          0.93844E-03      18   0.70488E-08   0.29816E-09 0.60453E+00 
c  r13          0.46669E-02      19   0.67626E-08   0.14650E-08 0.19808E+00 
c  r23          0.39969E-02      19   0.56424E-08   0.12817E-08 0.19800E+00 
c  epsilon      0.10971E+02      11   0.32467E-08   0.98295E-02 0.16550E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84447E-02 0.43348E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61355       0.0052543       0.0015073
v  Velocity[Y]            -0.57336         0.54428       0.0030789      0.00087321
v  Velocity[Z]              1.5656           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5794           5.437          4.3406          4.3632
v  Pressure                -36.471          359.99           87.62          169.81
v  r11                   0.0010599        0.081924        0.013069        0.018284
v  r22                    0.001111        0.082648        0.013349        0.018644
v  r33                   0.0016352         0.17428        0.027241        0.037202
v  r12                   -0.010666        0.013606     -0.00023374     -0.00030927
v  r13                   -0.045558        0.052805      9.2789e-05       0.0010136
v  r23                    -0.04671        0.051216      3.0096e-05      0.00057439
v  epsilon                0.068599          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9834e-05       0.0099178      0.00092439       0.0017424
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2791          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71348         0.85282


 TIME FOR THE TIME STEP            10112:        0.81228E+02

===============================================================


 INSTANT    0.101130000E-01   TIME STEP NUMBER           10113
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141993713E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.559756166E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136516007E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.277403421E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.465912422E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81163E-03   0.44996E-02 0.19883E+01 
c  Velocity[X]                                      0.13918E-03 
c  Velocity[Y]                                      0.12921E-03 
c  Velocity[Z]                                      0.42312E-02 
c  Pressure     0.36379E-04     133   0.92656E-02   0.25662E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.62870E-08   0.16800E-08 0.10031E+00 
c  r22          0.10850E-01      13   0.46588E-08   0.18485E-08 0.10158E+00 
c  r33          0.21857E-01      15   0.50944E-08   0.12824E-07 0.12808E+00 
c  r12          0.93844E-03      18   0.57413E-08   0.30318E-09 0.60853E+00 
c  r13          0.46669E-02      20   0.59304E-08   0.14952E-08 0.20017E+00 
c  r23          0.39969E-02      19   0.62042E-08   0.13367E-08 0.20204E+00 
c  epsilon      0.10971E+02      11   0.34976E-08   0.10476E-01 0.17299E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.84474E-02 0.43353E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369         0.61361       0.0052543       0.0015074
v  Velocity[Y]            -0.57348         0.54439       0.0030789      0.00087327
v  Velocity[Z]              1.5656           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5794           5.437          4.3406          4.3632
v  Pressure                -36.459          360.05          87.657          169.87
v  r11                   0.0010599         0.08192        0.013069        0.018284
v  r22                    0.001111        0.082647        0.013349        0.018644
v  r33                   0.0016352         0.17429        0.027241        0.037202
v  r12                   -0.010665          0.0136     -0.00023374     -0.00030927
v  r13                   -0.045559        0.052804       9.279e-05       0.0010136
v  r23                   -0.046709        0.051206      3.0097e-05      0.00057439
v  epsilon                  0.0686          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9836e-05       0.0099179      0.00092439       0.0017424
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb               0.00179           5.279          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71348         0.85282


 TIME FOR THE TIME STEP            10113:        0.85323E+02

===============================================================


 INSTANT    0.101140000E-01   TIME STEP NUMBER           10114
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.214526237E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133311835E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.156241819E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.121346672E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.173816814E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81261E-03   0.45514E-02 0.19979E+01 
c  Velocity[X]                                      0.13870E-03 
c  Velocity[Y]                                      0.13029E-03 
c  Velocity[Z]                                      0.42824E-02 
c  Pressure     0.36637E-04     133   0.93323E-02   0.25844E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.63041E-08   0.16501E-08 0.99759E-01 
c  r22          0.10850E-01      13   0.47054E-08   0.18720E-08 0.10228E+00 
c  r33          0.21857E-01      15   0.61715E-08   0.12767E-07 0.12804E+00 
c  r12          0.93844E-03      18   0.57956E-08   0.30506E-09 0.60962E+00 
c  r13          0.46669E-02      19   0.69747E-08   0.15124E-08 0.20050E+00 
c  r23          0.39969E-02      19   0.67128E-08   0.12997E-08 0.20064E+00 
c  epsilon      0.10971E+02      11   0.37479E-08   0.10074E-01 0.16729E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.84216E-02 0.43293E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61361       0.0052543       0.0015073
v  Velocity[Y]            -0.57357         0.54452       0.0030789      0.00087326
v  Velocity[Z]              1.5655           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5793           5.437          4.3406          4.3632
v  Pressure                -36.458          360.02          87.651          169.85
v  r11                   0.0010599        0.081914        0.013069        0.018284
v  r22                    0.001111        0.082646        0.013349        0.018644
v  r33                   0.0016352         0.17431        0.027241        0.037202
v  r12                   -0.010668          0.0136     -0.00023374     -0.00030927
v  r13                   -0.045562        0.052805      9.2791e-05       0.0010136
v  r23                   -0.046709        0.051198      3.0098e-05       0.0005744
v  epsilon                  0.0686          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9835e-05       0.0099179      0.00092439       0.0017424
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2789          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71348         0.85282


 TIME FOR THE TIME STEP            10114:        0.83574E+02

===============================================================


 INSTANT    0.101150000E-01   TIME STEP NUMBER           10115
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.133893629E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.665665205E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.280842044E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.515889458E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227426537E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81176E-03   0.45468E-02 0.20002E+01 
c  Velocity[X]                                      0.13951E-03 
c  Velocity[Y]                                      0.12967E-03 
c  Velocity[Z]                                      0.42776E-02 
c  Pressure     0.36564E-04     131   0.93037E-02   0.25792E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.61614E-08   0.16250E-08 0.99350E-01 
c  r22          0.10850E-01      13   0.50858E-08   0.18188E-08 0.10146E+00 
c  r33          0.21857E-01      15   0.67207E-08   0.12373E-07 0.12687E+00 
c  r12          0.93844E-03      18   0.56824E-08   0.29772E-09 0.60500E+00 
c  r13          0.46669E-02      20   0.56244E-08   0.14918E-08 0.19976E+00 
c  r23          0.39969E-02      20   0.57154E-08   0.12763E-08 0.19872E+00 
c  epsilon      0.10971E+02      11   0.36633E-08   0.94643E-02 0.16198E+00 
c  TempC        0.25716E+06      16   0.15105E-04   0.84037E-02 0.43255E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379         0.61356       0.0052543       0.0015073
v  Velocity[Y]            -0.57361         0.54433       0.0030789      0.00087326
v  Velocity[Z]              1.5653           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5791           5.437          4.3406          4.3632
v  Pressure                -36.426          360.06          87.667          169.88
v  r11                   0.0010599        0.081911        0.013069        0.018284
v  r22                    0.001111        0.082645        0.013349        0.018644
v  r33                   0.0016352         0.17434        0.027241        0.037202
v  r12                   -0.010673          0.0136     -0.00023374     -0.00030927
v  r13                   -0.045559        0.052802      9.2792e-05       0.0010136
v  r23                   -0.046709         0.05122      3.0098e-05       0.0005744
v  epsilon                0.068601          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9834e-05       0.0099179      0.00092439       0.0017424
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2791          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71348         0.85282


 TIME FOR THE TIME STEP            10115:        0.83062E+02

===============================================================


 INSTANT    0.101160000E-01   TIME STEP NUMBER           10116
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.501046192E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.322862390E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117908454E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.158870144E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.429264665E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69797E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81292E-03   0.45281E-02 0.19929E+01 
c  Velocity[X]                                      0.13916E-03 
c  Velocity[Y]                                      0.12937E-03 
c  Velocity[Z]                                      0.42595E-02 
c  Pressure     0.36368E-04     131   0.92590E-02   0.25654E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.61759E-08   0.16158E-08 0.99223E-01 
c  r22          0.10850E-01      13   0.53273E-08   0.18221E-08 0.10144E+00 
c  r33          0.21857E-01      15   0.62315E-08   0.12443E-07 0.12700E+00 
c  r12          0.93844E-03      18   0.63033E-08   0.29363E-09 0.60069E+00 
c  r13          0.46669E-02      20   0.61671E-08   0.14775E-08 0.19910E+00 
c  r23          0.39969E-02      20   0.67213E-08   0.12742E-08 0.19836E+00 
c  epsilon      0.10971E+02      11   0.34748E-08   0.98918E-02 0.16498E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.84560E-02 0.43432E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61362       0.0052543       0.0015073
v  Velocity[Y]            -0.57362         0.54432       0.0030789      0.00087326
v  Velocity[Z]              1.5656           5.437          4.3388          4.3625
v  ǁVelocityǁ               1.5793           5.437          4.3406          4.3632
v  Pressure                -36.425          360.06          87.685          169.88
v  r11                   0.0010599        0.081906        0.013069        0.018284
v  r22                    0.001111        0.082644        0.013349        0.018644
v  r33                   0.0016352         0.17432        0.027241        0.037202
v  r12                   -0.010672        0.013597     -0.00023374     -0.00030927
v  r13                   -0.045557        0.052803      9.2793e-05       0.0010136
v  r23                   -0.046709        0.051211        3.01e-05       0.0005744
v  epsilon                0.068601          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9834e-05       0.0099175      0.00092439       0.0017424
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2793         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8793         0.71349         0.85283


 TIME FOR THE TIME STEP            10116:        0.82730E+02

===============================================================


 INSTANT    0.101170000E-01   TIME STEP NUMBER           10117
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.114678069E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.970360312E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.978453460E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935012E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.782212045E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.508049304E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81188E-03   0.45198E-02 0.19908E+01 
c  Velocity[X]                                      0.13754E-03 
c  Velocity[Y]                                      0.12901E-03 
c  Velocity[Z]                                      0.42532E-02 
c  Pressure     0.36129E-04     133   0.92043E-02   0.25484E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60173E-08   0.16346E-08 0.99266E-01 
c  r22          0.10850E-01      13   0.54962E-08   0.18267E-08 0.10106E+00 
c  r33          0.21857E-01      14   0.66483E-08   0.12499E-07 0.12666E+00 
c  r12          0.93845E-03      18   0.64974E-08   0.29510E-09 0.60134E+00 
c  r13          0.46669E-02      20   0.57001E-08   0.14923E-08 0.19872E+00 
c  r23          0.39969E-02      20   0.61926E-08   0.12773E-08 0.19849E+00 
c  epsilon      0.10971E+02      11   0.33701E-08   0.99474E-02 0.16596E+00 
c  TempC        0.25716E+06      16   0.15105E-04   0.84262E-02 0.43311E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61364       0.0052543       0.0015073
v  Velocity[Y]            -0.57358         0.54438        0.003079      0.00087329
v  Velocity[Z]              1.5656          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4371          4.3406          4.3632
v  Pressure                -36.377          360.03          87.635          169.85
v  r11                   0.0010599        0.081901        0.013069        0.018284
v  r22                    0.001111        0.082639         0.01335        0.018644
v  r33                   0.0016352         0.17428        0.027241        0.037202
v  r12                   -0.010672        0.013595     -0.00023374     -0.00030927
v  r13                   -0.045561        0.052803      9.2793e-05       0.0010136
v  r23                   -0.046709        0.051198      3.0101e-05       0.0005744
v  epsilon                0.068602          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9836e-05       0.0099175      0.00092439       0.0017424
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2787          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71348         0.85283


 TIME FOR THE TIME STEP            10117:        0.81785E+02

===============================================================


 INSTANT    0.101180000E-01   TIME STEP NUMBER           10118
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.522298596E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.901685569E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934912E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.824065112E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.361594568E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.147601213E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81207E-03   0.45333E-02 0.19964E+01 
c  Velocity[X]                                      0.13954E-03 
c  Velocity[Y]                                      0.12970E-03 
c  Velocity[Z]                                      0.42641E-02 
c  Pressure     0.36414E-04     133   0.92725E-02   0.25686E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.62889E-08   0.16096E-08 0.98951E-01 
c  r22          0.10850E-01      13   0.55551E-08   0.18220E-08 0.10130E+00 
c  r33          0.21857E-01      14   0.70284E-08   0.12417E-07 0.12662E+00 
c  r12          0.93845E-03      18   0.68444E-08   0.29403E-09 0.60381E+00 
c  r13          0.46669E-02      20   0.66570E-08   0.14983E-08 0.19949E+00 
c  r23          0.39969E-02      20   0.63947E-08   0.12711E-08 0.19791E+00 
c  epsilon      0.10971E+02      11   0.34667E-08   0.96951E-02 0.16450E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.83901E-02 0.43204E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61359       0.0052542       0.0015073
v  Velocity[Y]            -0.57339         0.54448        0.003079      0.00087326
v  Velocity[Z]              1.5656          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4371          4.3406          4.3632
v  Pressure                -36.414          359.95           87.62           169.8
v  r11                   0.0010599        0.081892        0.013069        0.018284
v  r22                    0.001111        0.082638         0.01335        0.018644
v  r33                   0.0016352          0.1743        0.027241        0.037202
v  r12                   -0.010673        0.013589     -0.00023374     -0.00030927
v  r13                   -0.045559        0.052805      9.2794e-05       0.0010136
v  r23                    -0.04671          0.0512      3.0101e-05       0.0005744
v  epsilon                0.068602          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.984e-05       0.0099176       0.0009244       0.0017424
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2788          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71348         0.85282


 TIME FOR THE TIME STEP            10118:        0.85384E+02

===============================================================


 INSTANT    0.101190000E-01   TIME STEP NUMBER           10119
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.147843481E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.542680285E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.263939161E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.854671477E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.378200827E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      44   0.81199E-03   0.45563E-02 0.19979E+01 
c  Velocity[X]                                      0.13941E-03 
c  Velocity[Y]                                      0.12993E-03 
c  Velocity[Z]                                      0.42870E-02 
c  Pressure     0.36603E-04     134   0.93155E-02   0.25820E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.66352E-08   0.16978E-08 0.10065E+00 
c  r22          0.10850E-01      13   0.56386E-08   0.18670E-08 0.10162E+00 
c  r33          0.21857E-01      15   0.62477E-08   0.12914E-07 0.12820E+00 
c  r12          0.93845E-03      18   0.69553E-08   0.30595E-09 0.60826E+00 
c  r13          0.46669E-02      20   0.75480E-08   0.15131E-08 0.20002E+00 
c  r23          0.39969E-02      20   0.66157E-08   0.13236E-08 0.20156E+00 
c  epsilon      0.10971E+02      11   0.36481E-08   0.10869E-01 0.17546E+00 
c  TempC        0.25716E+06      16   0.15104E-04   0.85434E-02 0.43597E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61367       0.0052542       0.0015073
v  Velocity[Y]            -0.57349         0.54431        0.003079       0.0008733
v  Velocity[Z]              1.5657          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4371          4.3406          4.3632
v  Pressure                -36.382          360.09          87.689          169.91
v  r11                   0.0010599        0.081889        0.013069        0.018284
v  r22                    0.001111        0.082638         0.01335        0.018644
v  r33                   0.0016352         0.17433        0.027241        0.037202
v  r12                   -0.010671        0.013586     -0.00023374     -0.00030927
v  r13                   -0.045558        0.052802      9.2795e-05       0.0010136
v  r23                    -0.04671         0.05123      3.0102e-05       0.0005744
v  epsilon                0.068603           271.3          7.2634          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9844e-05       0.0099175       0.0009244       0.0017424
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2781          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71348         0.85282


 TIME FOR THE TIME STEP            10119:        0.83714E+02

===============================================================


 INSTANT    0.101200000E-01   TIME STEP NUMBER           10120
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100976481E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.189751606E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934918E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.379921909E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.603163800E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.217101727E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40360E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81254E-03   0.45228E-02 0.19905E+01 
c  Velocity[X]                                      0.13795E-03 
c  Velocity[Y]                                      0.12922E-03 
c  Velocity[Z]                                      0.42557E-02 
c  Pressure     0.36446E-04     133   0.92824E-02   0.25710E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.67600E-08   0.16532E-08 0.10006E+00 
c  r22          0.10850E-01      13   0.53241E-08   0.18267E-08 0.10158E+00 
c  r33          0.21857E-01      15   0.52117E-08   0.12496E-07 0.12726E+00 
c  r12          0.93845E-03      18   0.67816E-08   0.29555E-09 0.60338E+00 
c  r13          0.46669E-02      21   0.62698E-08   0.14846E-08 0.19934E+00 
c  r23          0.39969E-02      20   0.55389E-08   0.12896E-08 0.20001E+00 
c  epsilon      0.10971E+02      11   0.34602E-08   0.96842E-02 0.16327E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.84190E-02 0.43289E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61366       0.0052542       0.0015073
v  Velocity[Y]            -0.57349         0.54425        0.003079      0.00087332
v  Velocity[Z]              1.5656          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4371          4.3406          4.3632
v  Pressure                -36.427          360.13          87.718          169.94
v  r11                   0.0010599        0.081891        0.013069        0.018284
v  r22                   0.0011111        0.082639         0.01335        0.018644
v  r33                   0.0016352          0.1743        0.027241        0.037202
v  r12                   -0.010677        0.013585     -0.00023374     -0.00030927
v  r13                    -0.04556        0.052802      9.2796e-05       0.0010136
v  r23                   -0.046711        0.051217      3.0103e-05       0.0005744
v  epsilon                0.068603          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9844e-05       0.0099175       0.0009244       0.0017424
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2773          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71348         0.85282


 TIME FOR THE TIME STEP            10120:        0.83237E+02

===============================================================


 INSTANT    0.101210000E-01   TIME STEP NUMBER           10121
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.506629672E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.139239949E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.309562936E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.367092666E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.297562641E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81189E-03   0.45410E-02 0.19968E+01 
c  Velocity[X]                                      0.13859E-03 
c  Velocity[Y]                                      0.12984E-03 
c  Velocity[Z]                                      0.42726E-02 
c  Pressure     0.36656E-04     135   0.93304E-02   0.25856E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.65296E-08   0.16143E-08 0.98949E-01 
c  r22          0.10850E-01      13   0.50769E-08   0.18086E-08 0.10129E+00 
c  r33          0.21857E-01      14   0.70351E-08   0.12346E-07 0.12650E+00 
c  r12          0.93845E-03      18   0.61946E-08   0.29451E-09 0.60206E+00 
c  r13          0.46669E-02      20   0.71718E-08   0.14853E-08 0.19959E+00 
c  r23          0.39969E-02      19   0.71798E-08   0.12849E-08 0.19928E+00 
c  epsilon      0.10971E+02      11   0.32634E-08   0.96413E-02 0.16267E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.83889E-02 0.43208E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61363       0.0052542       0.0015073
v  Velocity[Y]             -0.5735         0.54432       0.0030791      0.00087333
v  Velocity[Z]              1.5656          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4371          4.3406          4.3632
v  Pressure                 -36.41             360          87.638          169.83
v  r11                   0.0010599        0.081893        0.013069        0.018284
v  r22                   0.0011111        0.082638         0.01335        0.018644
v  r33                   0.0016352         0.17427        0.027241        0.037202
v  r12                   -0.010679        0.013587     -0.00023374     -0.00030927
v  r13                   -0.045559        0.052802      9.2796e-05       0.0010136
v  r23                   -0.046712        0.051213      3.0104e-05       0.0005744
v  epsilon                0.068604          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9846e-05       0.0099174       0.0009244       0.0017424
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2766          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71349         0.85283


 TIME FOR THE TIME STEP            10121:        0.82890E+02

===============================================================


 INSTANT    0.101220000E-01   TIME STEP NUMBER           10122
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108358217E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.118730377E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.624237680E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.124761148E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.555975027E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81250E-03   0.45567E-02 0.19987E+01 
c  Velocity[X]                                      0.13998E-03 
c  Velocity[Y]                                      0.13047E-03 
c  Velocity[Z]                                      0.42863E-02 
c  Pressure     0.36707E-04     131   0.93481E-02   0.25893E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.64559E-08   0.16246E-08 0.99641E-01 
c  r22          0.10850E-01      13   0.56411E-08   0.18303E-08 0.10189E+00 
c  r33          0.21857E-01      15   0.61404E-08   0.12458E-07 0.12718E+00 
c  r12          0.93845E-03      18   0.67006E-08   0.30502E-09 0.60937E+00 
c  r13          0.46669E-02      20   0.60999E-08   0.14813E-08 0.19928E+00 
c  r23          0.39969E-02      19   0.66037E-08   0.12773E-08 0.19961E+00 
c  epsilon      0.10971E+02      11   0.31491E-08   0.98119E-02 0.16386E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84421E-02 0.43312E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61366       0.0052543       0.0015073
v  Velocity[Y]            -0.57347         0.54401        0.003079      0.00087332
v  Velocity[Z]              1.5656          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4371          4.3406          4.3632
v  Pressure                -36.439          360.01          87.654          169.84
v  r11                   0.0010599        0.081899        0.013069        0.018284
v  r22                   0.0011111        0.082639         0.01335        0.018644
v  r33                   0.0016352         0.17428        0.027241        0.037202
v  r12                   -0.010679        0.013585     -0.00023375     -0.00030927
v  r13                   -0.045557        0.052803      9.2797e-05       0.0010136
v  r23                   -0.046714        0.051235      3.0105e-05       0.0005744
v  epsilon                0.068604          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9847e-05       0.0099174       0.0009244       0.0017424
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2765         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765         0.71349         0.85283


 TIME FOR THE TIME STEP            10122:        0.82363E+02

===============================================================


 INSTANT    0.101230000E-01   TIME STEP NUMBER           10123
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111007217E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.316914523E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237719076E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.225367330E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.137666946E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21887E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81172E-03   0.45292E-02 0.19932E+01 
c  Velocity[X]                                      0.13949E-03 
c  Velocity[Y]                                      0.12876E-03 
c  Velocity[Z]                                      0.42610E-02 
c  Pressure     0.36227E-04     133   0.92257E-02   0.25554E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.62223E-08   0.16303E-08 0.99520E-01 
c  r22          0.10850E-01      13   0.52388E-08   0.18113E-08 0.10141E+00 
c  r33          0.21857E-01      14   0.69591E-08   0.12396E-07 0.12684E+00 
c  r12          0.93845E-03      18   0.54790E-08   0.30171E-09 0.60708E+00 
c  r13          0.46669E-02      20   0.58648E-08   0.14850E-08 0.19936E+00 
c  r23          0.39969E-02      19   0.72642E-08   0.12843E-08 0.19989E+00 
c  epsilon      0.10971E+02      11   0.32420E-08   0.97664E-02 0.16402E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.84393E-02 0.43336E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61367       0.0052542       0.0015073
v  Velocity[Y]            -0.57347          0.5435        0.003079      0.00087332
v  Velocity[Z]              1.5656          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4371          4.3406          4.3632
v  Pressure                -36.397          360.07           87.67          169.88
v  r11                   0.0010599        0.081902        0.013069        0.018284
v  r22                   0.0011111        0.082639         0.01335        0.018644
v  r33                   0.0016352         0.17431        0.027241        0.037202
v  r12                   -0.010677        0.013586     -0.00023375     -0.00030927
v  r13                    -0.04556        0.052802      9.2798e-05       0.0010136
v  r23                   -0.046715        0.051219      3.0105e-05       0.0005744
v  epsilon                0.068605          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9849e-05       0.0099178       0.0009244       0.0017424
v  CourantNb               0.44258             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2769          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71349         0.85282


 TIME FOR THE TIME STEP            10123:        0.82247E+02

===============================================================


 INSTANT    0.101240000E-01   TIME STEP NUMBER           10124
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.156716488E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.456876166E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.243580609E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205279440E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.575354995E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40359E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81279E-03   0.45588E-02 0.19978E+01 
c  Velocity[X]                                      0.13892E-03 
c  Velocity[Y]                                      0.12928E-03 
c  Velocity[Z]                                      0.42906E-02 
c  Pressure     0.36889E-04     138   0.93904E-02   0.26022E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.62795E-08   0.16170E-08 0.98909E-01 
c  r22          0.10850E-01      13   0.55301E-08   0.18073E-08 0.10123E+00 
c  r33          0.21857E-01      14   0.66997E-08   0.12337E-07 0.12620E+00 
c  r12          0.93845E-03      18   0.59721E-08   0.29951E-09 0.60503E+00 
c  r13          0.46669E-02      19   0.67969E-08   0.14902E-08 0.19950E+00 
c  r23          0.39969E-02      19   0.69192E-08   0.12686E-08 0.19801E+00 
c  epsilon      0.10971E+02      11   0.32148E-08   0.96363E-02 0.16390E+00 
c  TempC        0.25716E+06      16   0.15178E-04   0.84401E-02 0.43345E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61362       0.0052542       0.0015072
v  Velocity[Y]             -0.5733         0.54351        0.003079      0.00087329
v  Velocity[Z]              1.5656          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4371          4.3406          4.3632
v  Pressure                -36.423          360.07          87.669          169.88
v  r11                   0.0010599         0.08191        0.013069        0.018284
v  r22                   0.0011111        0.082639         0.01335        0.018644
v  r33                   0.0016352         0.17434        0.027241        0.037202
v  r12                   -0.010672        0.013586     -0.00023375     -0.00030927
v  r13                   -0.045559        0.052803      9.2799e-05       0.0010136
v  r23                   -0.046715        0.051203      3.0106e-05       0.0005744
v  epsilon                0.068605          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.985e-05        0.009918       0.0009244       0.0017424
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2775         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71349         0.85283


 TIME FOR THE TIME STEP            10124:        0.83349E+02

===============================================================


 INSTANT    0.101250000E-01   TIME STEP NUMBER           10125
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.264755756E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.264242071E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.449527848E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.264158765E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.617660064E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81129E-03   0.45464E-02 0.19963E+01 
c  Velocity[X]                                      0.13905E-03 
c  Velocity[Y]                                      0.12908E-03 
c  Velocity[Z]                                      0.42783E-02 
c  Pressure     0.36671E-04     133   0.93354E-02   0.25868E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59635E-08   0.16247E-08 0.99215E-01 
c  r22          0.10850E-01      13   0.54392E-08   0.18322E-08 0.10182E+00 
c  r33          0.21857E-01      14   0.66300E-08   0.12409E-07 0.12675E+00 
c  r12          0.93845E-03      18   0.59478E-08   0.29870E-09 0.60438E+00 
c  r13          0.46669E-02      19   0.67797E-08   0.14909E-08 0.20010E+00 
c  r23          0.39969E-02      19   0.72059E-08   0.12672E-08 0.19845E+00 
c  epsilon      0.10971E+02      11   0.31698E-08   0.98773E-02 0.16409E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.84149E-02 0.43329E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61366       0.0052542       0.0015072
v  Velocity[Y]            -0.57354         0.54373       0.0030791      0.00087331
v  Velocity[Z]              1.5656          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4371          4.3406          4.3632
v  Pressure                -36.415          360.05          87.663          169.87
v  r11                   0.0010599        0.081913         0.01307        0.018284
v  r22                   0.0011111        0.082635         0.01335        0.018644
v  r33                   0.0016352         0.17433        0.027241        0.037202
v  r12                   -0.010668        0.013588     -0.00023375     -0.00030927
v  r13                   -0.045559        0.052804        9.28e-05       0.0010136
v  r23                   -0.046715        0.051182      3.0106e-05       0.0005744
v  epsilon                0.068606          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.985e-05       0.0099182      0.00092441       0.0017424
v  CourantNb               0.44263             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2776          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71349         0.85283


 TIME FOR THE TIME STEP            10125:        0.80867E+02

===============================================================


 INSTANT    0.101260000E-01   TIME STEP NUMBER           10126
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.243592136E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.435745139E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.651035631E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.183986959E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.139285742E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81283E-03   0.45406E-02 0.19939E+01 
c  Velocity[X]                                      0.13936E-03 
c  Velocity[Y]                                      0.12982E-03 
c  Velocity[Z]                                      0.42714E-02 
c  Pressure     0.36231E-04     132   0.92169E-02   0.25557E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57800E-08   0.16478E-08 0.99788E-01 
c  r22          0.10850E-01      13   0.56514E-08   0.18191E-08 0.10186E+00 
c  r33          0.21857E-01      14   0.67412E-08   0.12632E-07 0.12826E+00 
c  r12          0.93845E-03      18   0.61827E-08   0.29792E-09 0.60338E+00 
c  r13          0.46669E-02      19   0.74374E-08   0.15015E-08 0.20146E+00 
c  r23          0.39969E-02      20   0.55902E-08   0.13080E-08 0.20177E+00 
c  epsilon      0.10971E+02      11   0.34083E-08   0.10260E-01 0.17210E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.83970E-02 0.43218E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61363       0.0052542       0.0015072
v  Velocity[Y]            -0.57342         0.54403       0.0030789      0.00087326
v  Velocity[Z]              1.5655          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4371          4.3406          4.3632
v  Pressure                -36.464          360.01          87.651          169.84
v  r11                   0.0010599        0.081909         0.01307        0.018284
v  r22                   0.0011111        0.082637         0.01335        0.018644
v  r33                   0.0016352         0.17429        0.027241        0.037202
v  r12                   -0.010675        0.013589     -0.00023375     -0.00030927
v  r13                   -0.045561        0.052806      9.2802e-05       0.0010136
v  r23                   -0.046715        0.051199      3.0106e-05       0.0005744
v  epsilon                0.068606          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9853e-05       0.0099183      0.00092441       0.0017424
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85283


 TIME FOR THE TIME STEP            10126:        0.79643E+02

===============================================================


 INSTANT    0.101270000E-01   TIME STEP NUMBER           10127
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.467575391E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.983186193E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.292691618E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178219113E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.305020571E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69799E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81173E-03   0.45626E-02 0.19990E+01 
c  Velocity[X]                                      0.13938E-03 
c  Velocity[Y]                                      0.12964E-03 
c  Velocity[Z]                                      0.42935E-02 
c  Pressure     0.36690E-04     133   0.93416E-02   0.25882E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.56648E-08   0.16154E-08 0.98767E-01 
c  r22          0.10850E-01      13   0.55520E-08   0.18471E-08 0.10231E+00 
c  r33          0.21857E-01      15   0.51894E-08   0.12475E-07 0.12714E+00 
c  r12          0.93845E-03      18   0.62411E-08   0.30206E-09 0.60616E+00 
c  r13          0.46669E-02      20   0.65635E-08   0.15054E-08 0.20129E+00 
c  r23          0.39969E-02      20   0.56709E-08   0.12523E-08 0.19693E+00 
c  epsilon      0.10971E+02      11   0.36381E-08   0.99577E-02 0.16585E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.84668E-02 0.43436E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61363       0.0052542       0.0015072
v  Velocity[Y]            -0.57359         0.54424       0.0030791      0.00087333
v  Velocity[Z]              1.5654          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4371          4.3406          4.3632
v  Pressure                  -36.4          360.01          87.652          169.85
v  r11                   0.0010599        0.081903         0.01307        0.018284
v  r22                   0.0011111        0.082639         0.01335        0.018644
v  r33                   0.0016352          0.1743        0.027241        0.037202
v  r12                   -0.010673        0.013588     -0.00023375     -0.00030927
v  r13                   -0.045559        0.052803      9.2803e-05       0.0010136
v  r23                   -0.046714        0.051193      3.0108e-05       0.0005744
v  epsilon                0.068607          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9856e-05       0.0099183      0.00092441       0.0017424
v  CourantNb               0.44267             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2781          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71349         0.85283


 TIME FOR THE TIME STEP            10127:        0.79383E+02

===============================================================


 INSTANT    0.101280000E-01   TIME STEP NUMBER           10128
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.212731024E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.302303558E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.526102830E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.236323053E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.296071627E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40358E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81207E-03   0.45312E-02 0.19943E+01 
c  Velocity[X]                                      0.13925E-03 
c  Velocity[Y]                                      0.12979E-03 
c  Velocity[Z]                                      0.42622E-02 
c  Pressure     0.36920E-04     133   0.93979E-02   0.26043E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.65467E-08   0.16538E-08 0.99795E-01 
c  r22          0.10850E-01      13   0.55563E-08   0.18528E-08 0.10212E+00 
c  r33          0.21857E-01      15   0.54855E-08   0.12735E-07 0.12792E+00 
c  r12          0.93845E-03      18   0.62662E-08   0.30582E-09 0.60837E+00 
c  r13          0.46669E-02      21   0.61255E-08   0.15203E-08 0.20168E+00 
c  r23          0.39969E-02      20   0.59401E-08   0.13098E-08 0.20072E+00 
c  epsilon      0.10971E+02      11   0.38468E-08   0.10134E-01 0.16520E+00 
c  TempC        0.25716E+06      16   0.15172E-04   0.84651E-02 0.43405E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61365       0.0052542       0.0015072
v  Velocity[Y]            -0.57359         0.54444       0.0030791       0.0008733
v  Velocity[Z]              1.5654          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4371          4.3406          4.3632
v  Pressure                 -36.42             360          87.641          169.83
v  r11                   0.0010599        0.081897         0.01307        0.018284
v  r22                   0.0011111        0.082641         0.01335        0.018644
v  r33                   0.0016352         0.17434        0.027241        0.037202
v  r12                   -0.010669        0.013588     -0.00023375     -0.00030927
v  r13                   -0.045558        0.052803      9.2804e-05       0.0010136
v  r23                   -0.046712        0.051184      3.0108e-05       0.0005744
v  epsilon                0.068607          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9855e-05       0.0099184      0.00092441       0.0017424
v  CourantNb               0.44257             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2784         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71349         0.85283


 TIME FOR THE TIME STEP            10128:        0.81164E+02

===============================================================


 INSTANT    0.101290000E-01   TIME STEP NUMBER           10129
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.186135932E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.202718778E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.433600132E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.533484198E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.143239299E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81216E-03   0.45301E-02 0.19942E+01 
c  Velocity[X]                                      0.13865E-03 
c  Velocity[Y]                                      0.12937E-03 
c  Velocity[Z]                                      0.42621E-02 
c  Pressure     0.36144E-04     133   0.92057E-02   0.25496E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.64407E-08   0.16341E-08 0.99352E-01 
c  r22          0.10850E-01      13   0.51745E-08   0.18226E-08 0.10184E+00 
c  r33          0.21857E-01      15   0.52528E-08   0.12506E-07 0.12740E+00 
c  r12          0.93845E-03      18   0.57598E-08   0.29420E-09 0.60440E+00 
c  r13          0.46669E-02      20   0.66420E-08   0.14834E-08 0.19995E+00 
c  r23          0.39969E-02      19   0.63547E-08   0.12889E-08 0.19985E+00 
c  epsilon      0.10971E+02      11   0.35012E-08   0.98058E-02 0.16352E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.83717E-02 0.43131E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61364       0.0052543       0.0015072
v  Velocity[Y]            -0.57364         0.54426        0.003079      0.00087327
v  Velocity[Z]              1.5655          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4371          4.3406          4.3632
v  Pressure                -36.416          360.12          87.708          169.93
v  r11                   0.0010599         0.08189         0.01307        0.018284
v  r22                   0.0011111        0.082643         0.01335        0.018644
v  r33                   0.0016352         0.17431        0.027241        0.037202
v  r12                    -0.01067        0.013589     -0.00023375     -0.00030927
v  r13                   -0.045562        0.052804      9.2805e-05       0.0010136
v  r23                    -0.04671        0.051206      3.0109e-05       0.0005744
v  epsilon                0.068608          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9855e-05       0.0099184      0.00092441       0.0017424
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2786          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71348         0.85282


 TIME FOR THE TIME STEP            10129:        0.79399E+02

===============================================================


 INSTANT    0.101300000E-01   TIME STEP NUMBER           10130
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.440411247E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.777280037E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.829146414E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.316642149E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.649456275E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69798E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      40   0.81161E-03   0.45663E-02 0.20015E+01 
c  Velocity[X]                                      0.14050E-03 
c  Velocity[Y]                                      0.12987E-03 
c  Velocity[Z]                                      0.42959E-02 
c  Pressure     0.36287E-04     133   0.92366E-02   0.25597E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.63012E-08   0.16359E-08 0.10000E+00 
c  r22          0.10850E-01      13   0.49491E-08   0.18375E-08 0.10265E+00 
c  r33          0.21857E-01      15   0.53707E-08   0.12528E-07 0.12821E+00 
c  r12          0.93845E-03      18   0.56256E-08   0.29841E-09 0.60950E+00 
c  r13          0.46669E-02      20   0.58914E-08   0.14939E-08 0.20120E+00 
c  r23          0.39969E-02      19   0.58704E-08   0.12852E-08 0.20064E+00 
c  epsilon      0.10971E+02      11   0.31643E-08   0.97195E-02 0.16504E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.84343E-02 0.43306E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61361       0.0052543       0.0015073
v  Velocity[Y]            -0.57365         0.54422        0.003079      0.00087328
v  Velocity[Z]              1.5656          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4371          4.3406          4.3632
v  Pressure                -36.456          359.98          87.658          169.84
v  r11                   0.0010598        0.081892         0.01307        0.018284
v  r22                   0.0011111        0.082644         0.01335        0.018644
v  r33                   0.0016352         0.17428        0.027241        0.037202
v  r12                    -0.01067        0.013597     -0.00023375     -0.00030927
v  r13                   -0.045559        0.052807      9.2806e-05       0.0010136
v  r23                   -0.046707        0.051196      3.0109e-05       0.0005744
v  epsilon                0.068608          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9853e-05       0.0099185      0.00092441       0.0017424
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2789          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71348         0.85282


 TIME FOR THE TIME STEP            10130:        0.81319E+02

===============================================================


 INSTANT    0.101310000E-01   TIME STEP NUMBER           10131
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.102649688E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.736650543E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.105297036E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.272090565E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.350209621E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69796E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81250E-03   0.45405E-02 0.19951E+01 
c  Velocity[X]                                      0.13962E-03 
c  Velocity[Y]                                      0.12941E-03 
c  Velocity[Z]                                      0.42715E-02 
c  Pressure     0.36254E-04     133   0.92221E-02   0.25573E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57893E-08   0.16226E-08 0.99468E-01 
c  r22          0.10850E-01      13   0.48881E-08   0.18223E-08 0.10181E+00 
c  r33          0.21857E-01      15   0.52713E-08   0.12402E-07 0.12720E+00 
c  r12          0.93845E-03      18   0.55681E-08   0.29408E-09 0.60739E+00 
c  r13          0.46669E-02      19   0.70787E-08   0.14768E-08 0.19964E+00 
c  r23          0.39970E-02      19   0.56416E-08   0.12752E-08 0.19985E+00 
c  epsilon      0.10971E+02      11   0.32391E-08   0.96577E-02 0.16268E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.84772E-02 0.43448E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61366       0.0052543       0.0015073
v  Velocity[Y]            -0.57374          0.5443       0.0030791       0.0008733
v  Velocity[Z]              1.5656          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4371          4.3406          4.3632
v  Pressure                 -36.39          360.03          87.648          169.86
v  r11                   0.0010598        0.081886         0.01307        0.018284
v  r22                   0.0011111        0.082645         0.01335        0.018644
v  r33                   0.0016352          0.1743        0.027241        0.037202
v  r12                   -0.010668        0.013603     -0.00023375     -0.00030927
v  r13                   -0.045558        0.052807      9.2806e-05       0.0010136
v  r23                   -0.046704        0.051191      3.0111e-05      0.00057441
v  epsilon                0.068609          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9853e-05       0.0099185      0.00092441       0.0017424
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2792          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8792         0.71349         0.85283


 TIME FOR THE TIME STEP            10131:        0.80641E+02

===============================================================


 INSTANT    0.101320000E-01   TIME STEP NUMBER           10132
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.236286771E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.284736211E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.244535693E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294730298E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.333915127E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69795E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81283E-03   0.45102E-02 0.19878E+01 
c  Velocity[X]                                      0.13856E-03 
c  Velocity[Y]                                      0.12935E-03 
c  Velocity[Z]                                      0.42423E-02 
c  Pressure     0.36808E-04     133   0.93760E-02   0.25964E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60451E-08   0.16623E-08 0.10062E+00 
c  r22          0.10850E-01      13   0.51622E-08   0.18611E-08 0.10243E+00 
c  r33          0.21857E-01      15   0.65419E-08   0.12788E-07 0.12886E+00 
c  r12          0.93845E-03      18   0.57151E-08   0.30417E-09 0.61006E+00 
c  r13          0.46669E-02      20   0.66651E-08   0.15204E-08 0.20092E+00 
c  r23          0.39970E-02      19   0.57039E-08   0.13204E-08 0.20364E+00 
c  epsilon      0.10971E+02      11   0.34282E-08   0.10364E-01 0.17185E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.83911E-02 0.43269E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61363       0.0052542       0.0015072
v  Velocity[Y]            -0.57362         0.54437       0.0030791      0.00087332
v  Velocity[Z]              1.5658          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4371          4.3406          4.3632
v  Pressure                -36.432          360.05          87.678          169.88
v  r11                   0.0010598        0.081885         0.01307        0.018284
v  r22                   0.0011111        0.082647         0.01335        0.018644
v  r33                   0.0016352         0.17431        0.027242        0.037202
v  r12                   -0.010665        0.013598     -0.00023375     -0.00030927
v  r13                   -0.045561        0.052808      9.2807e-05       0.0010136
v  r23                   -0.046701        0.051211      3.0111e-05      0.00057441
v  epsilon                0.068609          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9852e-05       0.0099185      0.00092441       0.0017424
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2784          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71348         0.85282


 TIME FOR THE TIME STEP            10132:        0.75661E+02

===============================================================


 INSTANT    0.101330000E-01   TIME STEP NUMBER           10133
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.244777083E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.137420960E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.109797783E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.765516514E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.272624976E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81122E-03   0.45449E-02 0.19980E+01 
c  Velocity[X]                                      0.13889E-03 
c  Velocity[Y]                                      0.12988E-03 
c  Velocity[Z]                                      0.42762E-02 
c  Pressure     0.36436E-04     132   0.92742E-02   0.25702E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.61226E-08   0.16104E-08 0.99339E-01 
c  r22          0.10850E-01      13   0.54791E-08   0.18328E-08 0.10216E+00 
c  r33          0.21857E-01      14   0.66386E-08   0.12446E-07 0.12788E+00 
c  r12          0.93845E-03      18   0.65357E-08   0.29807E-09 0.60750E+00 
c  r13          0.46669E-02      19   0.63018E-08   0.15013E-08 0.20059E+00 
c  r23          0.39970E-02      19   0.52704E-08   0.12691E-08 0.20027E+00 
c  epsilon      0.10971E+02      11   0.34431E-08   0.96777E-02 0.16330E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.84583E-02 0.43411E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61359       0.0052543       0.0015072
v  Velocity[Y]            -0.57366         0.54445       0.0030791      0.00087331
v  Velocity[Z]              1.5657          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4371          4.3406          4.3632
v  Pressure                -36.398          360.04          87.652          169.87
v  r11                   0.0010598        0.081883         0.01307        0.018284
v  r22                   0.0011111        0.082648         0.01335        0.018644
v  r33                   0.0016352          0.1743        0.027242        0.037202
v  r12                   -0.010667        0.013592     -0.00023375     -0.00030927
v  r13                    -0.04556        0.052809      9.2808e-05       0.0010136
v  r23                   -0.046699        0.051206      3.0112e-05      0.00057441
v  epsilon                 0.06861          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9851e-05       0.0099185      0.00092442       0.0017424
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2782          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71348         0.85282


 TIME FOR THE TIME STEP            10133:        0.78699E+02

===============================================================


 INSTANT    0.101340000E-01   TIME STEP NUMBER           10134
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140686497E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.196538912E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.320998620E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.142762399E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.328984582E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81282E-03   0.45514E-02 0.19960E+01 
c  Velocity[X]                                      0.13922E-03 
c  Velocity[Y]                                      0.12933E-03 
c  Velocity[Z]                                      0.42829E-02 
c  Pressure     0.36303E-04     132   0.92460E-02   0.25607E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.55682E-08   0.16244E-08 0.99828E-01 
c  r22          0.10850E-01      13   0.55090E-08   0.18171E-08 0.10190E+00 
c  r33          0.21857E-01      15   0.53711E-08   0.12435E-07 0.12800E+00 
c  r12          0.93845E-03      18   0.70831E-08   0.29999E-09 0.60870E+00 
c  r13          0.46669E-02      19   0.64084E-08   0.14864E-08 0.20095E+00 
c  r23          0.39970E-02      19   0.56999E-08   0.12823E-08 0.20188E+00 
c  epsilon      0.10971E+02      11   0.36247E-08   0.95895E-02 0.16307E+00 
c  TempC        0.25716E+06      16   0.15127E-04   0.84823E-02 0.43382E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63365          0.6136       0.0052543       0.0015072
v  Velocity[Y]            -0.57363         0.54423        0.003079      0.00087327
v  Velocity[Z]              1.5654          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4371          4.3406          4.3632
v  Pressure                -36.454          359.98          87.645          169.83
v  r11                   0.0010598        0.081886         0.01307        0.018284
v  r22                   0.0011111        0.082649         0.01335        0.018644
v  r33                   0.0016352         0.17428        0.027242        0.037202
v  r12                   -0.010672        0.013586     -0.00023375     -0.00030927
v  r13                   -0.045559        0.052811      9.2809e-05       0.0010136
v  r23                   -0.046697        0.051184      3.0112e-05      0.00057441
v  epsilon                 0.06861          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.985e-05       0.0099185      0.00092442       0.0017424
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2781          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71348         0.85283


 TIME FOR THE TIME STEP            10134:        0.77166E+02

===============================================================


 INSTANT    0.101350000E-01   TIME STEP NUMBER           10135
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.438861964E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.247220198E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.384679221E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.137712988E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.107769827E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81219E-03   0.45407E-02 0.19966E+01 
c  Velocity[X]                                      0.13859E-03 
c  Velocity[Y]                                      0.12940E-03 
c  Velocity[Z]                                      0.42727E-02 
c  Pressure     0.36777E-04     134   0.93669E-02   0.25942E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.53969E-08   0.16283E-08 0.99560E-01 
c  r22          0.10850E-01      13   0.51762E-08   0.18194E-08 0.10138E+00 
c  r33          0.21857E-01      15   0.70042E-08   0.12425E-07 0.12744E+00 
c  r12          0.93845E-03      18   0.61467E-08   0.29692E-09 0.60256E+00 
c  r13          0.46669E-02      19   0.58622E-08   0.14771E-08 0.19922E+00 
c  r23          0.39970E-02      19   0.56919E-08   0.12738E-08 0.19987E+00 
c  epsilon      0.10971E+02      11   0.35811E-08   0.98627E-02 0.16453E+00 
c  TempC        0.25716E+06      16   0.15103E-04   0.84254E-02 0.43343E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61362       0.0052543       0.0015072
v  Velocity[Y]            -0.57369         0.54422       0.0030791      0.00087331
v  Velocity[Z]              1.5654          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4371          4.3406          4.3632
v  Pressure                -36.408          360.06          87.679          169.89
v  r11                   0.0010598        0.081884         0.01307        0.018284
v  r22                   0.0011111        0.082644         0.01335        0.018644
v  r33                   0.0016352         0.17429        0.027242        0.037202
v  r12                   -0.010671        0.013587     -0.00023375     -0.00030927
v  r13                   -0.045561        0.052811      9.2809e-05       0.0010136
v  r23                   -0.046695        0.051176      3.0113e-05      0.00057441
v  epsilon                0.068611          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9853e-05       0.0099184      0.00092442       0.0017424
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2776          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71348         0.85282


 TIME FOR THE TIME STEP            10135:        0.79726E+02

===============================================================


 INSTANT    0.101360000E-01   TIME STEP NUMBER           10136
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.196713991E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153394838E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934913E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153729465E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.904046510E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.308306953E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81227E-03   0.45418E-02 0.19959E+01 
c  Velocity[X]                                      0.13977E-03 
c  Velocity[Y]                                      0.12974E-03 
c  Velocity[Z]                                      0.42723E-02 
c  Pressure     0.36354E-04     133   0.92527E-02   0.25645E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54818E-08   0.16417E-08 0.99910E-01 
c  r22          0.10850E-01      13   0.47897E-08   0.18291E-08 0.10178E+00 
c  r33          0.21857E-01      14   0.67006E-08   0.12531E-07 0.12759E+00 
c  r12          0.93845E-03      18   0.54766E-08   0.29219E-09 0.60135E+00 
c  r13          0.46669E-02      18   0.71870E-08   0.14948E-08 0.19996E+00 
c  r23          0.39970E-02      19   0.57691E-08   0.12850E-08 0.19971E+00 
c  epsilon      0.10971E+02      11   0.31806E-08   0.10063E-01 0.16733E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.84014E-02 0.43310E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61356       0.0052542       0.0015072
v  Velocity[Y]            -0.57357         0.54415       0.0030791       0.0008733
v  Velocity[Z]              1.5655          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4371          4.3406          4.3632
v  Pressure                -36.445          360.05          87.684          169.88
v  r11                   0.0010598        0.081886         0.01307        0.018284
v  r22                   0.0011111        0.082646         0.01335        0.018644
v  r33                   0.0016352         0.17432        0.027242        0.037202
v  r12                    -0.01067        0.013584     -0.00023375     -0.00030927
v  r13                   -0.045558        0.052812      9.2811e-05       0.0010136
v  r23                   -0.046694        0.051203      3.0113e-05      0.00057441
v  epsilon                0.068611          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9853e-05       0.0099184      0.00092442       0.0017424
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2768          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71349         0.85283


 TIME FOR THE TIME STEP            10136:        0.77667E+02

===============================================================


 INSTANT    0.101370000E-01   TIME STEP NUMBER           10137
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153320373E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.378434595E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.451589098E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.262017628E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168510442E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81229E-03   0.45332E-02 0.19925E+01 
c  Velocity[X]                                      0.13891E-03 
c  Velocity[Y]                                      0.12930E-03 
c  Velocity[Z]                                      0.42650E-02 
c  Pressure     0.36255E-04     132   0.92275E-02   0.25574E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.53683E-08   0.16166E-08 0.99277E-01 
c  r22          0.10850E-01      13   0.45149E-08   0.18424E-08 0.10183E+00 
c  r33          0.21857E-01      15   0.53145E-08   0.12496E-07 0.12740E+00 
c  r12          0.93845E-03      18   0.51154E-08   0.29671E-09 0.60433E+00 
c  r13          0.46669E-02      19   0.53914E-08   0.14929E-08 0.19998E+00 
c  r23          0.39970E-02      19   0.53662E-08   0.12636E-08 0.19878E+00 
c  epsilon      0.10971E+02      11   0.34304E-08   0.99532E-02 0.16503E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.84679E-02 0.43389E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61359       0.0052543       0.0015072
v  Velocity[Y]            -0.57371         0.54426       0.0030792      0.00087332
v  Velocity[Z]              1.5656          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4371          4.3406          4.3632
v  Pressure                -36.424          360.05          87.659          169.87
v  r11                   0.0010598        0.081886         0.01307        0.018284
v  r22                   0.0011111        0.082648         0.01335        0.018644
v  r33                   0.0016352          0.1743        0.027242        0.037202
v  r12                   -0.010671        0.013582     -0.00023375     -0.00030927
v  r13                   -0.045559        0.052811      9.2811e-05       0.0010136
v  r23                   -0.046693        0.051203      3.0114e-05      0.00057441
v  epsilon                0.068612          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9853e-05       0.0099183      0.00092442       0.0017424
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2766          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71349         0.85282


 TIME FOR THE TIME STEP            10137:        0.77977E+02

===============================================================


 INSTANT    0.101380000E-01   TIME STEP NUMBER           10138
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.926520364E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186647786E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.493085597E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107254013E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.652225954E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81192E-03   0.45251E-02 0.19927E+01 
c  Velocity[X]                                      0.13901E-03 
c  Velocity[Y]                                      0.13021E-03 
c  Velocity[Z]                                      0.42558E-02 
c  Pressure     0.36300E-04     131   0.92405E-02   0.25606E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54832E-08   0.16815E-08 0.10093E+00 
c  r22          0.10850E-01      12   0.64294E-08   0.18730E-08 0.10258E+00 
c  r33          0.21857E-01      14   0.68621E-08   0.12943E-07 0.12921E+00 
c  r12          0.93845E-03      18   0.49806E-08   0.30129E-09 0.60860E+00 
c  r13          0.46669E-02      19   0.56044E-08   0.15312E-08 0.20180E+00 
c  r23          0.39970E-02      18   0.65570E-08   0.13221E-08 0.20289E+00 
c  epsilon      0.10971E+02      11   0.34826E-08   0.10827E-01 0.17607E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.83776E-02 0.43166E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378          0.6136       0.0052543       0.0015073
v  Velocity[Y]             -0.5737         0.54439       0.0030791      0.00087332
v  Velocity[Z]              1.5656          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4371          4.3406          4.3632
v  Pressure                -36.463             360          87.642          169.84
v  r11                   0.0010598        0.081886         0.01307        0.018284
v  r22                   0.0011111        0.082651         0.01335        0.018644
v  r33                   0.0016352         0.17426        0.027242        0.037202
v  r12                   -0.010671        0.013585     -0.00023375     -0.00030927
v  r13                   -0.045561        0.052815      9.2813e-05       0.0010136
v  r23                   -0.046693         0.05119      3.0115e-05      0.00057441
v  epsilon                0.068613          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9855e-05       0.0099183      0.00092442       0.0017424
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017897           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85282


 TIME FOR THE TIME STEP            10138:        0.77449E+02

===============================================================


 INSTANT    0.101390000E-01   TIME STEP NUMBER           10139
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249407828E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.917685601E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.358223978E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.328107072E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.162951847E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81208E-03   0.45618E-02 0.20020E+01 
c  Velocity[X]                                      0.13948E-03 
c  Velocity[Y]                                      0.12903E-03 
c  Velocity[Z]                                      0.42933E-02 
c  Pressure     0.36574E-04     131   0.93073E-02   0.25800E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.56069E-08   0.16493E-08 0.99809E-01 
c  r22          0.10850E-01      13   0.45431E-08   0.18226E-08 0.10177E+00 
c  r33          0.21857E-01      15   0.57352E-08   0.12512E-07 0.12756E+00 
c  r12          0.93845E-03      18   0.51589E-08   0.29686E-09 0.60312E+00 
c  r13          0.46669E-02      19   0.54491E-08   0.14845E-08 0.19975E+00 
c  r23          0.39970E-02      18   0.66707E-08   0.12846E-08 0.19942E+00 
c  epsilon      0.10971E+02      11   0.34520E-08   0.98286E-02 0.16495E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.84521E-02 0.43362E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338         0.61357       0.0052543       0.0015073
v  Velocity[Y]            -0.57369         0.54418       0.0030791      0.00087332
v  Velocity[Z]              1.5653          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4371          4.3406          4.3632
v  Pressure                -36.448          360.08          87.678           169.9
v  r11                   0.0010598        0.081889         0.01307        0.018284
v  r22                   0.0011111        0.082652         0.01335        0.018644
v  r33                   0.0016352         0.17428        0.027242        0.037202
v  r12                   -0.010668        0.013586     -0.00023375     -0.00030927
v  r13                   -0.045559        0.052813      9.2814e-05       0.0010136
v  r23                   -0.046693        0.051213      3.0116e-05      0.00057441
v  epsilon                0.068613          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9857e-05       0.0099183      0.00092442       0.0017424
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2782         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71349         0.85283


 TIME FOR THE TIME STEP            10139:        0.77738E+02

===============================================================


 INSTANT    0.101400000E-01   TIME STEP NUMBER           10140
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.101270766E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.303678940E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.275233967E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.292099199E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.253340132E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81189E-03   0.45665E-02 0.19990E+01 
c  Velocity[X]                                      0.13948E-03 
c  Velocity[Y]                                      0.12895E-03 
c  Velocity[Z]                                      0.42981E-02 
c  Pressure     0.36639E-04     132   0.93311E-02   0.25846E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.58442E-08   0.16445E-08 0.10025E+00 
c  r22          0.10850E-01      13   0.51988E-08   0.18442E-08 0.10212E+00 
c  r33          0.21857E-01      15   0.61515E-08   0.12588E-07 0.12798E+00 
c  r12          0.93846E-03      18   0.56805E-08   0.30592E-09 0.61062E+00 
c  r13          0.46669E-02      19   0.71472E-08   0.15098E-08 0.20111E+00 
c  r23          0.39970E-02      18   0.66962E-08   0.12815E-08 0.20031E+00 
c  epsilon      0.10971E+02      11   0.32694E-08   0.99691E-02 0.16490E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.85089E-02 0.43547E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338          0.6136       0.0052543       0.0015073
v  Velocity[Y]            -0.57363         0.54423       0.0030791       0.0008733
v  Velocity[Z]              1.5654          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4371          4.3406          4.3632
v  Pressure                -36.515          360.01          87.645          169.84
v  r11                   0.0010598        0.081891         0.01307        0.018284
v  r22                   0.0011111        0.082654         0.01335        0.018644
v  r33                   0.0016352         0.17432        0.027242        0.037202
v  r12                   -0.010668        0.013582     -0.00023375     -0.00030927
v  r13                   -0.045558        0.052814      9.2816e-05       0.0010136
v  r23                   -0.046694        0.051193      3.0116e-05      0.00057441
v  epsilon                0.068614          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.986e-05        0.009918      0.00092442       0.0017424
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017897           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85283


 TIME FOR THE TIME STEP            10140:        0.78680E+02

===============================================================


 INSTANT    0.101410000E-01   TIME STEP NUMBER           10141
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.338606022E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.165072345E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.620938528E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.348028885E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.354539487E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81160E-03   0.45354E-02 0.19932E+01 
c  Velocity[X]                                      0.13894E-03 
c  Velocity[Y]                                      0.12979E-03 
c  Velocity[Z]                                      0.42667E-02 
c  Pressure     0.36248E-04     131   0.92290E-02   0.25571E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.61374E-08   0.16266E-08 0.99953E-01 
c  r22          0.10850E-01      13   0.47224E-08   0.17971E-08 0.10154E+00 
c  r33          0.21857E-01      15   0.56147E-08   0.12361E-07 0.12746E+00 
c  r12          0.93846E-03      18   0.56134E-08   0.30068E-09 0.60945E+00 
c  r13          0.46669E-02      19   0.71125E-08   0.14911E-08 0.20036E+00 
c  r23          0.39970E-02      19   0.61801E-08   0.12831E-08 0.20073E+00 
c  epsilon      0.10971E+02      10   0.54042E-08   0.95151E-02 0.16200E+00 
c  TempC        0.25716E+06      16   0.15104E-04   0.83735E-02 0.43218E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369         0.61357       0.0052544       0.0015073
v  Velocity[Y]            -0.57363         0.54426       0.0030792      0.00087338
v  Velocity[Z]              1.5653          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4371          4.3406          4.3632
v  Pressure                -36.472             360          87.636          169.83
v  r11                   0.0010598         0.08189         0.01307        0.018284
v  r22                   0.0011111        0.082656         0.01335        0.018644
v  r33                   0.0016352          0.1743        0.027242        0.037202
v  r12                   -0.010672        0.013584     -0.00023375     -0.00030927
v  r13                   -0.045562        0.052814      9.2816e-05       0.0010136
v  r23                   -0.046697        0.051188      3.0117e-05      0.00057441
v  epsilon                0.068614          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9863e-05       0.0099176      0.00092443       0.0017424
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017897           5.278         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85283


 TIME FOR THE TIME STEP            10141:        0.79524E+02

===============================================================


 INSTANT    0.101420000E-01   TIME STEP NUMBER           10142
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.299180641E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.144811660E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.305833467E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.213421178E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208766446E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81193E-03   0.45431E-02 0.19952E+01 
c  Velocity[X]                                      0.13844E-03 
c  Velocity[Y]                                      0.13035E-03 
c  Velocity[Z]                                      0.42743E-02 
c  Pressure     0.36243E-04     131   0.92272E-02   0.25566E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52451E-08   0.16423E-08 0.99487E-01 
c  r22          0.10850E-01      12   0.65101E-08   0.18218E-08 0.10162E+00 
c  r33          0.21857E-01      14   0.70356E-08   0.12561E-07 0.12749E+00 
c  r12          0.93846E-03      17   0.65725E-08   0.29455E-09 0.60319E+00 
c  r13          0.46670E-02      19   0.58815E-08   0.14739E-08 0.19991E+00 
c  r23          0.39970E-02      18   0.65717E-08   0.12813E-08 0.19977E+00 
c  epsilon      0.10971E+02      11   0.32647E-08   0.10157E-01 0.16831E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.83887E-02 0.43215E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63366         0.61355       0.0052544       0.0015073
v  Velocity[Y]            -0.57352         0.54434       0.0030791      0.00087331
v  Velocity[Z]              1.5653          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4371          4.3406          4.3632
v  Pressure                 -36.49          359.96          87.604           169.8
v  r11                   0.0010598         0.08189         0.01307        0.018284
v  r22                   0.0011111        0.082656         0.01335        0.018644
v  r33                   0.0016352         0.17427        0.027242        0.037202
v  r12                    -0.01067        0.013586     -0.00023375     -0.00030927
v  r13                   -0.045559        0.052815      9.2817e-05       0.0010136
v  r23                     -0.0467        0.051214      3.0118e-05      0.00057441
v  epsilon                0.068615          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9868e-05       0.0099176      0.00092443       0.0017425
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2784          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71349         0.85282


 TIME FOR THE TIME STEP            10142:        0.79034E+02

===============================================================


 INSTANT    0.101430000E-01   TIME STEP NUMBER           10143
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.112478027E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.351876061E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934900E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.138177762E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.368565622E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.723971573E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      40   0.81209E-03   0.45654E-02 0.19995E+01 
c  Velocity[X]                                      0.14036E-03 
c  Velocity[Y]                                      0.12927E-03 
c  Velocity[Z]                                      0.42958E-02 
c  Pressure     0.36476E-04     133   0.92822E-02   0.25731E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52527E-08   0.16196E-08 0.99620E-01 
c  r22          0.10850E-01      12   0.65260E-08   0.18217E-08 0.10134E+00 
c  r33          0.21857E-01      14   0.68968E-08   0.12410E-07 0.12706E+00 
c  r12          0.93846E-03      18   0.49286E-08   0.29329E-09 0.60181E+00 
c  r13          0.46670E-02      19   0.55452E-08   0.14864E-08 0.19950E+00 
c  r23          0.39970E-02      18   0.62893E-08   0.12592E-08 0.19835E+00 
c  epsilon      0.10971E+02      11   0.33211E-08   0.98236E-02 0.16528E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.85309E-02 0.43549E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161987


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61359       0.0052544       0.0015073
v  Velocity[Y]            -0.57369          0.5442       0.0030791      0.00087334
v  Velocity[Z]              1.5655          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4371          4.3406          4.3632
v  Pressure                -36.406          360.08          87.689          169.91
v  r11                   0.0010598        0.081889         0.01307        0.018284
v  r22                   0.0011111        0.082652         0.01335        0.018644
v  r33                   0.0016352         0.17429        0.027242        0.037202
v  r12                   -0.010666        0.013584     -0.00023375     -0.00030927
v  r13                   -0.045558        0.052816      9.2819e-05       0.0010136
v  r23                   -0.046703          0.0512      3.0119e-05      0.00057441
v  epsilon                0.068615          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9871e-05       0.0099176      0.00092443       0.0017425
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2781          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71349         0.85283


 TIME FOR THE TIME STEP            10143:        0.80740E+02

===============================================================


 INSTANT    0.101440000E-01   TIME STEP NUMBER           10144
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.206481985E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.228810039E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.296416089E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.204669937E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.528896245E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81319E-03   0.45260E-02 0.19920E+01 
c  Velocity[X]                                      0.13835E-03 
c  Velocity[Y]                                      0.12950E-03 
c  Velocity[Z]                                      0.42581E-02 
c  Pressure     0.36504E-04     132   0.92866E-02   0.25751E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52287E-08   0.16458E-08 0.99642E-01 
c  r22          0.10850E-01      13   0.47034E-08   0.18303E-08 0.10197E+00 
c  r33          0.21857E-01      14   0.70472E-08   0.12558E-07 0.12756E+00 
c  r12          0.93846E-03      17   0.69446E-08   0.30251E-09 0.60900E+00 
c  r13          0.46670E-02      19   0.64623E-08   0.14946E-08 0.20076E+00 
c  r23          0.39970E-02      19   0.59589E-08   0.12936E-08 0.19975E+00 
c  epsilon      0.10971E+02      11   0.33708E-08   0.97848E-02 0.16409E+00 
c  TempC        0.25716E+06      16   0.15165E-04   0.84069E-02 0.43254E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161984


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61359       0.0052544       0.0015073
v  Velocity[Y]            -0.57367         0.54411       0.0030791      0.00087335
v  Velocity[Z]              1.5655          5.4371          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4371          4.3406          4.3632
v  Pressure                -36.426          360.06           87.67          169.88
v  r11                   0.0010598        0.081885         0.01307        0.018284
v  r22                   0.0011111        0.082655         0.01335        0.018644
v  r33                   0.0016352         0.17432        0.027242        0.037202
v  r12                   -0.010664         0.01359     -0.00023375     -0.00030927
v  r13                   -0.045561        0.052817       9.282e-05       0.0010136
v  r23                   -0.046705        0.051185       3.012e-05      0.00057441
v  epsilon                0.068616          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9872e-05       0.0099177      0.00092443       0.0017425
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2787         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71349         0.85282


 TIME FOR THE TIME STEP            10144:        0.78368E+02

===============================================================


 INSTANT    0.101450000E-01   TIME STEP NUMBER           10145
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.202619336E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.200517900E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.702666165E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.189974829E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.146316246E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      44   0.81078E-03   0.45678E-02 0.20020E+01 
c  Velocity[X]                                      0.13919E-03 
c  Velocity[Y]                                      0.12965E-03 
c  Velocity[Z]                                      0.42989E-02 
c  Pressure     0.36655E-04     132   0.93338E-02   0.25856E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54172E-08   0.16587E-08 0.10003E+00 
c  r22          0.10850E-01      13   0.54791E-08   0.18466E-08 0.10189E+00 
c  r33          0.21857E-01      15   0.55111E-08   0.12757E-07 0.12807E+00 
c  r12          0.93846E-03      18   0.63933E-08   0.30207E-09 0.60401E+00 
c  r13          0.46670E-02      19   0.65403E-08   0.14988E-08 0.20027E+00 
c  r23          0.39970E-02      19   0.71968E-08   0.12988E-08 0.20019E+00 
c  epsilon      0.10971E+02      11   0.33430E-08   0.10550E-01 0.17325E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.84324E-02 0.43294E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63371         0.61356       0.0052544       0.0015073
v  Velocity[Y]             -0.5738         0.54414       0.0030792      0.00087334
v  Velocity[Z]              1.5657          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4372          4.3406          4.3632
v  Pressure                 -36.43          360.03          87.654          169.86
v  r11                   0.0010598        0.081879         0.01307        0.018284
v  r22                   0.0011111        0.082656         0.01335        0.018644
v  r33                   0.0016352          0.1743        0.027242        0.037202
v  r12                   -0.010662        0.013595     -0.00023375     -0.00030927
v  r13                    -0.04556        0.052816      9.2821e-05       0.0010136
v  r23                   -0.046706        0.051184      3.0121e-05      0.00057441
v  epsilon                0.068616          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9875e-05       0.0099179      0.00092443       0.0017425
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2786          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71349         0.85283


 TIME FOR THE TIME STEP            10145:        0.81104E+02

===============================================================


 INSTANT    0.101460000E-01   TIME STEP NUMBER           10146
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158272179E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.773135811E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.422188090E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.133191773E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.192559911E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81257E-03   0.45546E-02 0.19962E+01 
c  Velocity[X]                                      0.13984E-03 
c  Velocity[Y]                                      0.12963E-03 
c  Velocity[Z]                                      0.42851E-02 
c  Pressure     0.36020E-04     131   0.91808E-02   0.25409E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.52970E-08   0.16291E-08 0.99897E-01 
c  r22          0.10850E-01      13   0.55216E-08   0.18102E-08 0.10185E+00 
c  r33          0.21857E-01      15   0.56002E-08   0.12430E-07 0.12776E+00 
c  r12          0.93846E-03      18   0.68992E-08   0.29852E-09 0.60564E+00 
c  r13          0.46670E-02      19   0.66160E-08   0.14776E-08 0.20063E+00 
c  r23          0.39970E-02      19   0.73243E-08   0.12777E-08 0.20000E+00 
c  epsilon      0.10971E+02      11   0.32922E-08   0.96613E-02 0.16334E+00 
c  TempC        0.25716E+06      16   0.15127E-04   0.84483E-02 0.43400E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63371         0.61362       0.0052544       0.0015073
v  Velocity[Y]            -0.57359         0.54429       0.0030791      0.00087331
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4372          4.3406          4.3632
v  Pressure                 -36.47          360.01          87.654          169.85
v  r11                   0.0010598        0.081878         0.01307        0.018284
v  r22                   0.0011111        0.082659         0.01335        0.018644
v  r33                   0.0016351         0.17428        0.027242        0.037202
v  r12                   -0.010667         0.01359     -0.00023375     -0.00030927
v  r13                   -0.045559        0.052819      9.2822e-05       0.0010136
v  r23                   -0.046707        0.051214      3.0122e-05      0.00057441
v  epsilon                0.068617          271.18          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9878e-05        0.009918      0.00092443       0.0017425
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2787          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71348         0.85282


 TIME FOR THE TIME STEP            10146:        0.81514E+02

===============================================================


 INSTANT    0.101470000E-01   TIME STEP NUMBER           10147
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.553146942E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.105483789E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.224383238E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115538534E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.572819097E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81260E-03   0.45318E-02 0.19916E+01 
c  Velocity[X]                                      0.13843E-03 
c  Velocity[Y]                                      0.12941E-03 
c  Velocity[Z]                                      0.42640E-02 
c  Pressure     0.36490E-04     133   0.92877E-02   0.25740E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.51360E-08   0.16506E-08 0.99934E-01 
c  r22          0.10850E-01      13   0.54046E-08   0.18357E-08 0.10201E+00 
c  r33          0.21857E-01      15   0.70835E-08   0.12621E-07 0.12792E+00 
c  r12          0.93846E-03      18   0.64420E-08   0.29616E-09 0.60499E+00 
c  r13          0.46670E-02      20   0.61558E-08   0.14886E-08 0.20045E+00 
c  r23          0.39970E-02      19   0.71425E-08   0.12943E-08 0.20071E+00 
c  epsilon      0.10971E+02      11   0.33251E-08   0.10001E-01 0.16587E+00 
c  TempC        0.25716E+06      16   0.15094E-04   0.83939E-02 0.43224E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61362       0.0052544       0.0015073
v  Velocity[Y]            -0.57371         0.54443       0.0030792      0.00087334
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4372          4.3406          4.3632
v  Pressure                -36.456          360.07          87.679          169.89
v  r11                   0.0010598        0.081875         0.01307        0.018284
v  r22                   0.0011111         0.08266         0.01335        0.018644
v  r33                   0.0016351         0.17429        0.027242        0.037202
v  r12                   -0.010665        0.013584     -0.00023375     -0.00030927
v  r13                   -0.045561        0.052818      9.2823e-05       0.0010136
v  r23                   -0.046708        0.051209      3.0123e-05      0.00057441
v  epsilon                0.068617          271.19          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9884e-05       0.0099181      0.00092443       0.0017425
v  CourantNb               0.44263             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2783          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71349         0.85283


 TIME FOR THE TIME STEP            10147:        0.81555E+02

===============================================================


 INSTANT    0.101480000E-01   TIME STEP NUMBER           10148
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.290860278E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.288573212E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.170269509E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.241436082E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.646756273E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      45   0.81116E-03   0.45396E-02 0.19951E+01 
c  Velocity[X]                                      0.13866E-03 
c  Velocity[Y]                                      0.12938E-03 
c  Velocity[Z]                                      0.42716E-02 
c  Pressure     0.36519E-04     135   0.92989E-02   0.25761E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.51270E-08   0.16414E-08 0.99892E-01 
c  r22          0.10850E-01      13   0.54756E-08   0.18279E-08 0.10203E+00 
c  r33          0.21857E-01      15   0.59192E-08   0.12570E-07 0.12805E+00 
c  r12          0.93846E-03      18   0.53910E-08   0.29713E-09 0.60443E+00 
c  r13          0.46670E-02      20   0.60232E-08   0.14926E-08 0.20091E+00 
c  r23          0.39970E-02      20   0.54992E-08   0.12914E-08 0.20055E+00 
c  epsilon      0.10971E+02      11   0.32397E-08   0.99881E-02 0.16677E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.84625E-02 0.43460E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61356       0.0052545       0.0015073
v  Velocity[Y]            -0.57358         0.54409       0.0030791       0.0008733
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4372          4.3406          4.3632
v  Pressure                -36.489          360.02          87.662          169.85
v  r11                   0.0010598        0.081878         0.01307        0.018284
v  r22                   0.0011111        0.082661         0.01335        0.018644
v  r33                   0.0016351         0.17432        0.027242        0.037202
v  r12                   -0.010663        0.013586     -0.00023376     -0.00030927
v  r13                   -0.045559        0.052819      9.2824e-05       0.0010136
v  r23                   -0.046707        0.051205      3.0124e-05      0.00057441
v  epsilon                0.068618          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9889e-05       0.0099181      0.00092444       0.0017425
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2774         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71349         0.85283


 TIME FOR THE TIME STEP            10148:        0.82282E+02

===============================================================


 INSTANT    0.101490000E-01   TIME STEP NUMBER           10149
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116198122E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.404830660E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.414093246E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.828829926E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.274651051E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81234E-03   0.45260E-02 0.19921E+01 
c  Velocity[X]                                      0.13868E-03 
c  Velocity[Y]                                      0.12964E-03 
c  Velocity[Z]                                      0.42577E-02 
c  Pressure     0.36257E-04     133   0.92329E-02   0.25576E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.51847E-08   0.16138E-08 0.99437E-01 
c  r22          0.10850E-01      13   0.55252E-08   0.18210E-08 0.10129E+00 
c  r33          0.21857E-01      15   0.54995E-08   0.12359E-07 0.12704E+00 
c  r12          0.93846E-03      18   0.55445E-08   0.29599E-09 0.60671E+00 
c  r13          0.46670E-02      19   0.73035E-08   0.14907E-08 0.19943E+00 
c  r23          0.39970E-02      20   0.57567E-08   0.12664E-08 0.19941E+00 
c  epsilon      0.10971E+02      11   0.33765E-08   0.96854E-02 0.16383E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84313E-02 0.43318E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61363       0.0052544       0.0015073
v  Velocity[Y]            -0.57352         0.54411       0.0030792      0.00087336
v  Velocity[Z]              1.5653          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4372          4.3406          4.3632
v  Pressure                -36.407          360.08          87.676          169.89
v  r11                   0.0010598        0.081883         0.01307        0.018284
v  r22                   0.0011111        0.082662         0.01335        0.018644
v  r33                   0.0016351         0.17431        0.027242        0.037202
v  r12                    -0.01066         0.01358     -0.00023376     -0.00030927
v  r13                    -0.04556        0.052819      9.2825e-05       0.0010136
v  r23                   -0.046707        0.051225      3.0124e-05      0.00057441
v  epsilon                0.068619          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9895e-05       0.0099182      0.00092444       0.0017425
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2768          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71349         0.85283


 TIME FOR THE TIME STEP            10149:        0.80798E+02

===============================================================


 INSTANT    0.101500000E-01   TIME STEP NUMBER           10150
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.395232039E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.338806860E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.553466048E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.574263131E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.311079826E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81212E-03   0.45432E-02 0.19975E+01 
c  Velocity[X]                                      0.13940E-03 
c  Velocity[Y]                                      0.13004E-03 
c  Velocity[Z]                                      0.42738E-02 
c  Pressure     0.36747E-04     132   0.93575E-02   0.25922E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.53146E-08   0.16315E-08 0.99982E-01 
c  r22          0.10850E-01      13   0.52555E-08   0.18066E-08 0.10126E+00 
c  r33          0.21857E-01      15   0.61331E-08   0.12477E-07 0.12770E+00 
c  r12          0.93846E-03      18   0.55868E-08   0.29015E-09 0.60101E+00 
c  r13          0.46670E-02      20   0.65440E-08   0.14829E-08 0.19963E+00 
c  r23          0.39970E-02      20   0.57336E-08   0.12721E-08 0.20021E+00 
c  epsilon      0.10971E+02      11   0.34486E-08   0.98817E-02 0.16505E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.83430E-02 0.43047E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61362       0.0052544       0.0015073
v  Velocity[Y]            -0.57344         0.54425       0.0030792      0.00087331
v  Velocity[Z]              1.5657          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4372          4.3406          4.3632
v  Pressure                -36.444          359.96          87.614           169.8
v  r11                   0.0010597        0.081887         0.01307        0.018284
v  r22                   0.0011111        0.082665         0.01335        0.018644
v  r33                   0.0016351         0.17428        0.027242        0.037202
v  r12                   -0.010659        0.013581     -0.00023376     -0.00030927
v  r13                   -0.045562        0.052822      9.2825e-05       0.0010136
v  r23                   -0.046707        0.051214      3.0125e-05      0.00057441
v  epsilon                0.068619           271.2          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc               5.99e-05       0.0099182      0.00092444       0.0017425
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2766          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71348         0.85282


 TIME FOR THE TIME STEP            10150:        0.77301E+02

===============================================================


 INSTANT    0.101510000E-01   TIME STEP NUMBER           10151
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.245444754E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191920822E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934906E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.137838468E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.147046738E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.196094125E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81195E-03   0.45346E-02 0.19961E+01 
c  Velocity[X]                                      0.13957E-03 
c  Velocity[Y]                                      0.12955E-03 
c  Velocity[Z]                                      0.42655E-02 
c  Pressure     0.36523E-04     131   0.92929E-02   0.25763E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.57285E-08   0.16518E-08 0.10008E+00 
c  r22          0.10850E-01      13   0.52205E-08   0.18174E-08 0.10104E+00 
c  r33          0.21857E-01      15   0.61185E-08   0.12595E-07 0.12770E+00 
c  r12          0.93846E-03      18   0.65478E-08   0.30135E-09 0.60569E+00 
c  r13          0.46670E-02      20   0.63292E-08   0.14939E-08 0.19937E+00 
c  r23          0.39970E-02      20   0.56818E-08   0.13011E-08 0.20161E+00 
c  epsilon      0.10971E+02      11   0.34713E-08   0.10151E-01 0.16960E+00 
c  TempC        0.25716E+06      16   0.15118E-04   0.84537E-02 0.43417E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61358       0.0052546       0.0015073
v  Velocity[Y]            -0.57358          0.5441       0.0030793      0.00087336
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4372          4.3406          4.3632
v  Pressure                -36.431          360.09          87.684          169.91
v  r11                   0.0010597        0.081891         0.01307        0.018284
v  r22                   0.0011111        0.082661         0.01335        0.018644
v  r33                   0.0016351         0.17429        0.027242        0.037202
v  r12                   -0.010658        0.013577     -0.00023376     -0.00030927
v  r13                    -0.04556        0.052819      9.2826e-05       0.0010136
v  r23                   -0.046707        0.051213      3.0126e-05      0.00057441
v  epsilon                 0.06862          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9906e-05       0.0099182      0.00092444       0.0017425
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2773         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71349         0.85283


 TIME FOR THE TIME STEP            10151:        0.81231E+02

===============================================================


 INSTANT    0.101520000E-01   TIME STEP NUMBER           10152
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.355562800E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.325191078E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.984056820E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.104466386E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.192401500E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81269E-03   0.45366E-02 0.19942E+01 
c  Velocity[X]                                      0.13900E-03 
c  Velocity[Y]                                      0.12924E-03 
c  Velocity[Z]                                      0.42683E-02 
c  Pressure     0.36243E-04     132   0.92279E-02   0.25566E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60258E-08   0.16330E-08 0.10011E+00 
c  r22          0.10850E-01      13   0.50554E-08   0.18438E-08 0.10187E+00 
c  r33          0.21857E-01      15   0.67942E-08   0.12492E-07 0.12746E+00 
c  r12          0.93846E-03      18   0.69046E-08   0.30328E-09 0.60907E+00 
c  r13          0.46670E-02      19   0.72877E-08   0.15117E-08 0.20028E+00 
c  r23          0.39970E-02      20   0.67335E-08   0.12837E-08 0.20056E+00 
c  epsilon      0.10971E+02      11   0.33863E-08   0.98445E-02 0.16523E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.84751E-02 0.43452E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63368         0.61363       0.0052545       0.0015073
v  Velocity[Y]            -0.57358         0.54418       0.0030792       0.0008733
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4372          4.3406          4.3632
v  Pressure                -36.471          359.99          87.628          169.82
v  r11                   0.0010597        0.081898         0.01307        0.018284
v  r22                   0.0011111        0.082661         0.01335        0.018644
v  r33                   0.0016351         0.17432        0.027242        0.037202
v  r12                   -0.010657        0.013572     -0.00023376     -0.00030927
v  r13                   -0.045558        0.052819      9.2827e-05       0.0010136
v  r23                   -0.046707        0.051234      3.0127e-05      0.00057441
v  epsilon                 0.06862          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.991e-05       0.0099182      0.00092444       0.0017425
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2782          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71349         0.85283


 TIME FOR THE TIME STEP            10152:        0.79737E+02

===============================================================


 INSTANT    0.101530000E-01   TIME STEP NUMBER           10153
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.375583058E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.202105090E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.681937265E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.991736885E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186155329E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81197E-03   0.45082E-02 0.19875E+01 
c  Velocity[X]                                      0.13824E-03 
c  Velocity[Y]                                      0.12886E-03 
c  Velocity[Z]                                      0.42411E-02 
c  Pressure     0.36579E-04     133   0.93060E-02   0.25802E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.58367E-08   0.16142E-08 0.99502E-01 
c  r22          0.10850E-01      13   0.52356E-08   0.18045E-08 0.10099E+00 
c  r33          0.21857E-01      15   0.65265E-08   0.12367E-07 0.12701E+00 
c  r12          0.93846E-03      18   0.64862E-08   0.29431E-09 0.60369E+00 
c  r13          0.46670E-02      19   0.75010E-08   0.14852E-08 0.19970E+00 
c  r23          0.39970E-02      20   0.59867E-08   0.12734E-08 0.20013E+00 
c  epsilon      0.10971E+02      11   0.33507E-08   0.96038E-02 0.16169E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.84108E-02 0.43266E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61362       0.0052544       0.0015073
v  Velocity[Y]            -0.57371         0.54435       0.0030792      0.00087329
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4372          4.3406          4.3632
v  Pressure                -36.449          360.02          87.646          169.86
v  r11                   0.0010597        0.081905         0.01307        0.018284
v  r22                   0.0011111        0.082661         0.01335        0.018644
v  r33                   0.0016351          0.1743        0.027242        0.037202
v  r12                   -0.010655        0.013574     -0.00023376     -0.00030927
v  r13                   -0.045563        0.052819      9.2829e-05       0.0010136
v  r23                   -0.046706        0.051228      3.0127e-05      0.00057442
v  epsilon                0.068621          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9911e-05       0.0099181      0.00092444       0.0017425
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2784         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71349         0.85283


 TIME FOR THE TIME STEP            10153:        0.80567E+02

===============================================================


 INSTANT    0.101540000E-01   TIME STEP NUMBER           10154
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.121985800E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.367027949E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934908E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.303877943E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.274459357E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.175295106E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81226E-03   0.45689E-02 0.20014E+01 
c  Velocity[X]                                      0.13914E-03 
c  Velocity[Y]                                      0.12980E-03 
c  Velocity[Z]                                      0.43000E-02 
c  Pressure     0.36790E-04     133   0.93662E-02   0.25951E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.60217E-08   0.16198E-08 0.99863E-01 
c  r22          0.10850E-01      13   0.58892E-08   0.18143E-08 0.10117E+00 
c  r33          0.21857E-01      15   0.61076E-08   0.12428E-07 0.12743E+00 
c  r12          0.93846E-03      18   0.70632E-08   0.29524E-09 0.60685E+00 
c  r13          0.46670E-02      20   0.61236E-08   0.14889E-08 0.19916E+00 
c  r23          0.39970E-02      20   0.58339E-08   0.12746E-08 0.20032E+00 
c  epsilon      0.10971E+02      11   0.33001E-08   0.98676E-02 0.16536E+00 
c  TempC        0.25716E+06      16   0.15164E-04   0.84793E-02 0.43402E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61358       0.0052544       0.0015073
v  Velocity[Y]            -0.57355          0.5443       0.0030792      0.00087331
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4372          4.3406          4.3632
v  Pressure                -36.499          360.02          87.674          169.86
v  r11                   0.0010597         0.08191         0.01307        0.018284
v  r22                   0.0011111        0.082662         0.01335        0.018644
v  r33                   0.0016351         0.17428        0.027242        0.037202
v  r12                   -0.010654        0.013569     -0.00023376     -0.00030927
v  r13                    -0.04556         0.05282       9.283e-05       0.0010136
v  r23                   -0.046705        0.051216      3.0128e-05      0.00057442
v  epsilon                0.068621          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05        0.009918      0.00092444       0.0017425
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2784         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71349         0.85282


 TIME FOR THE TIME STEP            10154:        0.79404E+02

===============================================================


 INSTANT    0.101550000E-01   TIME STEP NUMBER           10155
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.308715382E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.183824921E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.693313790E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.102959586E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.295707620E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81226E-03   0.45594E-02 0.19990E+01 
c  Velocity[X]                                      0.13911E-03 
c  Velocity[Y]                                      0.12962E-03 
c  Velocity[Z]                                      0.42907E-02 
c  Pressure     0.36442E-04     133   0.92799E-02   0.25706E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.54371E-08   0.16446E-08 0.10036E+00 
c  r22          0.10850E-01      13   0.54446E-08   0.18291E-08 0.10138E+00 
c  r33          0.21857E-01      15   0.60401E-08   0.12480E-07 0.12764E+00 
c  r12          0.93846E-03      18   0.64583E-08   0.30320E-09 0.60874E+00 
c  r13          0.46670E-02      20   0.60449E-08   0.14911E-08 0.19954E+00 
c  r23          0.39970E-02      20   0.61761E-08   0.12744E-08 0.20095E+00 
c  epsilon      0.10970E+02      11   0.34278E-08   0.97645E-02 0.16480E+00 
c  TempC        0.25716E+06      16   0.15112E-04   0.84645E-02 0.43450E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61364       0.0052544       0.0015073
v  Velocity[Y]            -0.57363         0.54419       0.0030792      0.00087332
v  Velocity[Z]              1.5654          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4372          4.3406          4.3632
v  Pressure                 -36.43          360.08          87.688           169.9
v  r11                   0.0010597        0.081915         0.01307        0.018284
v  r22                   0.0011111        0.082662         0.01335        0.018644
v  r33                   0.0016351          0.1743        0.027242        0.037202
v  r12                   -0.010652        0.013568     -0.00023376     -0.00030927
v  r13                   -0.045559        0.052818      9.2831e-05       0.0010136
v  r23                   -0.046705        0.051241      3.0128e-05      0.00057442
v  epsilon                0.068622          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099179      0.00092444       0.0017425
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2782          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71348         0.85282


 TIME FOR THE TIME STEP            10155:        0.78412E+02

===============================================================


 INSTANT    0.101560000E-01   TIME STEP NUMBER           10156
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125402083E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.173645898E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.107174530E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319670365E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.939277843E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      40   0.81203E-03   0.45202E-02 0.19912E+01 
c  Velocity[X]                                      0.13871E-03 
c  Velocity[Y]                                      0.12916E-03 
c  Velocity[Z]                                      0.42523E-02 
c  Pressure     0.36321E-04     132   0.92494E-02   0.25621E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.53421E-08   0.16742E-08 0.10112E+00 
c  r22          0.10850E-01      13   0.53299E-08   0.18417E-08 0.10204E+00 
c  r33          0.21857E-01      15   0.55729E-08   0.12672E-07 0.12854E+00 
c  r12          0.93846E-03      18   0.56735E-08   0.29722E-09 0.60683E+00 
c  r13          0.46670E-02      19   0.70287E-08   0.14866E-08 0.20036E+00 
c  r23          0.39970E-02      20   0.61259E-08   0.12952E-08 0.20237E+00 
c  epsilon      0.10970E+02      11   0.36286E-08   0.10004E-01 0.16648E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.83800E-02 0.43247E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63371         0.61362       0.0052544       0.0015073
v  Velocity[Y]            -0.57361         0.54427       0.0030792      0.00087331
v  Velocity[Z]              1.5654          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4372          4.3406          4.3632
v  Pressure                -36.487          360.03          87.639          169.85
v  r11                   0.0010597        0.081925         0.01307        0.018284
v  r22                    0.001111        0.082661         0.01335        0.018644
v  r33                   0.0016351         0.17432        0.027242        0.037202
v  r12                   -0.010655        0.013562     -0.00023376     -0.00030928
v  r13                   -0.045562        0.052817      9.2831e-05       0.0010136
v  r23                   -0.046704        0.051234      3.0128e-05      0.00057442
v  epsilon                0.068623          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9917e-05       0.0099178      0.00092445       0.0017425
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2778          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71348         0.85282


 TIME FOR THE TIME STEP            10156:        0.80324E+02

===============================================================


 INSTANT    0.101570000E-01   TIME STEP NUMBER           10157
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105953048E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.233427735E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.222659400E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.175392620E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115454221E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81093E-03   0.45495E-02 0.19964E+01 
c  Velocity[X]                                      0.13909E-03 
c  Velocity[Y]                                      0.12999E-03 
c  Velocity[Z]                                      0.42804E-02 
c  Pressure     0.36539E-04     133   0.92969E-02   0.25774E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.59801E-08   0.16532E-08 0.10031E+00 
c  r22          0.10850E-01      13   0.51583E-08   0.18415E-08 0.10176E+00 
c  r33          0.21857E-01      15   0.61549E-08   0.12661E-07 0.12817E+00 
c  r12          0.93846E-03      18   0.56724E-08   0.30535E-09 0.61010E+00 
c  r13          0.46670E-02      20   0.59776E-08   0.15140E-08 0.20106E+00 
c  r23          0.39970E-02      20   0.58193E-08   0.12989E-08 0.20164E+00 
c  epsilon      0.10970E+02      11   0.36674E-08   0.99088E-02 0.16467E+00 
c  TempC        0.25716E+06      16   0.15107E-04   0.84084E-02 0.43224E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63372         0.61355       0.0052544       0.0015073
v  Velocity[Y]            -0.57371         0.54434       0.0030793      0.00087333
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4372          4.3406          4.3632
v  Pressure                -36.403          359.99          87.621          169.82
v  r11                   0.0010597        0.081929         0.01307        0.018284
v  r22                    0.001111        0.082658         0.01335        0.018644
v  r33                   0.0016351          0.1743        0.027242        0.037202
v  r12                   -0.010655        0.013558     -0.00023376     -0.00030928
v  r13                   -0.045561        0.052815      9.2833e-05       0.0010136
v  r23                   -0.046704        0.051228      3.0129e-05      0.00057442
v  epsilon                0.068623          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099178      0.00092445       0.0017425
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2778          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71349         0.85283


 TIME FOR THE TIME STEP            10157:        0.80254E+02

===============================================================


 INSTANT    0.101580000E-01   TIME STEP NUMBER           10158
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.279520769E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.883143644E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.649188506E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.808753050E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.256319441E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81190E-03   0.45359E-02 0.19941E+01 
c  Velocity[X]                                      0.13928E-03 
c  Velocity[Y]                                      0.12982E-03 
c  Velocity[Z]                                      0.42668E-02 
c  Pressure     0.36630E-04     133   0.93256E-02   0.25838E-01 0.00000E+00 
c  r11          0.10583E-01      13   0.58456E-08   0.16523E-08 0.10078E+00 
c  r22          0.10850E-01      13   0.51390E-08   0.18243E-08 0.10161E+00 
c  r33          0.21857E-01      15   0.63162E-08   0.12623E-07 0.12864E+00 
c  r12          0.93846E-03      18   0.53314E-08   0.29586E-09 0.60786E+00 
c  r13          0.46670E-02      20   0.60620E-08   0.15078E-08 0.20138E+00 
c  r23          0.39970E-02      20   0.65388E-08   0.13047E-08 0.20288E+00 
c  epsilon      0.10970E+02      11   0.34914E-08   0.10138E-01 0.17123E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.84611E-02 0.43357E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61362       0.0052545       0.0015074
v  Velocity[Y]             -0.5737         0.54417       0.0030791      0.00087326
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4372          4.3406          4.3632
v  Pressure                -36.471          360.03          87.677          169.87
v  r11                   0.0010597        0.081931         0.01307        0.018284
v  r22                    0.001111        0.082658         0.01335        0.018644
v  r33                   0.0016351         0.17428        0.027242        0.037202
v  r12                   -0.010653        0.013561     -0.00023376     -0.00030928
v  r13                   -0.045559        0.052817      9.2834e-05       0.0010136
v  r23                   -0.046704        0.051216       3.013e-05      0.00057442
v  epsilon                0.068624          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05       0.0099179      0.00092445       0.0017425
v  CourantNb               0.44256             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2771         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71349         0.85283


 TIME FOR THE TIME STEP            10158:        0.79400E+02

===============================================================


 INSTANT    0.101590000E-01   TIME STEP NUMBER           10159
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.119096435E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.620590049E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.710795007E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935016E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166448124E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157342338E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81272E-03   0.45251E-02 0.19920E+01 
c  Velocity[X]                                      0.13811E-03 
c  Velocity[Y]                                      0.12860E-03 
c  Velocity[Z]                                      0.42584E-02 
c  Pressure     0.36250E-04     133   0.92305E-02   0.25570E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56089E-08   0.16363E-08 0.99772E-01 
c  r22          0.10850E-01      13   0.52448E-08   0.18433E-08 0.10148E+00 
c  r33          0.21857E-01      15   0.64521E-08   0.12537E-07 0.12724E+00 
c  r12          0.93846E-03      18   0.58503E-08   0.29891E-09 0.60590E+00 
c  r13          0.46670E-02      20   0.58416E-08   0.15036E-08 0.19992E+00 
c  r23          0.39970E-02      20   0.61118E-08   0.12822E-08 0.19960E+00 
c  epsilon      0.10970E+02      11   0.33725E-08   0.10065E-01 0.16614E+00 
c  TempC        0.25716E+06      16   0.15112E-04   0.84355E-02 0.43319E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61363       0.0052546       0.0015074
v  Velocity[Y]             -0.5737         0.54425       0.0030792      0.00087329
v  Velocity[Z]              1.5656          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4372          4.3406          4.3632
v  Pressure                -36.419             360          87.637          169.84
v  r11                   0.0010597        0.081932         0.01307        0.018284
v  r22                    0.001111        0.082653         0.01335        0.018644
v  r33                   0.0016351         0.17429        0.027242        0.037202
v  r12                   -0.010654        0.013562     -0.00023376     -0.00030928
v  r13                   -0.045562        0.052815      9.2835e-05       0.0010136
v  r23                   -0.046705        0.051239      3.0131e-05      0.00057442
v  epsilon                0.068625          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099179      0.00092445       0.0017425
v  CourantNb               0.44276             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2771          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71349         0.85283


 TIME FOR THE TIME STEP            10159:        0.78523E+02

===============================================================


 INSTANT    0.101600000E-01   TIME STEP NUMBER           10160
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.362711419E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.494886707E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.313250889E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282763364E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.517920572E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81174E-03   0.45281E-02 0.19940E+01 
c  Velocity[X]                                      0.13958E-03 
c  Velocity[Y]                                      0.12866E-03 
c  Velocity[Z]                                      0.42599E-02 
c  Pressure     0.36638E-04     131   0.93313E-02   0.25845E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60013E-08   0.16239E-08 0.99579E-01 
c  r22          0.10850E-01      13   0.58439E-08   0.18579E-08 0.10171E+00 
c  r33          0.21857E-01      15   0.63055E-08   0.12604E-07 0.12758E+00 
c  r12          0.93846E-03      18   0.56298E-08   0.30200E-09 0.60910E+00 
c  r13          0.46670E-02      19   0.68426E-08   0.15393E-08 0.20098E+00 
c  r23          0.39970E-02      20   0.55008E-08   0.12892E-08 0.20091E+00 
c  epsilon      0.10970E+02      11   0.33623E-08   0.10077E-01 0.16654E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.83859E-02 0.43229E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63372         0.61355       0.0052545       0.0015074
v  Velocity[Y]             -0.5737         0.54442       0.0030792      0.00087327
v  Velocity[Z]              1.5654          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4372          4.3406          4.3632
v  Pressure                -36.495             360          87.638          169.83
v  r11                   0.0010597        0.081932         0.01307        0.018284
v  r22                    0.001111        0.082654         0.01335        0.018644
v  r33                   0.0016351         0.17432        0.027242        0.037202
v  r12                   -0.010655        0.013562     -0.00023376     -0.00030928
v  r13                    -0.04556        0.052816      9.2836e-05       0.0010136
v  r23                   -0.046705        0.051223      3.0131e-05      0.00057442
v  epsilon                0.068625          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099179      0.00092445       0.0017425
v  CourantNb               0.44264             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2776         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71349         0.85283


 TIME FOR THE TIME STEP            10160:        0.79959E+02

===============================================================


 INSTANT    0.101610000E-01   TIME STEP NUMBER           10161
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199016440E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.263546575E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.415210987E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.583800876E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.161686587E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      43   0.81241E-03   0.45550E-02 0.19982E+01 
c  Velocity[X]                                      0.13969E-03 
c  Velocity[Y]                                      0.12919E-03 
c  Velocity[Z]                                      0.42861E-02 
c  Pressure     0.36482E-04     132   0.92870E-02   0.25735E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58296E-08   0.16009E-08 0.99715E-01 
c  r22          0.10850E-01      13   0.60094E-08   0.17656E-08 0.10087E+00 
c  r33          0.21857E-01      15   0.55247E-08   0.12046E-07 0.12629E+00 
c  r12          0.93846E-03      18   0.56526E-08   0.29549E-09 0.60387E+00 
c  r13          0.46670E-02      19   0.64899E-08   0.14473E-08 0.19807E+00 
c  r23          0.39970E-02      19   0.71461E-08   0.12478E-08 0.19950E+00 
c  epsilon      0.10970E+02      11   0.33387E-08   0.90946E-02 0.15866E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.84265E-02 0.43361E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61363       0.0052546       0.0015074
v  Velocity[Y]            -0.57387         0.54412       0.0030792      0.00087328
v  Velocity[Z]              1.5654          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4372          4.3406          4.3632
v  Pressure                 -36.46           360.1          87.695          169.92
v  r11                   0.0010597        0.081929         0.01307        0.018284
v  r22                    0.001111        0.082656         0.01335        0.018644
v  r33                   0.0016351         0.17431        0.027242        0.037202
v  r12                   -0.010655        0.013559     -0.00023376     -0.00030928
v  r13                    -0.04556        0.052815      9.2837e-05       0.0010136
v  r23                   -0.046707        0.051205      3.0132e-05      0.00057442
v  epsilon                0.068626          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05        0.009918      0.00092445       0.0017425
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb             0.0017894           5.278          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71348         0.85282


 TIME FOR THE TIME STEP            10161:        0.78478E+02

===============================================================


 INSTANT    0.101620000E-01   TIME STEP NUMBER           10162
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.372097069E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.382241866E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.336609838E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111763874E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136728718E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81286E-03   0.45336E-02 0.19931E+01 
c  Velocity[X]                                      0.13842E-03 
c  Velocity[Y]                                      0.12942E-03 
c  Velocity[Z]                                      0.42658E-02 
c  Pressure     0.36283E-04     133   0.92368E-02   0.25593E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60413E-08   0.16203E-08 0.99537E-01 
c  r22          0.10850E-01      13   0.55295E-08   0.18100E-08 0.10135E+00 
c  r33          0.21857E-01      15   0.74864E-08   0.12438E-07 0.12699E+00 
c  r12          0.93846E-03      18   0.54981E-08   0.29395E-09 0.60068E+00 
c  r13          0.46670E-02      19   0.71401E-08   0.14692E-08 0.19871E+00 
c  r23          0.39970E-02      19   0.68489E-08   0.12748E-08 0.20049E+00 
c  epsilon      0.10970E+02      11   0.35051E-08   0.10018E-01 0.16608E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84234E-02 0.43270E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61361       0.0052546       0.0015074
v  Velocity[Y]            -0.57367         0.54417       0.0030792      0.00087327
v  Velocity[Z]              1.5652          5.4372          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4372          4.3406          4.3632
v  Pressure                -36.452          360.01           87.65          169.85
v  r11                   0.0010597        0.081924         0.01307        0.018284
v  r22                    0.001111        0.082658         0.01335        0.018644
v  r33                    0.001635         0.17428        0.027242        0.037202
v  r12                   -0.010656        0.013558     -0.00023376     -0.00030928
v  r13                   -0.045563        0.052816      9.2838e-05       0.0010136
v  r23                   -0.046707        0.051216      3.0132e-05      0.00057442
v  epsilon                0.068627          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9919e-05       0.0099179      0.00092445       0.0017425
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb             0.0017893          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71348         0.85282


 TIME FOR THE TIME STEP            10162:        0.80137E+02

===============================================================


 INSTANT    0.101630000E-01   TIME STEP NUMBER           10163
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.721539887E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.257631964E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.392065229E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119173054E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.560805056E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      40   0.81208E-03   0.45550E-02 0.19993E+01 
c  Velocity[X]                                      0.13956E-03 
c  Velocity[Y]                                      0.12984E-03 
c  Velocity[Z]                                      0.42856E-02 
c  Pressure     0.36846E-04     133   0.93717E-02   0.25991E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59468E-08   0.16448E-08 0.10015E+00 
c  r22          0.10850E-01      13   0.56690E-08   0.18560E-08 0.10224E+00 
c  r33          0.21857E-01      15   0.62495E-08   0.12719E-07 0.12821E+00 
c  r12          0.93846E-03      18   0.56974E-08   0.30123E-09 0.60817E+00 
c  r13          0.46670E-02      19   0.67800E-08   0.15211E-08 0.20167E+00 
c  r23          0.39970E-02      19   0.64176E-08   0.12901E-08 0.20067E+00 
c  epsilon      0.10970E+02      11   0.35248E-08   0.10261E-01 0.16751E+00 
c  TempC        0.25716E+06      16   0.15110E-04   0.84455E-02 0.43334E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161988


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61358       0.0052546       0.0015075
v  Velocity[Y]            -0.57383         0.54429       0.0030792      0.00087329
v  Velocity[Z]              1.5653          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4372          4.3406          4.3632
v  Pressure                -36.441          360.09          87.713          169.92
v  r11                   0.0010597        0.081919         0.01307        0.018284
v  r22                    0.001111        0.082659         0.01335        0.018644
v  r33                    0.001635          0.1743        0.027242        0.037202
v  r12                   -0.010656        0.013556     -0.00023376     -0.00030928
v  r13                   -0.045561        0.052813      9.2839e-05       0.0010136
v  r23                   -0.046708        0.051213      3.0132e-05      0.00057442
v  epsilon                0.068627          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9919e-05       0.0099177      0.00092445       0.0017425
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017893          5.2779          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71349         0.85283


 TIME FOR THE TIME STEP            10163:        0.80026E+02

===============================================================


 INSTANT    0.101640000E-01   TIME STEP NUMBER           10164
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.266299142E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.252479958E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.300783849E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935024E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.144734308E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.537946813E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81227E-03   0.45591E-02 0.20005E+01 
c  Velocity[X]                                      0.13942E-03 
c  Velocity[Y]                                      0.12956E-03 
c  Velocity[Z]                                      0.42901E-02 
c  Pressure     0.36786E-04     132   0.93647E-02   0.25949E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60788E-08   0.16521E-08 0.10072E+00 
c  r22          0.10851E-01      13   0.57395E-08   0.18248E-08 0.10192E+00 
c  r33          0.21857E-01      15   0.74105E-08   0.12534E-07 0.12808E+00 
c  r12          0.93846E-03      18   0.55924E-08   0.30513E-09 0.61710E+00 
c  r13          0.46670E-02      20   0.58083E-08   0.15051E-08 0.20104E+00 
c  r23          0.39970E-02      19   0.56643E-08   0.12797E-08 0.19998E+00 
c  epsilon      0.10970E+02      11   0.36411E-08   0.98568E-02 0.16520E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.84644E-02 0.43405E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61358       0.0052546       0.0015075
v  Velocity[Y]            -0.57373         0.54446       0.0030792      0.00087326
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4372          4.3406          4.3632
v  Pressure                -36.457             360          87.644          169.84
v  r11                   0.0010597        0.081922         0.01307        0.018284
v  r22                    0.001111         0.08266         0.01335        0.018644
v  r33                    0.001635         0.17433        0.027242        0.037202
v  r12                   -0.010657        0.013564     -0.00023376     -0.00030928
v  r13                   -0.045559        0.052813       9.284e-05       0.0010136
v  r23                   -0.046709        0.051202      3.0134e-05      0.00057442
v  epsilon                0.068628          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099177      0.00092446       0.0017425
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017893          5.2775         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71349         0.85283


 TIME FOR THE TIME STEP            10164:        0.80250E+02

===============================================================


 INSTANT    0.101650000E-01   TIME STEP NUMBER           10165
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153787682E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229335730E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.264141679E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.479020114E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.415320584E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81118E-03   0.45238E-02 0.19897E+01 
c  Velocity[X]                                      0.13814E-03 
c  Velocity[Y]                                      0.12830E-03 
c  Velocity[Z]                                      0.42574E-02 
c  Pressure     0.36078E-04     132   0.91864E-02   0.25448E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60217E-08   0.16511E-08 0.10063E+00 
c  r22          0.10851E-01      13   0.55602E-08   0.18469E-08 0.10180E+00 
c  r33          0.21857E-01      15   0.61244E-08   0.12688E-07 0.12840E+00 
c  r12          0.93846E-03      18   0.53918E-08   0.30205E-09 0.61194E+00 
c  r13          0.46670E-02      20   0.58547E-08   0.15099E-08 0.20076E+00 
c  r23          0.39970E-02      19   0.61317E-08   0.12965E-08 0.20240E+00 
c  epsilon      0.10970E+02      11   0.33968E-08   0.10556E-01 0.17420E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.83659E-02 0.43159E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61359       0.0052546       0.0015074
v  Velocity[Y]            -0.57367         0.54427       0.0030793      0.00087329
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4372          4.3406          4.3632
v  Pressure                -36.391          360.05          87.633          169.86
v  r11                   0.0010597        0.081919         0.01307        0.018284
v  r22                    0.001111        0.082657         0.01335        0.018644
v  r33                    0.001635         0.17431        0.027242        0.037202
v  r12                   -0.010658        0.013567     -0.00023376     -0.00030928
v  r13                   -0.045564        0.052815      9.2841e-05       0.0010136
v  r23                    -0.04671        0.051223      3.0135e-05      0.00057442
v  epsilon                0.068628          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9919e-05       0.0099176      0.00092446       0.0017425
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017893          5.2779          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71348         0.85282


 TIME FOR THE TIME STEP            10165:        0.82554E+02

===============================================================


 INSTANT    0.101660000E-01   TIME STEP NUMBER           10166
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.590703924E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.846006924E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.353361691E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227517126E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.391986724E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      44   0.81279E-03   0.45593E-02 0.19989E+01 
c  Velocity[X]                                      0.13969E-03 
c  Velocity[Y]                                      0.12928E-03 
c  Velocity[Z]                                      0.42904E-02 
c  Pressure     0.36781E-04     132   0.93706E-02   0.25946E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.63807E-08   0.16190E-08 0.99545E-01 
c  r22          0.10851E-01      13   0.52630E-08   0.18558E-08 0.10196E+00 
c  r33          0.21857E-01      15   0.65580E-08   0.12540E-07 0.12742E+00 
c  r12          0.93846E-03      18   0.56516E-08   0.29722E-09 0.60403E+00 
c  r13          0.46670E-02      19   0.62746E-08   0.15116E-08 0.20027E+00 
c  r23          0.39970E-02      19   0.64272E-08   0.12716E-08 0.19914E+00 
c  epsilon      0.10970E+02      11   0.33736E-08   0.10140E-01 0.16771E+00 
c  TempC        0.25716E+06      16   0.15125E-04   0.84203E-02 0.43296E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61354       0.0052546       0.0015074
v  Velocity[Y]            -0.57355         0.54422       0.0030792      0.00087325
v  Velocity[Z]              1.5657          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4372          4.3406          4.3632
v  Pressure                -36.476          360.02          87.656          169.84
v  r11                   0.0010597        0.081921         0.01307        0.018284
v  r22                    0.001111        0.082658         0.01335        0.018644
v  r33                    0.001635         0.17428        0.027242        0.037202
v  r12                   -0.010659        0.013576     -0.00023376     -0.00030928
v  r13                    -0.04556        0.052816      9.2842e-05       0.0010136
v  r23                   -0.046711         0.05121      3.0135e-05      0.00057442
v  epsilon                0.068629           271.2          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099177      0.00092446       0.0017425
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017893          5.2776          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71348         0.85282


 TIME FOR THE TIME STEP            10166:        0.79887E+02

===============================================================


 INSTANT    0.101670000E-01   TIME STEP NUMBER           10167
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.260870776E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.315955126E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.155125134E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.471860884E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.743742738E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      42   0.81158E-03   0.45667E-02 0.20010E+01 
c  Velocity[X]                                      0.13867E-03 
c  Velocity[Y]                                      0.12914E-03 
c  Velocity[Z]                                      0.42989E-02 
c  Pressure     0.36484E-04     132   0.92898E-02   0.25736E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.61568E-08   0.16252E-08 0.99925E-01 
c  r22          0.10851E-01      13   0.51276E-08   0.17958E-08 0.10137E+00 
c  r33          0.21857E-01      15   0.59822E-08   0.12310E-07 0.12736E+00 
c  r12          0.93846E-03      18   0.55180E-08   0.29341E-09 0.60547E+00 
c  r13          0.46670E-02      19   0.67744E-08   0.14727E-08 0.20001E+00 
c  r23          0.39970E-02      19   0.54260E-08   0.12691E-08 0.19998E+00 
c  epsilon      0.10970E+02      11   0.35021E-08   0.95992E-02 0.16300E+00 
c  TempC        0.25716E+06      16   0.15101E-04   0.84669E-02 0.43383E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63365         0.61358       0.0052546       0.0015074
v  Velocity[Y]            -0.57355         0.54435       0.0030793      0.00087328
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4372          4.3406          4.3632
v  Pressure                  -36.4          360.04          87.664          169.87
v  r11                   0.0010597         0.08192         0.01307        0.018284
v  r22                    0.001111        0.082659         0.01335        0.018644
v  r33                    0.001635          0.1743        0.027242        0.037202
v  r12                    -0.01066        0.013576     -0.00023376     -0.00030928
v  r13                    -0.04556        0.052814      9.2842e-05       0.0010136
v  r23                   -0.046712        0.051198      3.0136e-05      0.00057442
v  epsilon                 0.06863          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099177      0.00092446       0.0017425
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017893          5.2777          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71349         0.85282


 TIME FOR THE TIME STEP            10167:        0.80157E+02

===============================================================


 INSTANT    0.101680000E-01   TIME STEP NUMBER           10168
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.280422785E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149528395E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127152439E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.314900225E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.236672675E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      40   0.81208E-03   0.45051E-02 0.19865E+01 
c  Velocity[X]                                      0.13813E-03 
c  Velocity[Y]                                      0.12825E-03 
c  Velocity[Z]                                      0.42388E-02 
c  Pressure     0.36508E-04     133   0.92952E-02   0.25753E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59196E-08   0.16411E-08 0.10021E+00 
c  r22          0.10851E-01      13   0.50531E-08   0.18505E-08 0.10233E+00 
c  r33          0.21857E-01      15   0.66564E-08   0.12669E-07 0.12852E+00 
c  r12          0.93847E-03      18   0.54741E-08   0.30168E-09 0.60843E+00 
c  r13          0.46670E-02      19   0.76096E-08   0.15083E-08 0.20166E+00 
c  r23          0.39970E-02      19   0.57982E-08   0.12855E-08 0.20088E+00 
c  epsilon      0.10970E+02      11   0.35625E-08   0.10051E-01 0.16694E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.84053E-02 0.43269E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63363         0.61356       0.0052546       0.0015074
v  Velocity[Y]            -0.57339         0.54444       0.0030792      0.00087328
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4372          4.3406          4.3632
v  Pressure                -36.428          360.02          87.646          169.84
v  r11                   0.0010597        0.081917         0.01307        0.018284
v  r22                    0.001111        0.082658         0.01335        0.018644
v  r33                    0.001635         0.17432        0.027242        0.037202
v  r12                    -0.01066        0.013575     -0.00023376     -0.00030928
v  r13                   -0.045562        0.052815      9.2843e-05       0.0010136
v  r23                   -0.046713        0.051209      3.0137e-05      0.00057442
v  epsilon                 0.06863          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099177      0.00092446       0.0017425
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017893          5.2782          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71348         0.85282


 TIME FOR THE TIME STEP            10168:        0.75163E+02

===============================================================


 INSTANT    0.101690000E-01   TIME STEP NUMBER           10169
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.318908378E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.868412368E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.985861373E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.943051928E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.249535084E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36448E+01      41   0.81127E-03   0.45535E-02 0.19967E+01 
c  Velocity[X]                                      0.13865E-03 
c  Velocity[Y]                                      0.12959E-03 
c  Velocity[Z]                                      0.42853E-02 
c  Pressure     0.36560E-04     133   0.93059E-02   0.25789E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60590E-08   0.16310E-08 0.99837E-01 
c  r22          0.10851E-01      13   0.53119E-08   0.18237E-08 0.10121E+00 
c  r33          0.21857E-01      15   0.57748E-08   0.12523E-07 0.12736E+00 
c  r12          0.93847E-03      18   0.52802E-08   0.30401E-09 0.60622E+00 
c  r13          0.46670E-02      18   0.68628E-08   0.15017E-08 0.19992E+00 
c  r23          0.39970E-02      19   0.53174E-08   0.12776E-08 0.19997E+00 
c  epsilon      0.10970E+02      11   0.34499E-08   0.99599E-02 0.16481E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.84624E-02 0.43358E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369         0.61353       0.0052546       0.0015074
v  Velocity[Y]            -0.57347         0.54452       0.0030792      0.00087327
v  Velocity[Z]              1.5654          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4372          4.3406          4.3632
v  Pressure                -36.409          360.07          87.679          169.89
v  r11                   0.0010597        0.081919         0.01307        0.018284
v  r22                    0.001111        0.082657         0.01335        0.018644
v  r33                    0.001635         0.17431        0.027242        0.037202
v  r12                   -0.010661         0.01358     -0.00023376     -0.00030928
v  r13                   -0.045562        0.052814      9.2845e-05       0.0010136
v  r23                   -0.046714        0.051205      3.0138e-05      0.00057442
v  epsilon                0.068631          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9917e-05       0.0099177      0.00092446       0.0017425
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017892           5.278         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85283


 TIME FOR THE TIME STEP            10169:        0.77186E+02

===============================================================


 INSTANT    0.101700000E-01   TIME STEP NUMBER           10170
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.164178217E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110948850E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934904E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123985804E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.390315638E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.370951675E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81240E-03   0.45432E-02 0.19968E+01 
c  Velocity[X]                                      0.13985E-03 
c  Velocity[Y]                                      0.12990E-03 
c  Velocity[Z]                                      0.42734E-02 
c  Pressure     0.36422E-04     132   0.92768E-02   0.25692E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59754E-08   0.16513E-08 0.10102E+00 
c  r22          0.10851E-01      13   0.54007E-08   0.18070E-08 0.10189E+00 
c  r33          0.21857E-01      15   0.58681E-08   0.12507E-07 0.12834E+00 
c  r12          0.93847E-03      18   0.48387E-08   0.29936E-09 0.60943E+00 
c  r13          0.46670E-02      19   0.53609E-08   0.14764E-08 0.20018E+00 
c  r23          0.39970E-02      19   0.58955E-08   0.12839E-08 0.20130E+00 
c  epsilon      0.10970E+02      11   0.34694E-08   0.95600E-02 0.16388E+00 
c  TempC        0.25716E+06      16   0.15120E-04   0.84455E-02 0.43341E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63371         0.61356       0.0052545       0.0015074
v  Velocity[Y]            -0.57346         0.54432       0.0030792      0.00087325
v  Velocity[Z]              1.5656          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4372          4.3406          4.3632
v  Pressure                -36.479          360.12           87.74          169.94
v  r11                   0.0010596        0.081918         0.01307        0.018284
v  r22                    0.001111        0.082657         0.01335        0.018644
v  r33                    0.001635         0.17429        0.027242        0.037202
v  r12                   -0.010658        0.013588     -0.00023376     -0.00030928
v  r13                    -0.04556        0.052816      9.2846e-05       0.0010136
v  r23                   -0.046714        0.051195      3.0139e-05      0.00057442
v  epsilon                0.068632          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099177      0.00092446       0.0017425
v  CourantNb                0.4426             0.6         0.59908         0.59839
v  FourierNb             0.0017892          5.2776         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71349         0.85283


 TIME FOR THE TIME STEP            10170:        0.76100E+02

===============================================================


 INSTANT    0.101710000E-01   TIME STEP NUMBER           10171
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.260672831E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.215734924E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935041E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.314891773E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935027E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.415250356E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.563231898E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81224E-03   0.45242E-02 0.19913E+01 
c  Velocity[X]                                      0.13790E-03 
c  Velocity[Y]                                      0.12936E-03 
c  Velocity[Z]                                      0.42569E-02 
c  Pressure     0.36428E-04     134   0.92746E-02   0.25696E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57701E-08   0.17027E-08 0.10193E+00 
c  r22          0.10851E-01      13   0.54322E-08   0.18468E-08 0.10173E+00 
c  r33          0.21857E-01      15   0.67350E-08   0.12778E-07 0.12865E+00 
c  r12          0.93847E-03      18   0.48422E-08   0.30788E-09 0.61411E+00 
c  r13          0.46670E-02      19   0.64636E-08   0.14846E-08 0.19889E+00 
c  r23          0.39970E-02      19   0.57241E-08   0.13092E-08 0.20304E+00 
c  epsilon      0.10970E+02      11   0.34550E-08   0.99228E-02 0.16581E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.83579E-02 0.43150E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63371         0.61357       0.0052545       0.0015073
v  Velocity[Y]             -0.5735         0.54443       0.0030793      0.00087332
v  Velocity[Z]              1.5657          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4372          4.3406          4.3632
v  Pressure                -36.443          360.04          87.666          169.88
v  r11                   0.0010596        0.081911         0.01307        0.018284
v  r22                    0.001111        0.082652         0.01335        0.018644
v  r33                    0.001635         0.17429        0.027242        0.037202
v  r12                   -0.010656        0.013594     -0.00023376     -0.00030928
v  r13                   -0.045563        0.052815      9.2846e-05       0.0010136
v  r23                   -0.046713        0.051194      3.0139e-05      0.00057442
v  epsilon                0.068633          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9911e-05       0.0099177      0.00092446       0.0017425
v  CourantNb               0.44266             0.6         0.59908         0.59839
v  FourierNb             0.0017892          5.2775         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71349         0.85283


 TIME FOR THE TIME STEP            10171:        0.75344E+02

===============================================================


 INSTANT    0.101720000E-01   TIME STEP NUMBER           10172
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.258043899E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.278627253E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934909E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.274566282E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.589218182E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.192839981E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81214E-03   0.45240E-02 0.19925E+01 
c  Velocity[X]                                      0.13907E-03 
c  Velocity[Y]                                      0.12860E-03 
c  Velocity[Z]                                      0.42563E-02 
c  Pressure     0.36306E-04     132   0.92420E-02   0.25610E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56610E-08   0.16917E-08 0.10151E+00 
c  r22          0.10851E-01      13   0.51892E-08   0.18447E-08 0.10201E+00 
c  r33          0.21857E-01      15   0.60067E-08   0.12937E-07 0.12953E+00 
c  r12          0.93847E-03      18   0.49698E-08   0.30240E-09 0.61104E+00 
c  r13          0.46670E-02      19   0.61046E-08   0.15247E-08 0.20140E+00 
c  r23          0.39970E-02      19   0.63137E-08   0.13451E-08 0.20478E+00 
c  epsilon      0.10970E+02      11   0.34851E-08   0.10607E-01 0.17492E+00 
c  TempC        0.25716E+06      16   0.15173E-04   0.84267E-02 0.43367E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162015


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379         0.61354       0.0052545       0.0015073
v  Velocity[Y]            -0.57346         0.54412       0.0030792      0.00087327
v  Velocity[Z]              1.5654          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4372          4.3406          4.3632
v  Pressure                -36.486          359.98          87.642          169.83
v  r11                   0.0010596        0.081913         0.01307        0.018284
v  r22                    0.001111        0.082652         0.01335        0.018644
v  r33                    0.001635         0.17432        0.027242        0.037202
v  r12                   -0.010654          0.0136     -0.00023376     -0.00030928
v  r13                    -0.04556        0.052816      9.2847e-05       0.0010136
v  r23                   -0.046713        0.051228      3.0139e-05      0.00057442
v  epsilon                0.068633          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9907e-05       0.0099176      0.00092447       0.0017425
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb             0.0017892           5.277         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71349         0.85282


 TIME FOR THE TIME STEP            10172:        0.79006E+02

===============================================================


 INSTANT    0.101730000E-01   TIME STEP NUMBER           10173
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.252032870E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.199815136E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182998940E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.408308671E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.243203055E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81156E-03   0.45334E-02 0.19926E+01 
c  Velocity[X]                                      0.13907E-03 
c  Velocity[Y]                                      0.12901E-03 
c  Velocity[Z]                                      0.42653E-02 
c  Pressure     0.36290E-04     133   0.92433E-02   0.25599E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55088E-08   0.16874E-08 0.10162E+00 
c  r22          0.10851E-01      13   0.53205E-08   0.18762E-08 0.10292E+00 
c  r33          0.21857E-01      15   0.65970E-08   0.12838E-07 0.12935E+00 
c  r12          0.93847E-03      18   0.50437E-08   0.30295E-09 0.61269E+00 
c  r13          0.46670E-02      19   0.72936E-08   0.15148E-08 0.20144E+00 
c  r23          0.39970E-02      19   0.56011E-08   0.12961E-08 0.20187E+00 
c  epsilon      0.10970E+02      11   0.34853E-08   0.10139E-01 0.16830E+00 
c  TempC        0.25716E+06      16   0.15122E-04   0.84588E-02 0.43376E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61356       0.0052546       0.0015074
v  Velocity[Y]            -0.57346         0.54414       0.0030792      0.00087326
v  Velocity[Z]              1.5653          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4372          4.3406          4.3632
v  Pressure                  -36.4          360.13          87.703          169.93
v  r11                   0.0010596        0.081917         0.01307        0.018284
v  r22                    0.001111        0.082653         0.01335        0.018644
v  r33                    0.001635         0.17431        0.027242        0.037202
v  r12                   -0.010656        0.013598     -0.00023376     -0.00030928
v  r13                   -0.045561        0.052814      9.2848e-05       0.0010136
v  r23                   -0.046712        0.051228      3.0141e-05      0.00057442
v  epsilon                0.068634          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9903e-05       0.0099177      0.00092447       0.0017425
v  CourantNb               0.44262             0.6         0.59908         0.59839
v  FourierNb             0.0017892           5.277         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71349         0.85283


 TIME FOR THE TIME STEP            10173:        0.79968E+02

===============================================================


 INSTANT    0.101740000E-01   TIME STEP NUMBER           10174
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.521667346E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.458167617E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.681597224E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.375497595E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.346874053E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81272E-03   0.45204E-02 0.19906E+01 
c  Velocity[X]                                      0.13878E-03 
c  Velocity[Y]                                      0.12904E-03 
c  Velocity[Z]                                      0.42526E-02 
c  Pressure     0.36447E-04     131   0.92751E-02   0.25709E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52773E-08   0.16364E-08 0.10000E+00 
c  r22          0.10851E-01      13   0.50724E-08   0.18246E-08 0.10210E+00 
c  r33          0.21857E-01      15   0.60883E-08   0.12416E-07 0.12773E+00 
c  r12          0.93847E-03      17   0.69324E-08   0.30542E-09 0.61348E+00 
c  r13          0.46670E-02      19   0.70115E-08   0.14713E-08 0.20012E+00 
c  r23          0.39970E-02      19   0.62793E-08   0.12791E-08 0.19994E+00 
c  epsilon      0.10970E+02      11   0.34112E-08   0.95043E-02 0.16250E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83670E-02 0.43122E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61358       0.0052545       0.0015074
v  Velocity[Y]            -0.57342          0.5443       0.0030792      0.00087327
v  Velocity[Z]              1.5653          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4372          4.3406          4.3632
v  Pressure                -36.434          359.98          87.633          169.81
v  r11                   0.0010596        0.081918         0.01307        0.018284
v  r22                    0.001111        0.082655         0.01335        0.018644
v  r33                    0.001635         0.17427        0.027242        0.037203
v  r12                   -0.010653        0.013596     -0.00023376     -0.00030928
v  r13                   -0.045564        0.052815      9.2849e-05       0.0010136
v  r23                   -0.046712        0.051222      3.0141e-05      0.00057442
v  epsilon                0.068635           271.2          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc               5.99e-05       0.0099177      0.00092447       0.0017425
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017891          5.2769         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71349         0.85283


 TIME FOR THE TIME STEP            10174:        0.78653E+02

===============================================================


 INSTANT    0.101750000E-01   TIME STEP NUMBER           10175
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138681259E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.291648486E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120176141E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.133487420E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.210971410E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81138E-03   0.45437E-02 0.19993E+01 
c  Velocity[X]                                      0.13994E-03 
c  Velocity[Y]                                      0.13013E-03 
c  Velocity[Z]                                      0.42736E-02 
c  Pressure     0.36741E-04     131   0.93563E-02   0.25917E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.50566E-08   0.16251E-08 0.99781E-01 
c  r22          0.10851E-01      13   0.53182E-08   0.18313E-08 0.10228E+00 
c  r33          0.21857E-01      15   0.58547E-08   0.12383E-07 0.12740E+00 
c  r12          0.93847E-03      17   0.64636E-08   0.30217E-09 0.61048E+00 
c  r13          0.46670E-02      19   0.71900E-08   0.14911E-08 0.19998E+00 
c  r23          0.39970E-02      19   0.63769E-08   0.12732E-08 0.19853E+00 
c  epsilon      0.10970E+02      11   0.32978E-08   0.96406E-02 0.16487E+00 
c  TempC        0.25716E+06      16   0.15100E-04   0.84522E-02 0.43387E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61356       0.0052546       0.0015074
v  Velocity[Y]            -0.57362          0.5445       0.0030793       0.0008733
v  Velocity[Z]              1.5653          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4372          4.3406          4.3632
v  Pressure                -36.407          360.03          87.649          169.85
v  r11                   0.0010596         0.08192         0.01307        0.018284
v  r22                    0.001111        0.082656         0.01335        0.018644
v  r33                    0.001635         0.17429        0.027242        0.037203
v  r12                   -0.010651        0.013596     -0.00023376     -0.00030928
v  r13                   -0.045561        0.052814       9.285e-05       0.0010136
v  r23                   -0.046712        0.051253      3.0142e-05      0.00057442
v  epsilon                0.068635          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9901e-05       0.0099179      0.00092447       0.0017425
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb             0.0017891          5.2771          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71348         0.85282


 TIME FOR THE TIME STEP            10175:        0.79304E+02

===============================================================


 INSTANT    0.101760000E-01   TIME STEP NUMBER           10176
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.479071293E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.438662047E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.222754445E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.308480415E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.635300130E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      40   0.81244E-03   0.45395E-02 0.19976E+01 
c  Velocity[X]                                      0.13875E-03 
c  Velocity[Y]                                      0.12936E-03 
c  Velocity[Z]                                      0.42714E-02 
c  Pressure     0.36529E-04     131   0.93080E-02   0.25768E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51255E-08   0.16492E-08 0.10064E+00 
c  r22          0.10851E-01      13   0.51053E-08   0.18765E-08 0.10297E+00 
c  r33          0.21857E-01      15   0.54830E-08   0.12719E-07 0.12878E+00 
c  r12          0.93847E-03      17   0.64732E-08   0.30660E-09 0.61467E+00 
c  r13          0.46670E-02      19   0.60284E-08   0.15271E-08 0.20204E+00 
c  r23          0.39970E-02      19   0.58640E-08   0.12810E-08 0.20035E+00 
c  epsilon      0.10970E+02      11   0.34137E-08   0.10107E-01 0.16746E+00 
c  TempC        0.25716E+06      16   0.15179E-04   0.84559E-02 0.43377E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61357       0.0052546       0.0015074
v  Velocity[Y]            -0.57351         0.54421       0.0030793      0.00087327
v  Velocity[Z]              1.5654          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4372          4.3406          4.3632
v  Pressure                 -36.48          360.07          87.696           169.9
v  r11                   0.0010596        0.081926         0.01307        0.018284
v  r22                    0.001111        0.082657         0.01335        0.018644
v  r33                    0.001635         0.17433        0.027242        0.037203
v  r12                    -0.01065        0.013591     -0.00023376     -0.00030928
v  r13                   -0.045559        0.052814       9.285e-05       0.0010136
v  r23                   -0.046712        0.051235      3.0142e-05      0.00057442
v  epsilon                0.068636          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc               5.99e-05       0.0099179      0.00092447       0.0017425
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017891          5.2778         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71349         0.85282


 TIME FOR THE TIME STEP            10176:        0.79839E+02

===============================================================


 INSTANT    0.101770000E-01   TIME STEP NUMBER           10177
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.983419408E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.252544769E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.231392182E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935019E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.496829818E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.336928831E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935011E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81180E-03   0.45213E-02 0.19915E+01 
c  Velocity[X]                                      0.13717E-03 
c  Velocity[Y]                                      0.12979E-03 
c  Velocity[Z]                                      0.42544E-02 
c  Pressure     0.35884E-04     131   0.91343E-02   0.25312E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.45722E-08   0.16716E-08 0.10115E+00 
c  r22          0.10851E-01      13   0.45925E-08   0.18528E-08 0.10258E+00 
c  r33          0.21857E-01      15   0.59681E-08   0.12720E-07 0.12924E+00 
c  r12          0.93847E-03      17   0.65327E-08   0.30188E-09 0.61144E+00 
c  r13          0.46670E-02      19   0.55611E-08   0.15083E-08 0.20186E+00 
c  r23          0.39970E-02      19   0.57863E-08   0.13028E-08 0.20252E+00 
c  epsilon      0.10970E+02      11   0.34080E-08   0.10054E-01 0.16638E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.83906E-02 0.43238E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63372         0.61356       0.0052546       0.0015074
v  Velocity[Y]            -0.57361         0.54421       0.0030793      0.00087324
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4372          4.3406          4.3632
v  Pressure                -36.417          360.09          87.678           169.9
v  r11                   0.0010596        0.081931         0.01307        0.018284
v  r22                    0.001111        0.082652         0.01335        0.018644
v  r33                   0.0016349          0.1743        0.027243        0.037203
v  r12                   -0.010648        0.013592     -0.00023376     -0.00030928
v  r13                   -0.045564        0.052816      9.2851e-05       0.0010136
v  r23                   -0.046711        0.051229      3.0143e-05      0.00057442
v  epsilon                0.068637          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9899e-05       0.0099178      0.00092447       0.0017425
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017891          5.2771         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71349         0.85283


 TIME FOR THE TIME STEP            10177:        0.78665E+02

===============================================================


 INSTANT    0.101780000E-01   TIME STEP NUMBER           10178
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267516462E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.473914447E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.631855516E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.183898283E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.213024356E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81252E-03   0.45240E-02 0.19896E+01 
c  Velocity[X]                                      0.13934E-03 
c  Velocity[Y]                                      0.12968E-03 
c  Velocity[Z]                                      0.42550E-02 
c  Pressure     0.36396E-04     131   0.92658E-02   0.25674E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.47712E-08   0.16372E-08 0.10043E+00 
c  r22          0.10851E-01      13   0.47494E-08   0.18038E-08 0.10177E+00 
c  r33          0.21857E-01      15   0.56773E-08   0.12397E-07 0.12822E+00 
c  r12          0.93847E-03      18   0.55438E-08   0.29192E-09 0.60527E+00 
c  r13          0.46670E-02      18   0.69876E-08   0.14656E-08 0.20061E+00 
c  r23          0.39970E-02      19   0.54572E-08   0.12615E-08 0.20068E+00 
c  epsilon      0.10970E+02      11   0.33246E-08   0.95685E-02 0.16330E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.84260E-02 0.43278E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63377         0.61354       0.0052546       0.0015074
v  Velocity[Y]            -0.57362         0.54433       0.0030792      0.00087323
v  Velocity[Z]              1.5654          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4372          4.3406          4.3632
v  Pressure                -36.477          360.01          87.674          169.86
v  r11                   0.0010596         0.08194         0.01307        0.018284
v  r22                    0.001111        0.082653         0.01335        0.018644
v  r33                   0.0016349         0.17427        0.027243        0.037203
v  r12                   -0.010646        0.013589     -0.00023376     -0.00030928
v  r13                   -0.045561        0.052817      9.2852e-05       0.0010136
v  r23                    -0.04671        0.051255      3.0143e-05      0.00057442
v  epsilon                0.068638          271.18          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9899e-05       0.0099178      0.00092447       0.0017425
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017891          5.2766         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71349         0.85283


 TIME FOR THE TIME STEP            10178:        0.80000E+02

===============================================================


 INSTANT    0.101790000E-01   TIME STEP NUMBER           10179
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120673911E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.880866540E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.262697551E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232927615E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.146638339E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81248E-03   0.45608E-02 0.19984E+01 
c  Velocity[X]                                      0.13995E-03 
c  Velocity[Y]                                      0.12990E-03 
c  Velocity[Z]                                      0.42910E-02 
c  Pressure     0.36411E-04     133   0.92706E-02   0.25684E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.46400E-08   0.16371E-08 0.10054E+00 
c  r22          0.10851E-01      13   0.46102E-08   0.18088E-08 0.10204E+00 
c  r33          0.21857E-01      15   0.57783E-08   0.12418E-07 0.12821E+00 
c  r12          0.93847E-03      17   0.67656E-08   0.30196E-09 0.61149E+00 
c  r13          0.46670E-02      18   0.68641E-08   0.14691E-08 0.20040E+00 
c  r23          0.39970E-02      18   0.62756E-08   0.12779E-08 0.20086E+00 
c  epsilon      0.10970E+02      11   0.33202E-08   0.99249E-02 0.16987E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.84879E-02 0.43436E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61356       0.0052546       0.0015073
v  Velocity[Y]            -0.57366          0.5445       0.0030793      0.00087325
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4372          4.3406          4.3632
v  Pressure                -36.415          360.09           87.71          169.92
v  r11                   0.0010596        0.081944         0.01307        0.018284
v  r22                    0.001111        0.082654         0.01335        0.018644
v  r33                   0.0016349          0.1743        0.027243        0.037203
v  r12                   -0.010649        0.013584     -0.00023376     -0.00030928
v  r13                    -0.04556        0.052809      9.2854e-05       0.0010136
v  r23                    -0.04671        0.051244      3.0144e-05      0.00057442
v  epsilon                0.068638           271.2          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc               5.99e-05       0.0099177      0.00092447       0.0017425
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017891          5.2771         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71349         0.85283


 TIME FOR THE TIME STEP            10179:        0.81307E+02

===============================================================


 INSTANT    0.101800000E-01   TIME STEP NUMBER           10180
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.545740737E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.984774270E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.239391521E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.555411257E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.156582027E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81160E-03   0.44870E-02 0.19844E+01 
c  Velocity[X]                                      0.13813E-03 
c  Velocity[Y]                                      0.12873E-03 
c  Velocity[Z]                                      0.42201E-02 
c  Pressure     0.36515E-04     132   0.92988E-02   0.25758E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53035E-08   0.16395E-08 0.10023E+00 
c  r22          0.10851E-01      13   0.46342E-08   0.18313E-08 0.10242E+00 
c  r33          0.21857E-01      15   0.71021E-08   0.12590E-07 0.12825E+00 
c  r12          0.93847E-03      18   0.55243E-08   0.29987E-09 0.60912E+00 
c  r13          0.46670E-02      19   0.61862E-08   0.14959E-08 0.20109E+00 
c  r23          0.39970E-02      19   0.55256E-08   0.12850E-08 0.20007E+00 
c  epsilon      0.10970E+02      11   0.33568E-08   0.10055E-01 0.16733E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.83907E-02 0.43237E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338         0.61355       0.0052545       0.0015073
v  Velocity[Y]            -0.57373         0.54426       0.0030793      0.00087324
v  Velocity[Z]              1.5656          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4372          4.3406          4.3632
v  Pressure                -36.448          360.06          87.689           169.9
v  r11                   0.0010596        0.081945         0.01307        0.018284
v  r22                    0.001111        0.082652         0.01335        0.018644
v  r33                   0.0016349         0.17431        0.027243        0.037203
v  r12                   -0.010652        0.013577     -0.00023376     -0.00030928
v  r13                   -0.045563        0.052806      9.2854e-05       0.0010136
v  r23                   -0.046711        0.051218      3.0144e-05      0.00057442
v  epsilon                0.068639          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9902e-05       0.0099178      0.00092448       0.0017425
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb              0.001789           5.277          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71349         0.85282


 TIME FOR THE TIME STEP            10180:        0.80173E+02

===============================================================


 INSTANT    0.101810000E-01   TIME STEP NUMBER           10181
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.876836664E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.465715589E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.174084257E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.144434290E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.412373613E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81196E-03   0.45624E-02 0.19998E+01 
c  Velocity[X]                                      0.13978E-03 
c  Velocity[Y]                                      0.12928E-03 
c  Velocity[Z]                                      0.42934E-02 
c  Pressure     0.36406E-04     131   0.92656E-02   0.25681E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.46237E-08   0.16221E-08 0.10010E+00 
c  r22          0.10851E-01      13   0.53623E-08   0.18013E-08 0.10188E+00 
c  r33          0.21857E-01      15   0.62447E-08   0.12279E-07 0.12752E+00 
c  r12          0.93847E-03      18   0.65677E-08   0.30146E-09 0.61221E+00 
c  r13          0.46670E-02      19   0.65179E-08   0.14572E-08 0.19957E+00 
c  r23          0.39970E-02      19   0.64169E-08   0.12658E-08 0.19962E+00 
c  epsilon      0.10970E+02      11   0.33804E-08   0.93815E-02 0.16139E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.83799E-02 0.43178E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63359         0.61352       0.0052546       0.0015074
v  Velocity[Y]            -0.57384         0.54435       0.0030794      0.00087328
v  Velocity[Z]              1.5652          5.4372          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4372          4.3406          4.3632
v  Pressure                -36.388          359.97          87.615          169.81
v  r11                   0.0010596        0.081944         0.01307        0.018284
v  r22                    0.001111         0.08265         0.01335        0.018644
v  r33                   0.0016349          0.1743        0.027243        0.037203
v  r12                   -0.010653        0.013577     -0.00023376     -0.00030928
v  r13                   -0.045562        0.052803      9.2855e-05       0.0010136
v  r23                   -0.046711        0.051209      3.0145e-05      0.00057442
v  epsilon                 0.06864          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9901e-05       0.0099178      0.00092448       0.0017425
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb              0.001789          5.2773         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71349         0.85283


 TIME FOR THE TIME STEP            10181:        0.79097E+02

===============================================================


 INSTANT    0.101820000E-01   TIME STEP NUMBER           10182
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.101002974E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232835010E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.163836447E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.141070012E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179773480E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81296E-03   0.45667E-02 0.20000E+01 
c  Velocity[X]                                      0.13966E-03 
c  Velocity[Y]                                      0.12992E-03 
c  Velocity[Z]                                      0.42971E-02 
c  Pressure     0.36655E-04     133   0.93308E-02   0.25857E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53309E-08   0.16454E-08 0.10061E+00 
c  r22          0.10851E-01      13   0.49226E-08   0.18374E-08 0.10237E+00 
c  r33          0.21857E-01      16   0.65348E-08   0.12625E-07 0.12885E+00 
c  r12          0.93847E-03      18   0.60562E-08   0.30558E-09 0.61276E+00 
c  r13          0.46670E-02      20   0.68944E-08   0.15179E-08 0.20230E+00 
c  r23          0.39970E-02      19   0.63181E-08   0.12997E-08 0.20216E+00 
c  epsilon      0.10970E+02      11   0.37923E-08   0.97956E-02 0.16508E+00 
c  TempC        0.25716E+06      16   0.15120E-04   0.84506E-02 0.43354E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6336         0.61355       0.0052546       0.0015074
v  Velocity[Y]            -0.57372         0.54454       0.0030792       0.0008732
v  Velocity[Z]              1.5654          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4372          4.3406          4.3632
v  Pressure                -36.478          360.01          87.652          169.84
v  r11                   0.0010596        0.081945         0.01307        0.018284
v  r22                    0.001111        0.082648         0.01335        0.018644
v  r33                   0.0016349         0.17428        0.027243        0.037203
v  r12                   -0.010653        0.013569     -0.00023376     -0.00030928
v  r13                    -0.04556        0.052804      9.2857e-05       0.0010136
v  r23                   -0.046711        0.051219      3.0145e-05      0.00057442
v  epsilon                0.068641          271.19          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9897e-05       0.0099179      0.00092448       0.0017425
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb              0.001789           5.278         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85283


 TIME FOR THE TIME STEP            10182:        0.79081E+02

===============================================================


 INSTANT    0.101830000E-01   TIME STEP NUMBER           10183
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195165335E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182759787E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119256437E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.629759839E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.272039146E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81140E-03   0.45152E-02 0.19929E+01 
c  Velocity[X]                                      0.13835E-03 
c  Velocity[Y]                                      0.12948E-03 
c  Velocity[Z]                                      0.42474E-02 
c  Pressure     0.36205E-04     131   0.92173E-02   0.25539E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56115E-08   0.16489E-08 0.10083E+00 
c  r22          0.10851E-01      13   0.48558E-08   0.18387E-08 0.10239E+00 
c  r33          0.21857E-01      15   0.61986E-08   0.12541E-07 0.12842E+00 
c  r12          0.93847E-03      18   0.57140E-08   0.30309E-09 0.61308E+00 
c  r13          0.46670E-02      19   0.70918E-08   0.14980E-08 0.20130E+00 
c  r23          0.39970E-02      19   0.64812E-08   0.12750E-08 0.20031E+00 
c  epsilon      0.10970E+02      11   0.34099E-08   0.98195E-02 0.16540E+00 
c  TempC        0.25716E+06      16   0.15095E-04   0.84830E-02 0.43438E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364         0.61355       0.0052546       0.0015073
v  Velocity[Y]            -0.57378         0.54422       0.0030793      0.00087322
v  Velocity[Z]              1.5651          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4372          4.3406          4.3632
v  Pressure                -36.401           360.1          87.708          169.92
v  r11                   0.0010596        0.081938         0.01307        0.018284
v  r22                    0.001111        0.082643         0.01335        0.018644
v  r33                   0.0016349         0.17428        0.027243        0.037203
v  r12                    -0.01065        0.013571     -0.00023376     -0.00030928
v  r13                   -0.045564        0.052804      9.2858e-05       0.0010136
v  r23                   -0.046711         0.05121      3.0145e-05      0.00057442
v  epsilon                0.068642           271.2          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9896e-05       0.0099181      0.00092448       0.0017425
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb              0.001789          5.2782          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71349         0.85282


 TIME FOR THE TIME STEP            10183:        0.80442E+02

===============================================================


 INSTANT    0.101840000E-01   TIME STEP NUMBER           10184
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.205185795E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.751674962E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285465479E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.178965611E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.328395104E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81226E-03   0.45161E-02 0.19922E+01 
c  Velocity[X]                                      0.13855E-03 
c  Velocity[Y]                                      0.12926E-03 
c  Velocity[Z]                                      0.42483E-02 
c  Pressure     0.36629E-04     132   0.93241E-02   0.25839E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56107E-08   0.16308E-08 0.10003E+00 
c  r22          0.10851E-01      13   0.49213E-08   0.18344E-08 0.10223E+00 
c  r33          0.21857E-01      14   0.70949E-08   0.12462E-07 0.12781E+00 
c  r12          0.93847E-03      18   0.51979E-08   0.29518E-09 0.60823E+00 
c  r13          0.46670E-02      19   0.71363E-08   0.14843E-08 0.20032E+00 
c  r23          0.39970E-02      20   0.57924E-08   0.12625E-08 0.19958E+00 
c  epsilon      0.10970E+02      11   0.32756E-08   0.96684E-02 0.16299E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.84471E-02 0.43318E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61353       0.0052545       0.0015073
v  Velocity[Y]            -0.57372         0.54423       0.0030792      0.00087321
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4372          4.3406          4.3632
v  Pressure                 -36.43          360.02          87.651          169.85
v  r11                   0.0010596        0.081928         0.01307        0.018284
v  r22                   0.0011109        0.082642         0.01335        0.018644
v  r33                   0.0016349         0.17431        0.027243        0.037203
v  r12                    -0.01065        0.013569     -0.00023376     -0.00030928
v  r13                   -0.045561        0.052801      9.2858e-05       0.0010136
v  r23                   -0.046711        0.051196      3.0146e-05      0.00057442
v  epsilon                0.068642          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9893e-05       0.0099177      0.00092448       0.0017425
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb              0.001789           5.278         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85282


 TIME FOR THE TIME STEP            10184:        0.80648E+02

===============================================================


 INSTANT    0.101850000E-01   TIME STEP NUMBER           10185
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.157279695E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.135254618E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.248867701E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127529072E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.473428954E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81117E-03   0.45382E-02 0.19931E+01 
c  Velocity[X]                                      0.13952E-03 
c  Velocity[Y]                                      0.12913E-03 
c  Velocity[Z]                                      0.42696E-02 
c  Pressure     0.36141E-04     133   0.92110E-02   0.25493E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.61551E-08   0.16415E-08 0.10016E+00 
c  r22          0.10851E-01      13   0.49158E-08   0.17990E-08 0.10110E+00 
c  r33          0.21857E-01      15   0.53640E-08   0.12407E-07 0.12745E+00 
c  r12          0.93847E-03      18   0.55830E-08   0.30028E-09 0.60906E+00 
c  r13          0.46670E-02      19   0.72103E-08   0.14761E-08 0.19920E+00 
c  r23          0.39970E-02      19   0.71306E-08   0.12717E-08 0.19999E+00 
c  epsilon      0.10970E+02      11   0.32118E-08   0.95844E-02 0.16246E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84196E-02 0.43302E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369         0.61356       0.0052546       0.0015073
v  Velocity[Y]            -0.57382         0.54438       0.0030793      0.00087321
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4373          4.3406          4.3632
v  Pressure                -36.405          360.11          87.702          169.92
v  r11                   0.0010596        0.081915         0.01307        0.018284
v  r22                   0.0011109        0.082641         0.01335        0.018644
v  r33                   0.0016349          0.1743        0.027243        0.037203
v  r12                   -0.010649        0.013567     -0.00023376     -0.00030928
v  r13                   -0.045562        0.052797      9.2859e-05       0.0010136
v  r23                   -0.046711        0.051196      3.0146e-05      0.00057442
v  epsilon                0.068643           271.2          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9892e-05       0.0099174      0.00092448       0.0017425
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb              0.001789          5.2776          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71349         0.85282


 TIME FOR THE TIME STEP            10185:        0.79220E+02

===============================================================


 INSTANT    0.101860000E-01   TIME STEP NUMBER           10186
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.288084661E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.176063195E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140855644E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935035E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221920430E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.430936150E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81311E-03   0.44980E-02 0.19872E+01 
c  Velocity[X]                                      0.13815E-03 
c  Velocity[Y]                                      0.12933E-03 
c  Velocity[Z]                                      0.42305E-02 
c  Pressure     0.36446E-04     132   0.92833E-02   0.25709E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58465E-08   0.16505E-08 0.10027E+00 
c  r22          0.10851E-01      13   0.45898E-08   0.18119E-08 0.10163E+00 
c  r33          0.21857E-01      15   0.68553E-08   0.12535E-07 0.12811E+00 
c  r12          0.93847E-03      18   0.53822E-08   0.30193E-09 0.60970E+00 
c  r13          0.46670E-02      20   0.59836E-08   0.14790E-08 0.20022E+00 
c  r23          0.39970E-02      20   0.57831E-08   0.13070E-08 0.20229E+00 
c  epsilon      0.10970E+02      11   0.33608E-08   0.99791E-02 0.17021E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.83703E-02 0.43182E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61356       0.0052546       0.0015073
v  Velocity[Y]            -0.57377         0.54448       0.0030792       0.0008732
v  Velocity[Z]              1.5655          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4373          4.3406          4.3632
v  Pressure                -36.493          360.02          87.659          169.85
v  r11                   0.0010596        0.081907         0.01307        0.018284
v  r22                   0.0011109         0.08264         0.01335        0.018644
v  r33                   0.0016349         0.17427        0.027243        0.037203
v  r12                   -0.010651        0.013571     -0.00023376     -0.00030928
v  r13                   -0.045564        0.052798      9.2859e-05       0.0010136
v  r23                   -0.046711        0.051227      3.0146e-05      0.00057442
v  epsilon                0.068644          271.16          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9891e-05       0.0099174      0.00092448       0.0017425
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017889          5.2774         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71349         0.85283


 TIME FOR THE TIME STEP            10186:        0.79183E+02

===============================================================


 INSTANT    0.101870000E-01   TIME STEP NUMBER           10187
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.913990570E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.402684028E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.302474127E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.873117130E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.103044285E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81132E-03   0.45409E-02 0.19964E+01 
c  Velocity[X]                                      0.13813E-03 
c  Velocity[Y]                                      0.12930E-03 
c  Velocity[Z]                                      0.42735E-02 
c  Pressure     0.36526E-04     133   0.92910E-02   0.25765E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57293E-08   0.16259E-08 0.99638E-01 
c  r22          0.10851E-01      13   0.50827E-08   0.18384E-08 0.10212E+00 
c  r33          0.21857E-01      15   0.64548E-08   0.12488E-07 0.12764E+00 
c  r12          0.93847E-03      18   0.57245E-08   0.29332E-09 0.60376E+00 
c  r13          0.46670E-02      19   0.72728E-08   0.14828E-08 0.20004E+00 
c  r23          0.39970E-02      20   0.58410E-08   0.12631E-08 0.19822E+00 
c  epsilon      0.10970E+02      11   0.34060E-08   0.97711E-02 0.16440E+00 
c  TempC        0.25716E+06      16   0.15125E-04   0.84107E-02 0.43284E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61354       0.0052545       0.0015073
v  Velocity[Y]            -0.57386          0.5443       0.0030792      0.00087323
v  Velocity[Z]              1.5655          5.4372          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4372          4.3406          4.3632
v  Pressure                -36.392          360.04          87.657          169.86
v  r11                   0.0010596        0.081904         0.01307        0.018284
v  r22                   0.0011109        0.082638         0.01335        0.018644
v  r33                   0.0016349         0.17429        0.027243        0.037203
v  r12                   -0.010653        0.013575     -0.00023376     -0.00030928
v  r13                   -0.045562        0.052794       9.286e-05       0.0010136
v  r23                   -0.046711        0.051217      3.0146e-05      0.00057442
v  epsilon                0.068645          271.15          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9895e-05       0.0099175      0.00092449       0.0017425
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017889          5.2768         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71349         0.85283


 TIME FOR THE TIME STEP            10187:        0.79087E+02

===============================================================


 INSTANT    0.101880000E-01   TIME STEP NUMBER           10188
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.396848072E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.157644804E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934902E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.288962783E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.255304111E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226889406E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81247E-03   0.45413E-02 0.19958E+01 
c  Velocity[X]                                      0.13911E-03 
c  Velocity[Y]                                      0.12923E-03 
c  Velocity[Z]                                      0.42730E-02 
c  Pressure     0.36501E-04     131   0.92948E-02   0.25747E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57549E-08   0.16330E-08 0.99909E-01 
c  r22          0.10851E-01      13   0.47576E-08   0.18290E-08 0.10157E+00 
c  r33          0.21857E-01      15   0.60989E-08   0.12469E-07 0.12719E+00 
c  r12          0.93847E-03      18   0.55648E-08   0.30267E-09 0.60910E+00 
c  r13          0.46670E-02      19   0.61521E-08   0.15108E-08 0.20071E+00 
c  r23          0.39970E-02      19   0.63593E-08   0.12757E-08 0.19914E+00 
c  epsilon      0.10970E+02      11   0.35115E-08   0.98729E-02 0.16523E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84414E-02 0.43357E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63366         0.61356       0.0052546       0.0015074
v  Velocity[Y]            -0.57386         0.54442       0.0030792      0.00087319
v  Velocity[Z]              1.5652          5.4373          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4373          4.3406          4.3632
v  Pressure                -36.448          360.06          87.675          169.88
v  r11                   0.0010596        0.081905         0.01307        0.018284
v  r22                   0.0011109        0.082637         0.01335        0.018644
v  r33                   0.0016349         0.17432        0.027243        0.037203
v  r12                   -0.010653        0.013574     -0.00023376     -0.00030928
v  r13                    -0.04556        0.052796      9.2861e-05       0.0010136
v  r23                    -0.04671        0.051201      3.0147e-05      0.00057442
v  epsilon                0.068646          271.19          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9899e-05       0.0099176      0.00092449       0.0017425
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017889          5.2762         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8762         0.71349         0.85283


 TIME FOR THE TIME STEP            10188:        0.80668E+02

===============================================================


 INSTANT    0.101890000E-01   TIME STEP NUMBER           10189
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127972657E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.597167601E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.767392660E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110881405E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.552516209E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81211E-03   0.45199E-02 0.19900E+01 
c  Velocity[X]                                      0.13805E-03 
c  Velocity[Y]                                      0.12909E-03 
c  Velocity[Z]                                      0.42528E-02 
c  Pressure     0.36184E-04     132   0.92088E-02   0.25524E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.62200E-08   0.16476E-08 0.10050E+00 
c  r22          0.10851E-01      13   0.46934E-08   0.18113E-08 0.10152E+00 
c  r33          0.21857E-01      15   0.54905E-08   0.12416E-07 0.12755E+00 
c  r12          0.93847E-03      18   0.53611E-08   0.29803E-09 0.60604E+00 
c  r13          0.46670E-02      18   0.66773E-08   0.14833E-08 0.19946E+00 
c  r23          0.39971E-02      19   0.61740E-08   0.12805E-08 0.19973E+00 
c  epsilon      0.10970E+02      11   0.35046E-08   0.97617E-02 0.16569E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.84078E-02 0.43219E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63363         0.61356       0.0052545       0.0015073
v  Velocity[Y]             -0.5739          0.5441       0.0030792       0.0008732
v  Velocity[Z]              1.5654          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                -36.403          360.11          87.694          169.92
v  r11                   0.0010596        0.081906         0.01307        0.018284
v  r22                   0.0011109        0.082638         0.01335        0.018644
v  r33                   0.0016349         0.17429        0.027243        0.037203
v  r12                   -0.010655        0.013578     -0.00023376     -0.00030928
v  r13                   -0.045565        0.052798      9.2861e-05       0.0010136
v  r23                   -0.046709        0.051229      3.0148e-05      0.00057442
v  epsilon                0.068646          271.19          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9902e-05       0.0099175      0.00092449       0.0017425
v  CourantNb               0.44217             0.6         0.59908         0.59839
v  FourierNb             0.0017889          5.2765          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765         0.71349         0.85282


 TIME FOR THE TIME STEP            10189:        0.80802E+02

===============================================================


 INSTANT    0.101900000E-01   TIME STEP NUMBER           10190
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178515901E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69781E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.889418437E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69781E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.176819465E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69781E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.314138135E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69781E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.953382733E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69781E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81117E-03   0.45475E-02 0.19970E+01 
c  Velocity[X]                                      0.13896E-03 
c  Velocity[Y]                                      0.12956E-03 
c  Velocity[Z]                                      0.42790E-02 
c  Pressure     0.36586E-04     133   0.93072E-02   0.25807E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.62157E-08   0.16114E-08 0.99140E-01 
c  r22          0.10851E-01      13   0.47305E-08   0.18113E-08 0.10152E+00 
c  r33          0.21857E-01      15   0.56000E-08   0.12301E-07 0.12661E+00 
c  r12          0.93847E-03      18   0.52380E-08   0.29386E-09 0.60372E+00 
c  r13          0.46670E-02      19   0.55058E-08   0.14746E-08 0.19965E+00 
c  r23          0.39971E-02      19   0.61326E-08   0.12575E-08 0.19746E+00 
c  epsilon      0.10970E+02      11   0.33351E-08   0.97250E-02 0.16299E+00 
c  TempC        0.25716E+06      16   0.15125E-04   0.84373E-02 0.43298E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63372         0.61352       0.0052546       0.0015073
v  Velocity[Y]            -0.57382         0.54418       0.0030791      0.00087319
v  Velocity[Z]              1.5654          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                 -36.43          359.99          87.644          169.82
v  r11                   0.0010595        0.081909         0.01307        0.018284
v  r22                   0.0011109        0.082635         0.01335        0.018644
v  r33                   0.0016349         0.17427        0.027243        0.037203
v  r12                   -0.010656        0.013576     -0.00023376     -0.00030928
v  r13                   -0.045561        0.052802      9.2862e-05       0.0010136
v  r23                   -0.046709        0.051218      3.0148e-05      0.00057442
v  epsilon                0.068647          271.15          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9904e-05       0.0099175      0.00092449       0.0017425
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017889          5.2765         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765         0.71349         0.85283


 TIME FOR THE TIME STEP            10190:        0.79364E+02

===============================================================


 INSTANT    0.101910000E-01   TIME STEP NUMBER           10191
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151222069E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69781E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.344892735E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69781E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.211136945E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69781E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.246821930E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69781E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.554068907E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69781E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81249E-03   0.45592E-02 0.19988E+01 
c  Velocity[X]                                      0.13941E-03 
c  Velocity[Y]                                      0.12940E-03 
c  Velocity[Z]                                      0.42904E-02 
c  Pressure     0.36467E-04     133   0.92876E-02   0.25724E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.62400E-08   0.16365E-08 0.99766E-01 
c  r22          0.10851E-01      13   0.48926E-08   0.17956E-08 0.10084E+00 
c  r33          0.21857E-01      15   0.70075E-08   0.12324E-07 0.12637E+00 
c  r12          0.93847E-03      18   0.53083E-08   0.29851E-09 0.60426E+00 
c  r13          0.46670E-02      19   0.73390E-08   0.14732E-08 0.19881E+00 
c  r23          0.39971E-02      19   0.71922E-08   0.12610E-08 0.19688E+00 
c  epsilon      0.10970E+02      11   0.34246E-08   0.98122E-02 0.16433E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.84481E-02 0.43392E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61357       0.0052546       0.0015073
v  Velocity[Y]            -0.57388         0.54434       0.0030792      0.00087324
v  Velocity[Z]              1.5653          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4373          4.3406          4.3632
v  Pressure                -36.398          360.16          87.729          169.96
v  r11                   0.0010595        0.081906         0.01307        0.018284
v  r22                   0.0011109        0.082636         0.01335        0.018644
v  r33                   0.0016348         0.17429        0.027243        0.037203
v  r12                   -0.010655        0.013578     -0.00023376     -0.00030928
v  r13                    -0.04556        0.052801      9.2862e-05       0.0010136
v  r23                   -0.046709        0.051207      3.0149e-05      0.00057442
v  epsilon                0.068648          271.16          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9909e-05       0.0099175      0.00092449       0.0017425
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017888          5.2772         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71349         0.85282


 TIME FOR THE TIME STEP            10191:        0.78070E+02

===============================================================


 INSTANT    0.101920000E-01   TIME STEP NUMBER           10192
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.424499649E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.266832251E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.770159787E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935014E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136103016E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.846371413E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81281E-03   0.44901E-02 0.19843E+01 
c  Velocity[X]                                      0.13843E-03 
c  Velocity[Y]                                      0.12886E-03 
c  Velocity[Z]                                      0.42228E-02 
c  Pressure     0.36312E-04     133   0.92425E-02   0.25614E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.62477E-08   0.16800E-08 0.10079E+00 
c  r22          0.10851E-01      13   0.49655E-08   0.18140E-08 0.10131E+00 
c  r33          0.21857E-01      15   0.64328E-08   0.12643E-07 0.12791E+00 
c  r12          0.93847E-03      18   0.56655E-08   0.30017E-09 0.60555E+00 
c  r13          0.46670E-02      19   0.68580E-08   0.14842E-08 0.19961E+00 
c  r23          0.39971E-02      19   0.71519E-08   0.13132E-08 0.20169E+00 
c  epsilon      0.10970E+02      11   0.32835E-08   0.10500E-01 0.17377E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.83821E-02 0.43200E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61357       0.0052546       0.0015073
v  Velocity[Y]            -0.57363         0.54446       0.0030792      0.00087321
v  Velocity[Z]              1.5655          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                -36.491          360.01          87.644          169.84
v  r11                   0.0010595        0.081907         0.01307        0.018284
v  r22                   0.0011109        0.082636         0.01335        0.018644
v  r33                   0.0016348         0.17431        0.027243        0.037203
v  r12                   -0.010659        0.013576     -0.00023376     -0.00030928
v  r13                   -0.045564        0.052801      9.2863e-05       0.0010136
v  r23                   -0.046708        0.051219      3.0149e-05      0.00057443
v  epsilon                0.068649          271.18          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9911e-05       0.0099176      0.00092449       0.0017425
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017888          5.2777         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71349         0.85283


 TIME FOR THE TIME STEP            10192:        0.80588E+02

===============================================================


 INSTANT    0.101930000E-01   TIME STEP NUMBER           10193
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.175273399E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.390070510E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.469751527E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.310318160E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.510750879E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81125E-03   0.45448E-02 0.19967E+01 
c  Velocity[X]                                      0.13886E-03 
c  Velocity[Y]                                      0.12975E-03 
c  Velocity[Z]                                      0.42762E-02 
c  Pressure     0.36459E-04     131   0.92848E-02   0.25718E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58989E-08   0.16153E-08 0.99450E-01 
c  r22          0.10851E-01      13   0.52784E-08   0.18130E-08 0.10164E+00 
c  r33          0.21857E-01      15   0.56665E-08   0.12366E-07 0.12706E+00 
c  r12          0.93847E-03      18   0.52170E-08   0.29743E-09 0.60655E+00 
c  r13          0.46670E-02      19   0.63171E-08   0.14917E-08 0.19994E+00 
c  r23          0.39971E-02      19   0.71618E-08   0.12732E-08 0.19857E+00 
c  epsilon      0.10970E+02      11   0.31652E-08   0.96262E-02 0.16277E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.84523E-02 0.43361E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61356       0.0052547       0.0015073
v  Velocity[Y]            -0.57369         0.54428       0.0030793      0.00087326
v  Velocity[Z]              1.5652          5.4373          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4373          4.3406          4.3632
v  Pressure                  -36.4             360          87.648          169.84
v  r11                   0.0010595        0.081908         0.01307        0.018284
v  r22                   0.0011109        0.082638         0.01335        0.018644
v  r33                   0.0016348          0.1743        0.027243        0.037203
v  r12                   -0.010657        0.013574     -0.00023376     -0.00030928
v  r13                   -0.045563        0.052801      9.2864e-05       0.0010136
v  r23                   -0.046708        0.051204      3.0149e-05      0.00057443
v  epsilon                 0.06865          271.19          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9911e-05       0.0099179      0.00092449       0.0017425
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017888           5.278         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85283


 TIME FOR THE TIME STEP            10193:        0.79711E+02

===============================================================


 INSTANT    0.101940000E-01   TIME STEP NUMBER           10194
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.935687491E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.196570793E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.797477200E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.274344493E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.206480855E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81224E-03   0.45808E-02 0.20022E+01 
c  Velocity[X]                                      0.13937E-03 
c  Velocity[Y]                                      0.12971E-03 
c  Velocity[Z]                                      0.43117E-02 
c  Pressure     0.36470E-04     131   0.92851E-02   0.25726E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55771E-08   0.16451E-08 0.10011E+00 
c  r22          0.10851E-01      13   0.51632E-08   0.17894E-08 0.10072E+00 
c  r33          0.21857E-01      15   0.60067E-08   0.12425E-07 0.12733E+00 
c  r12          0.93847E-03      18   0.49610E-08   0.29869E-09 0.60721E+00 
c  r13          0.46670E-02      19   0.68267E-08   0.14787E-08 0.19937E+00 
c  r23          0.39971E-02      19   0.62271E-08   0.12948E-08 0.20069E+00 
c  epsilon      0.10970E+02      10   0.54432E-08   0.96971E-02 0.16318E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84708E-02 0.43400E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61356       0.0052546       0.0015073
v  Velocity[Y]            -0.57357         0.54437       0.0030793      0.00087325
v  Velocity[Z]              1.5654          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                -36.422          360.03          87.668          169.86
v  r11                   0.0010595        0.081906         0.01307        0.018284
v  r22                   0.0011109        0.082639         0.01335        0.018644
v  r33                   0.0016348         0.17427        0.027243        0.037203
v  r12                   -0.010657        0.013582     -0.00023376     -0.00030928
v  r13                   -0.045562        0.052803      9.2866e-05       0.0010136
v  r23                   -0.046707        0.051185      3.0151e-05      0.00057443
v  epsilon                0.068651          271.15          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9909e-05       0.0099176      0.00092449       0.0017425
v  CourantNb               0.44213             0.6         0.59908         0.59839
v  FourierNb             0.0017888          5.2777         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71349         0.85283


 TIME FOR THE TIME STEP            10194:        0.82243E+02

===============================================================


 INSTANT    0.101950000E-01   TIME STEP NUMBER           10195
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171362738E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.866762475E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125182835E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.948765769E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.342467432E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81235E-03   0.45196E-02 0.19912E+01 
c  Velocity[X]                                      0.13843E-03 
c  Velocity[Y]                                      0.12891E-03 
c  Velocity[Z]                                      0.42523E-02 
c  Pressure     0.36315E-04     133   0.92459E-02   0.25617E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53605E-08   0.16698E-08 0.10095E+00 
c  r22          0.10851E-01      13   0.52623E-08   0.18462E-08 0.10214E+00 
c  r33          0.21857E-01      15   0.55890E-08   0.12656E-07 0.12849E+00 
c  r12          0.93847E-03      18   0.49405E-08   0.29752E-09 0.60902E+00 
c  r13          0.46670E-02      19   0.69907E-08   0.15170E-08 0.20114E+00 
c  r23          0.39971E-02      19   0.67776E-08   0.13007E-08 0.20223E+00 
c  epsilon      0.10970E+02      11   0.33426E-08   0.97634E-02 0.16453E+00 
c  TempC        0.25716E+06      16   0.15105E-04   0.83761E-02 0.43149E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61358       0.0052547       0.0015073
v  Velocity[Y]            -0.57364         0.54437       0.0030793      0.00087329
v  Velocity[Z]              1.5656          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4373          4.3406          4.3632
v  Pressure                -36.431          360.14          87.717          169.94
v  r11                   0.0010595        0.081904         0.01307        0.018284
v  r22                   0.0011109        0.082636         0.01335        0.018644
v  r33                   0.0016348         0.17427        0.027243        0.037203
v  r12                   -0.010655        0.013576     -0.00023376     -0.00030928
v  r13                   -0.045564        0.052803      9.2867e-05       0.0010136
v  r23                   -0.046706        0.051202      3.0152e-05      0.00057443
v  epsilon                0.068651          271.16          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9909e-05       0.0099173       0.0009245       0.0017425
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017888          5.2775          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71348         0.85282


 TIME FOR THE TIME STEP            10195:        0.83530E+02

===============================================================


 INSTANT    0.101960000E-01   TIME STEP NUMBER           10196
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.344871415E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282430481E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.590300375E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.326072994E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.196172545E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81192E-03   0.45299E-02 0.19925E+01 
c  Velocity[X]                                      0.13948E-03 
c  Velocity[Y]                                      0.12926E-03 
c  Velocity[Z]                                      0.42611E-02 
c  Pressure     0.36600E-04     132   0.93214E-02   0.25818E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60435E-08   0.16729E-08 0.10116E+00 
c  r22          0.10851E-01      13   0.53068E-08   0.18262E-08 0.10206E+00 
c  r33          0.21857E-01      15   0.62064E-08   0.12574E-07 0.12859E+00 
c  r12          0.93848E-03      18   0.51763E-08   0.30008E-09 0.60677E+00 
c  r13          0.46670E-02      19   0.67643E-08   0.14847E-08 0.20008E+00 
c  r23          0.39971E-02      19   0.72004E-08   0.13019E-08 0.20203E+00 
c  epsilon      0.10970E+02      11   0.33770E-08   0.96906E-02 0.16655E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.84175E-02 0.43296E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379         0.61354       0.0052547       0.0015074
v  Velocity[Y]            -0.57359         0.54446       0.0030793      0.00087326
v  Velocity[Z]              1.5654          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                -36.477          359.99          87.642          169.83
v  r11                   0.0010595        0.081899         0.01307        0.018284
v  r22                   0.0011109        0.082637         0.01335        0.018644
v  r33                   0.0016348          0.1743        0.027243        0.037203
v  r12                   -0.010654         0.01357     -0.00023376     -0.00030928
v  r13                   -0.045561        0.052803      9.2869e-05       0.0010136
v  r23                   -0.046706        0.051192      3.0153e-05      0.00057443
v  epsilon                0.068652          271.18          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9908e-05       0.0099173       0.0009245       0.0017425
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017887          5.2776          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71348         0.85282


 TIME FOR THE TIME STEP            10196:        0.82392E+02

===============================================================


 INSTANT    0.101970000E-01   TIME STEP NUMBER           10197
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.113719459E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.189370924E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.379016873E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.400003166E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242559761E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81165E-03   0.45377E-02 0.19944E+01 
c  Velocity[X]                                      0.13965E-03 
c  Velocity[Y]                                      0.12896E-03 
c  Velocity[Z]                                      0.42691E-02 
c  Pressure     0.36338E-04     132   0.92461E-02   0.25632E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54411E-08   0.16532E-08 0.10062E+00 
c  r22          0.10851E-01      13   0.52781E-08   0.18431E-08 0.10231E+00 
c  r33          0.21857E-01      15   0.54128E-08   0.12572E-07 0.12854E+00 
c  r12          0.93848E-03      18   0.50573E-08   0.29861E-09 0.60737E+00 
c  r13          0.46670E-02      19   0.65620E-08   0.14992E-08 0.20073E+00 
c  r23          0.39971E-02      19   0.59598E-08   0.12836E-08 0.20077E+00 
c  epsilon      0.10970E+02      11   0.32557E-08   0.97794E-02 0.16572E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.84634E-02 0.43473E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379         0.61356       0.0052547       0.0015074
v  Velocity[Y]            -0.57366         0.54458       0.0030793      0.00087325
v  Velocity[Z]              1.5655          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4373          4.3406          4.3632
v  Pressure                -36.419          360.01          87.626          169.84
v  r11                   0.0010595         0.08189         0.01307        0.018284
v  r22                   0.0011109        0.082638         0.01335        0.018644
v  r33                   0.0016348         0.17429        0.027243        0.037203
v  r12                   -0.010651        0.013575     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052803       9.287e-05       0.0010136
v  r23                   -0.046706        0.051179      3.0154e-05      0.00057443
v  epsilon                0.068653          271.16          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9907e-05       0.0099173       0.0009245       0.0017425
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017887          5.2776         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71349         0.85282


 TIME FOR THE TIME STEP            10197:        0.82318E+02

===============================================================


 INSTANT    0.101980000E-01   TIME STEP NUMBER           10198
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105818234E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.142208363E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.301076378E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.424843729E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.728930907E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81270E-03   0.45236E-02 0.19930E+01 
c  Velocity[X]                                      0.13863E-03 
c  Velocity[Y]                                      0.12949E-03 
c  Velocity[Z]                                      0.42555E-02 
c  Pressure     0.36515E-04     133   0.92985E-02   0.25757E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54081E-08   0.16948E-08 0.10163E+00 
c  r22          0.10851E-01      13   0.53713E-08   0.18216E-08 0.10191E+00 
c  r33          0.21857E-01      15   0.56120E-08   0.12756E-07 0.12941E+00 
c  r12          0.93848E-03      18   0.55210E-08   0.30499E-09 0.61232E+00 
c  r13          0.46670E-02      19   0.57172E-08   0.14898E-08 0.20027E+00 
c  r23          0.39971E-02      19   0.66336E-08   0.13273E-08 0.20353E+00 
c  epsilon      0.10970E+02      11   0.32333E-08   0.10092E-01 0.17095E+00 
c  TempC        0.25716E+06      16   0.15142E-04   0.83721E-02 0.43165E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61355       0.0052547       0.0015074
v  Velocity[Y]            -0.57356         0.54435       0.0030792       0.0008732
v  Velocity[Z]              1.5653          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4373          4.3406          4.3632
v  Pressure                -36.485          360.05          87.679          169.88
v  r11                   0.0010595        0.081876         0.01307        0.018284
v  r22                   0.0011109         0.08264         0.01335        0.018644
v  r33                   0.0016348         0.17425        0.027243        0.037203
v  r12                    -0.01065        0.013577     -0.00023377     -0.00030928
v  r13                   -0.045565        0.052806      9.2871e-05       0.0010136
v  r23                   -0.046705        0.051171      3.0154e-05      0.00057443
v  epsilon                0.068654          271.15          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9906e-05       0.0099175       0.0009245       0.0017425
v  CourantNb                0.4422             0.6         0.59908         0.59839
v  FourierNb             0.0017887          5.2778         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71349         0.85283


 TIME FOR THE TIME STEP            10198:        0.82281E+02

===============================================================


 INSTANT    0.101990000E-01   TIME STEP NUMBER           10199
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129425470E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120393243E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.210379821E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.152303447E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.897753604E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81170E-03   0.45797E-02 0.20030E+01 
c  Velocity[X]                                      0.13962E-03 
c  Velocity[Y]                                      0.12935E-03 
c  Velocity[Z]                                      0.43107E-02 
c  Pressure     0.36697E-04     133   0.93419E-02   0.25886E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59711E-08   0.16118E-08 0.99379E-01 
c  r22          0.10851E-01      13   0.54325E-08   0.18110E-08 0.10136E+00 
c  r33          0.21857E-01      15   0.63992E-08   0.12283E-07 0.12676E+00 
c  r12          0.93848E-03      18   0.56161E-08   0.30490E-09 0.61119E+00 
c  r13          0.46670E-02      19   0.53340E-08   0.14831E-08 0.19943E+00 
c  r23          0.39971E-02      19   0.60194E-08   0.12591E-08 0.19822E+00 
c  epsilon      0.10970E+02      11   0.32604E-08   0.95692E-02 0.16299E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.84790E-02 0.43398E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61353       0.0052547       0.0015073
v  Velocity[Y]            -0.57354         0.54442       0.0030793      0.00087323
v  Velocity[Z]              1.5652          5.4373          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4373          4.3406          4.3632
v  Pressure                -36.383          360.03          87.658          169.86
v  r11                   0.0010595        0.081865         0.01307        0.018284
v  r22                   0.0011109         0.08264         0.01335        0.018644
v  r33                   0.0016348         0.17427        0.027243        0.037203
v  r12                   -0.010651        0.013586     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052804      9.2872e-05       0.0010136
v  r23                   -0.046706        0.051192      3.0154e-05      0.00057443
v  epsilon                0.068655          271.13          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9906e-05       0.0099176       0.0009245       0.0017425
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017887          5.2778         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71349         0.85283


 TIME FOR THE TIME STEP            10199:        0.81340E+02

===============================================================


 INSTANT    0.102000000E-01   TIME STEP NUMBER           10200
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.311975347E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171677371E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.237876497E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.970728470E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.866893550E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81196E-03   0.45288E-02 0.19907E+01 
c  Velocity[X]                                      0.13886E-03 
c  Velocity[Y]                                      0.12877E-03 
c  Velocity[Z]                                      0.42611E-02 
c  Pressure     0.36378E-04     132   0.92632E-02   0.25661E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56515E-08   0.16478E-08 0.10005E+00 
c  r22          0.10851E-01      13   0.53197E-08   0.18332E-08 0.10163E+00 
c  r33          0.21857E-01      15   0.56777E-08   0.12576E-07 0.12769E+00 
c  r12          0.93848E-03      18   0.56042E-08   0.29912E-09 0.60761E+00 
c  r13          0.46670E-02      19   0.58232E-08   0.15034E-08 0.20027E+00 
c  r23          0.39971E-02      19   0.65935E-08   0.12761E-08 0.19891E+00 
c  epsilon      0.10970E+02      11   0.33073E-08   0.10024E-01 0.16538E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.84518E-02 0.43354E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338         0.61353       0.0052548       0.0015074
v  Velocity[Y]            -0.57335          0.5446       0.0030793      0.00087322
v  Velocity[Z]              1.5654          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4373          4.3406          4.3632
v  Pressure                -36.479          360.03          87.664          169.87
v  r11                   0.0010595        0.081856         0.01307        0.018284
v  r22                   0.0011109        0.082639         0.01335        0.018644
v  r33                   0.0016348          0.1743        0.027243        0.037203
v  r12                   -0.010651         0.01359     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052804      9.2873e-05       0.0010136
v  r23                   -0.046707        0.051193      3.0155e-05      0.00057443
v  epsilon                0.068656          271.16          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9907e-05       0.0099177       0.0009245       0.0017425
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017887          5.2776         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71349         0.85283


 TIME FOR THE TIME STEP            10200:        0.80156E+02

===============================================================


 INSTANT    0.102010000E-01   TIME STEP NUMBER           10201
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.152876408E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.143508838E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.167015509E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.215978808E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.277703259E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81198E-03   0.45077E-02 0.19885E+01 
c  Velocity[X]                                      0.13876E-03 
c  Velocity[Y]                                      0.12882E-03 
c  Velocity[Z]                                      0.42402E-02 
c  Pressure     0.36440E-04     132   0.92758E-02   0.25704E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57162E-08   0.16113E-08 0.99368E-01 
c  r22          0.10851E-01      13   0.52941E-08   0.18194E-08 0.10152E+00 
c  r33          0.21857E-01      15   0.66669E-08   0.12432E-07 0.12729E+00 
c  r12          0.93848E-03      18   0.56407E-08   0.29584E-09 0.60523E+00 
c  r13          0.46670E-02      19   0.57983E-08   0.15091E-08 0.20075E+00 
c  r23          0.39971E-02      19   0.60885E-08   0.12551E-08 0.19776E+00 
c  epsilon      0.10970E+02      11   0.35621E-08   0.98946E-02 0.16525E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.83299E-02 0.43111E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338         0.61354       0.0052548       0.0015074
v  Velocity[Y]             -0.5735         0.54423       0.0030793      0.00087323
v  Velocity[Z]              1.5653          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4373          4.3406          4.3632
v  Pressure                -36.405          360.02          87.641          169.85
v  r11                   0.0010595        0.081855         0.01307        0.018284
v  r22                   0.0011109        0.082635         0.01335        0.018644
v  r33                   0.0016348         0.17427        0.027243        0.037203
v  r12                   -0.010652         0.01359     -0.00023377     -0.00030928
v  r13                   -0.045565        0.052806      9.2874e-05       0.0010136
v  r23                   -0.046707        0.051193      3.0156e-05      0.00057443
v  epsilon                0.068657          271.15          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9908e-05       0.0099177       0.0009245       0.0017425
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017887          5.2775         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001       0.0002096      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71349         0.85283


 TIME FOR THE TIME STEP            10201:        0.82316E+02

===============================================================


 INSTANT    0.102020000E-01   TIME STEP NUMBER           10202
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.800696400E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111564632E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.751921204E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.263685150E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.118188247E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81215E-03   0.45299E-02 0.19962E+01 
c  Velocity[X]                                      0.13841E-03 
c  Velocity[Y]                                      0.12943E-03 
c  Velocity[Z]                                      0.42620E-02 
c  Pressure     0.36339E-04     133   0.92422E-02   0.25633E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56597E-08   0.16672E-08 0.10062E+00 
c  r22          0.10851E-01      13   0.53532E-08   0.18470E-08 0.10228E+00 
c  r33          0.21857E-01      15   0.52593E-08   0.12729E-07 0.12871E+00 
c  r12          0.93848E-03      18   0.57398E-08   0.30100E-09 0.60821E+00 
c  r13          0.46670E-02      19   0.59126E-08   0.14953E-08 0.20052E+00 
c  r23          0.39971E-02      19   0.53630E-08   0.13064E-08 0.20132E+00 
c  epsilon      0.10970E+02      11   0.35368E-08   0.10110E-01 0.16850E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.84602E-02 0.43406E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384          0.6135       0.0052548       0.0015074
v  Velocity[Y]             -0.5735         0.54427       0.0030793      0.00087326
v  Velocity[Z]              1.5653          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4373          4.3406          4.3632
v  Pressure                -36.462          359.97          87.621          169.81
v  r11                   0.0010595         0.08185         0.01307        0.018284
v  r22                   0.0011109        0.082636         0.01335        0.018644
v  r33                   0.0016348         0.17425        0.027243        0.037203
v  r12                    -0.01065        0.013595     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052808      9.2875e-05       0.0010136
v  r23                   -0.046707        0.051217      3.0157e-05      0.00057443
v  epsilon                0.068658          271.12          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9909e-05       0.0099178       0.0009245       0.0017425
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017886          5.2775         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71349         0.85283


 TIME FOR THE TIME STEP            10202:        0.79926E+02

===============================================================


 INSTANT    0.102030000E-01   TIME STEP NUMBER           10203
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106817863E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.426031083E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.348443009E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267893159E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.325289077E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81245E-03   0.45502E-02 0.19974E+01 
c  Velocity[X]                                      0.13891E-03 
c  Velocity[Y]                                      0.12951E-03 
c  Velocity[Z]                                      0.42818E-02 
c  Pressure     0.36451E-04     133   0.92770E-02   0.25712E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54691E-08   0.16246E-08 0.99497E-01 
c  r22          0.10851E-01      13   0.49299E-08   0.18483E-08 0.10193E+00 
c  r33          0.21857E-01      15   0.54074E-08   0.12521E-07 0.12747E+00 
c  r12          0.93848E-03      18   0.51723E-08   0.29945E-09 0.60401E+00 
c  r13          0.46670E-02      19   0.61653E-08   0.15116E-08 0.20060E+00 
c  r23          0.39971E-02      19   0.62008E-08   0.12695E-08 0.19897E+00 
c  epsilon      0.10970E+02      11   0.34010E-08   0.99389E-02 0.16505E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.85058E-02 0.43473E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161986


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61354       0.0052548       0.0015074
v  Velocity[Y]            -0.57367         0.54443       0.0030793      0.00087325
v  Velocity[Z]              1.5653          5.4373          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4373          4.3406          4.3632
v  Pressure                -36.405          360.05          87.659          169.87
v  r11                   0.0010595        0.081858         0.01307        0.018284
v  r22                   0.0011109        0.082639         0.01335        0.018644
v  r33                   0.0016348         0.17427        0.027243        0.037203
v  r12                   -0.010649        0.013591     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052806      9.2875e-05       0.0010136
v  r23                   -0.046707        0.051208      3.0157e-05      0.00057443
v  epsilon                0.068659          271.14          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.991e-05       0.0099178      0.00092451       0.0017425
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017886          5.2782         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71349         0.85283


 TIME FOR THE TIME STEP            10203:        0.81553E+02

===============================================================


 INSTANT    0.102040000E-01   TIME STEP NUMBER           10204
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.723593432E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.194746572E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.577268129E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178869194E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319232807E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81234E-03   0.45155E-02 0.19869E+01 
c  Velocity[X]                                      0.13770E-03 
c  Velocity[Y]                                      0.12842E-03 
c  Velocity[Z]                                      0.42494E-02 
c  Pressure     0.36308E-04     133   0.92495E-02   0.25611E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54396E-08   0.16715E-08 0.10075E+00 
c  r22          0.10851E-01      13   0.45404E-08   0.18488E-08 0.10203E+00 
c  r33          0.21857E-01      15   0.59016E-08   0.12787E-07 0.12885E+00 
c  r12          0.93848E-03      18   0.54321E-08   0.30036E-09 0.60988E+00 
c  r13          0.46670E-02      19   0.56758E-08   0.15013E-08 0.20073E+00 
c  r23          0.39971E-02      19   0.53613E-08   0.12991E-08 0.20211E+00 
c  epsilon      0.10970E+02      11   0.33953E-08   0.10521E-01 0.17383E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.83793E-02 0.43223E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379          0.6135       0.0052548       0.0015074
v  Velocity[Y]            -0.57362         0.54451       0.0030793      0.00087323
v  Velocity[Z]              1.5655          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                -36.512          360.07          87.693           169.9
v  r11                   0.0010595        0.081858         0.01307        0.018284
v  r22                   0.0011109        0.082641         0.01335        0.018644
v  r33                   0.0016348         0.17429        0.027243        0.037203
v  r12                   -0.010655        0.013586     -0.00023377     -0.00030928
v  r13                   -0.045564        0.052807      9.2877e-05       0.0010136
v  r23                   -0.046708        0.051202      3.0158e-05      0.00057443
v  epsilon                 0.06866          271.16          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9911e-05       0.0099179      0.00092451       0.0017425
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017886          5.2785         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71349         0.85283


 TIME FOR THE TIME STEP            10204:        0.82178E+02

===============================================================


 INSTANT    0.102050000E-01   TIME STEP NUMBER           10205
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.428288886E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129998753E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.361646195E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129536115E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.303434320E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81095E-03   0.45466E-02 0.19968E+01 
c  Velocity[X]                                      0.13896E-03 
c  Velocity[Y]                                      0.12933E-03 
c  Velocity[Z]                                      0.42783E-02 
c  Pressure     0.36431E-04     133   0.92748E-02   0.25698E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56795E-08   0.15983E-08 0.99046E-01 
c  r22          0.10851E-01      13   0.46423E-08   0.18063E-08 0.10150E+00 
c  r33          0.21857E-01      14   0.70623E-08   0.12263E-07 0.12686E+00 
c  r12          0.93848E-03      18   0.54842E-08   0.29543E-09 0.60469E+00 
c  r13          0.46670E-02      19   0.55272E-08   0.14787E-08 0.19940E+00 
c  r23          0.39971E-02      19   0.58228E-08   0.12488E-08 0.19731E+00 
c  epsilon      0.10970E+02      11   0.32661E-08   0.96559E-02 0.16373E+00 
c  TempC        0.25716E+06      16   0.15122E-04   0.84009E-02 0.43222E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161987


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61353       0.0052548       0.0015074
v  Velocity[Y]            -0.57364         0.54432       0.0030793      0.00087323
v  Velocity[Z]              1.5655          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4373          4.3406          4.3632
v  Pressure                -36.421          360.06          87.661          169.88
v  r11                   0.0010595        0.081862         0.01307        0.018284
v  r22                   0.0011109        0.082644         0.01335        0.018644
v  r33                   0.0016348         0.17427        0.027243        0.037203
v  r12                   -0.010659         0.01359     -0.00023377     -0.00030928
v  r13                   -0.045563        0.052807      9.2878e-05       0.0010136
v  r23                   -0.046707        0.051224      3.0159e-05      0.00057443
v  epsilon                0.068661          271.16          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9912e-05       0.0099179      0.00092451       0.0017425
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017886          5.2788         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71349         0.85283


 TIME FOR THE TIME STEP            10205:        0.84785E+02

===============================================================


 INSTANT    0.102060000E-01   TIME STEP NUMBER           10206
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.760277962E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.144249304E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.239085261E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.440819933E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208212773E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81216E-03   0.45799E-02 0.20024E+01 
c  Velocity[X]                                      0.13969E-03 
c  Velocity[Y]                                      0.12999E-03 
c  Velocity[Z]                                      0.43102E-02 
c  Pressure     0.36780E-04     132   0.93642E-02   0.25944E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51840E-08   0.16327E-08 0.99797E-01 
c  r22          0.10851E-01      13   0.46470E-08   0.18094E-08 0.10167E+00 
c  r33          0.21857E-01      14   0.68896E-08   0.12450E-07 0.12766E+00 
c  r12          0.93848E-03      18   0.60518E-08   0.29708E-09 0.60606E+00 
c  r13          0.46671E-02      19   0.54889E-08   0.14832E-08 0.20046E+00 
c  r23          0.39971E-02      19   0.58361E-08   0.12943E-08 0.20046E+00 
c  epsilon      0.10970E+02      11   0.33795E-08   0.97355E-02 0.16379E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84125E-02 0.43237E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61349       0.0052548       0.0015074
v  Velocity[Y]            -0.57362         0.54444       0.0030793      0.00087322
v  Velocity[Z]              1.5653          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                -36.486          359.96          87.614           169.8
v  r11                   0.0010595        0.081864         0.01307        0.018284
v  r22                   0.0011109        0.082646         0.01335        0.018644
v  r33                   0.0016347         0.17425        0.027243        0.037203
v  r12                   -0.010666        0.013584     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052807      9.2879e-05       0.0010136
v  r23                   -0.046707         0.05122       3.016e-05      0.00057443
v  epsilon                0.068662          271.12          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9912e-05       0.0099179      0.00092451       0.0017425
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017886          5.2773          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71348         0.85282


 TIME FOR THE TIME STEP            10206:        0.15265E+03

===============================================================


 INSTANT    0.102070000E-01   TIME STEP NUMBER           10207
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108450030E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.324430442E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.198718714E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.217001995E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.246743676E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81275E-03   0.44943E-02 0.19876E+01 
c  Velocity[X]                                      0.13797E-03 
c  Velocity[Y]                                      0.12914E-03 
c  Velocity[Z]                                      0.42272E-02 
c  Pressure     0.35984E-04     133   0.91642E-02   0.25383E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.48786E-08   0.16141E-08 0.99231E-01 
c  r22          0.10851E-01      12   0.65827E-08   0.18155E-08 0.10152E+00 
c  r33          0.21857E-01      14   0.64788E-08   0.12367E-07 0.12696E+00 
c  r12          0.93848E-03      18   0.61243E-08   0.30071E-09 0.60541E+00 
c  r13          0.46671E-02      18   0.69420E-08   0.15060E-08 0.20069E+00 
c  r23          0.39971E-02      19   0.54361E-08   0.12685E-08 0.19811E+00 
c  epsilon      0.10970E+02      11   0.31634E-08   0.98156E-02 0.16456E+00 
c  TempC        0.25716E+06      16   0.15112E-04   0.84405E-02 0.43398E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161987


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379         0.61351       0.0052548       0.0015074
v  Velocity[Y]            -0.57355          0.5444       0.0030793      0.00087321
v  Velocity[Z]              1.5652          5.4373          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4373          4.3406          4.3632
v  Pressure                -36.401          360.03          87.638          169.85
v  r11                   0.0010595        0.081871         0.01307        0.018284
v  r22                   0.0011109        0.082643         0.01335        0.018644
v  r33                   0.0016347         0.17426        0.027243        0.037203
v  r12                   -0.010664        0.013578     -0.00023377     -0.00030928
v  r13                   -0.045564        0.052808       9.288e-05       0.0010136
v  r23                   -0.046705         0.05121       3.016e-05      0.00057443
v  epsilon                0.068662          271.14          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099178      0.00092451       0.0017425
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017886          5.2764         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8764         0.71349         0.85283


 TIME FOR THE TIME STEP            10207:        0.20807E+03

===============================================================


 INSTANT    0.102080000E-01   TIME STEP NUMBER           10208
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.287803428E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.365055899E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934903E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.236851407E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.281131159E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.217220285E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81161E-03   0.45394E-02 0.19960E+01 
c  Velocity[X]                                      0.13887E-03 
c  Velocity[Y]                                      0.12978E-03 
c  Velocity[Z]                                      0.42708E-02 
c  Pressure     0.36806E-04     131   0.93662E-02   0.25964E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55662E-08   0.16031E-08 0.98965E-01 
c  r22          0.10851E-01      13   0.48026E-08   0.18380E-08 0.10182E+00 
c  r33          0.21857E-01      15   0.64976E-08   0.12442E-07 0.12705E+00 
c  r12          0.93848E-03      18   0.60119E-08   0.29472E-09 0.60308E+00 
c  r13          0.46671E-02      19   0.73646E-08   0.15201E-08 0.20056E+00 
c  r23          0.39971E-02      19   0.51777E-08   0.12645E-08 0.19810E+00 
c  epsilon      0.10970E+02      11   0.33513E-08   0.99656E-02 0.16610E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84313E-02 0.43356E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61352       0.0052548       0.0015074
v  Velocity[Y]            -0.57341         0.54446       0.0030792       0.0008732
v  Velocity[Z]              1.5653          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4373          4.3406          4.3632
v  Pressure                 -36.45          360.04          87.673          169.87
v  r11                   0.0010595        0.081872         0.01307        0.018284
v  r22                   0.0011109        0.082645         0.01335        0.018644
v  r33                   0.0016347          0.1743        0.027243        0.037203
v  r12                   -0.010659        0.013577     -0.00023377     -0.00030928
v  r13                   -0.045562         0.05281      9.2881e-05       0.0010136
v  r23                   -0.046704        0.051227      3.0161e-05      0.00057443
v  epsilon                0.068663          271.17          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099178      0.00092451       0.0017425
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017885           5.277         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71349         0.85283


 TIME FOR THE TIME STEP            10208:        0.86241E+02

===============================================================


 INSTANT    0.102090000E-01   TIME STEP NUMBER           10209
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249849639E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.298971775E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.189353901E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.260822504E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111746770E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81143E-03   0.45387E-02 0.19946E+01 
c  Velocity[X]                                      0.13933E-03 
c  Velocity[Y]                                      0.12854E-03 
c  Velocity[Z]                                      0.42709E-02 
c  Pressure     0.36366E-04     131   0.92627E-02   0.25653E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.63061E-08   0.16203E-08 0.99370E-01 
c  r22          0.10851E-01      13   0.51990E-08   0.18115E-08 0.10115E+00 
c  r33          0.21857E-01      15   0.66226E-08   0.12382E-07 0.12680E+00 
c  r12          0.93848E-03      18   0.56620E-08   0.29770E-09 0.60841E+00 
c  r13          0.46671E-02      20   0.75645E-08   0.14833E-08 0.19867E+00 
c  r23          0.39971E-02      18   0.69346E-08   0.12855E-08 0.19935E+00 
c  epsilon      0.10970E+02      11   0.33899E-08   0.97061E-02 0.16302E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84321E-02 0.43318E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61353       0.0052548       0.0015074
v  Velocity[Y]            -0.57363         0.54453       0.0030793      0.00087323
v  Velocity[Z]              1.5654          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                -36.419          360.08           87.68           169.9
v  r11                   0.0010595        0.081878         0.01307        0.018284
v  r22                   0.0011109        0.082647         0.01335        0.018644
v  r33                   0.0016347         0.17429        0.027243        0.037203
v  r12                   -0.010655        0.013583     -0.00023377     -0.00030928
v  r13                   -0.045563        0.052809      9.2882e-05       0.0010136
v  r23                   -0.046703        0.051214      3.0161e-05      0.00057443
v  epsilon                0.068664          271.15          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099178      0.00092451       0.0017425
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017885           5.278         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85283


 TIME FOR THE TIME STEP            10209:        0.89191E+02

===============================================================


 INSTANT    0.102100000E-01   TIME STEP NUMBER           10210
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.131226852E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.137702053E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.421284407E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203050190E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.152371960E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81262E-03   0.45475E-02 0.19947E+01 
c  Velocity[X]                                      0.13845E-03 
c  Velocity[Y]                                      0.12960E-03 
c  Velocity[Z]                                      0.42794E-02 
c  Pressure     0.36683E-04     133   0.93381E-02   0.25876E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.68145E-08   0.16325E-08 0.99537E-01 
c  r22          0.10851E-01      13   0.57207E-08   0.18128E-08 0.10131E+00 
c  r33          0.21857E-01      15   0.73004E-08   0.12496E-07 0.12729E+00 
c  r12          0.93848E-03      18   0.56164E-08   0.29569E-09 0.60583E+00 
c  r13          0.46671E-02      21   0.61999E-08   0.14959E-08 0.19986E+00 
c  r23          0.39971E-02      19   0.55334E-08   0.12909E-08 0.20022E+00 
c  epsilon      0.10970E+02      11   0.33936E-08   0.10232E-01 0.17053E+00 
c  TempC        0.25716E+06      16   0.15125E-04   0.84163E-02 0.43231E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383          0.6135       0.0052548       0.0015074
v  Velocity[Y]            -0.57355         0.54428       0.0030793      0.00087319
v  Velocity[Z]              1.5653          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4373          4.3406          4.3632
v  Pressure                 -36.49          360.02          87.663          169.86
v  r11                   0.0010594        0.081875         0.01307        0.018284
v  r22                   0.0011109        0.082649         0.01335        0.018644
v  r33                   0.0016347         0.17425        0.027243        0.037203
v  r12                   -0.010658        0.013579     -0.00023377     -0.00030928
v  r13                   -0.045565         0.05281      9.2883e-05       0.0010136
v  r23                   -0.046702        0.051209      3.0162e-05      0.00057443
v  epsilon                0.068665          271.13          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099177      0.00092451       0.0017425
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017885           5.279         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71349         0.85283


 TIME FOR THE TIME STEP            10210:        0.89206E+02

===============================================================


 INSTANT    0.102110000E-01   TIME STEP NUMBER           10211
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162278196E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183899856E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.261997739E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.699217289E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.183238352E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81184E-03   0.45450E-02 0.19979E+01 
c  Velocity[X]                                      0.13861E-03 
c  Velocity[Y]                                      0.12909E-03 
c  Velocity[Z]                                      0.42773E-02 
c  Pressure     0.36580E-04     133   0.93115E-02   0.25803E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.62970E-08   0.16363E-08 0.99621E-01 
c  r22          0.10851E-01      13   0.62424E-08   0.18390E-08 0.10161E+00 
c  r33          0.21857E-01      15   0.66514E-08   0.12568E-07 0.12719E+00 
c  r12          0.93848E-03      18   0.63232E-08   0.29464E-09 0.60477E+00 
c  r13          0.46671E-02      20   0.71793E-08   0.15000E-08 0.19976E+00 
c  r23          0.39971E-02      19   0.59846E-08   0.12686E-08 0.19802E+00 
c  epsilon      0.10970E+02      11   0.34194E-08   0.99829E-02 0.16454E+00 
c  TempC        0.25716E+06      16   0.15127E-04   0.84378E-02 0.43354E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61355       0.0052548       0.0015074
v  Velocity[Y]            -0.57357         0.54437       0.0030794      0.00087324
v  Velocity[Z]              1.5654          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                -36.385          360.02          87.657          169.85
v  r11                   0.0010594        0.081874         0.01307        0.018284
v  r22                   0.0011109        0.082649         0.01335        0.018644
v  r33                   0.0016347         0.17427        0.027243        0.037203
v  r12                   -0.010656        0.013574     -0.00023377     -0.00030928
v  r13                   -0.045563        0.052809      9.2885e-05       0.0010136
v  r23                   -0.046701         0.05123      3.0163e-05      0.00057443
v  epsilon                0.068666          271.13          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099177      0.00092452       0.0017425
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017884          5.2795         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8795         0.71349         0.85283


 TIME FOR THE TIME STEP            10211:        0.87634E+02

===============================================================


 INSTANT    0.102120000E-01   TIME STEP NUMBER           10212
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.968494648E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.139548236E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.617932572E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.166798474E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.132551918E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81202E-03   0.45361E-02 0.19930E+01 
c  Velocity[X]                                      0.13906E-03 
c  Velocity[Y]                                      0.12941E-03 
c  Velocity[Z]                                      0.42676E-02 
c  Pressure     0.36578E-04     133   0.93107E-02   0.25802E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.63399E-08   0.16247E-08 0.99308E-01 
c  r22          0.10851E-01      13   0.58312E-08   0.18234E-08 0.10150E+00 
c  r33          0.21857E-01      15   0.74507E-08   0.12504E-07 0.12711E+00 
c  r12          0.93848E-03      18   0.62045E-08   0.29985E-09 0.60630E+00 
c  r13          0.46671E-02      20   0.61255E-08   0.14983E-08 0.19998E+00 
c  r23          0.39971E-02      19   0.64190E-08   0.12811E-08 0.19897E+00 
c  epsilon      0.10970E+02      11   0.36444E-08   0.10040E-01 0.16605E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.84944E-02 0.43491E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61354       0.0052548       0.0015073
v  Velocity[Y]            -0.57351         0.54447       0.0030793      0.00087323
v  Velocity[Z]              1.5655          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4373          4.3406          4.3632
v  Pressure                -36.475          360.03          87.665          169.86
v  r11                   0.0010594        0.081872         0.01307        0.018284
v  r22                   0.0011109        0.082649         0.01335        0.018644
v  r33                   0.0016347          0.1743        0.027243        0.037203
v  r12                   -0.010655        0.013577     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052809      9.2886e-05       0.0010136
v  r23                   -0.046702        0.051221      3.0163e-05      0.00057443
v  epsilon                0.068667          271.15          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099176      0.00092452       0.0017425
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017884          5.2791         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71349         0.85282


 TIME FOR THE TIME STEP            10212:        0.85671E+02

===============================================================


 INSTANT    0.102130000E-01   TIME STEP NUMBER           10213
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141975425E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.128092163E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.962829725E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.989634236E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138275941E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81263E-03   0.45237E-02 0.19914E+01 
c  Velocity[X]                                      0.13823E-03 
c  Velocity[Y]                                      0.12951E-03 
c  Velocity[Z]                                      0.42559E-02 
c  Pressure     0.36294E-04     132   0.92402E-02   0.25602E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.65338E-08   0.16252E-08 0.99438E-01 
c  r22          0.10851E-01      13   0.57686E-08   0.18130E-08 0.10154E+00 
c  r33          0.21857E-01      15   0.65538E-08   0.12410E-07 0.12717E+00 
c  r12          0.93848E-03      18   0.59753E-08   0.30405E-09 0.60950E+00 
c  r13          0.46671E-02      20   0.61810E-08   0.15056E-08 0.20021E+00 
c  r23          0.39971E-02      19   0.65283E-08   0.12818E-08 0.19868E+00 
c  epsilon      0.10970E+02      11   0.34801E-08   0.97767E-02 0.16472E+00 
c  TempC        0.25716E+06      16   0.15102E-04   0.83829E-02 0.43185E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61351       0.0052549       0.0015074
v  Velocity[Y]            -0.57357         0.54414       0.0030793      0.00087322
v  Velocity[Z]              1.5653          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4373          4.3406          4.3632
v  Pressure                 -36.41          360.09          87.678          169.91
v  r11                   0.0010594        0.081877         0.01307        0.018284
v  r22                   0.0011109        0.082645         0.01335        0.018644
v  r33                   0.0016347         0.17427        0.027243        0.037203
v  r12                   -0.010664        0.013577     -0.00023377     -0.00030928
v  r13                   -0.045566        0.052811      9.2887e-05       0.0010136
v  r23                   -0.046702        0.051213      3.0164e-05      0.00057443
v  epsilon                0.068668          271.17          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099176      0.00092452       0.0017425
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017884           5.279         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71349         0.85283


 TIME FOR THE TIME STEP            10213:        0.90937E+02

===============================================================


 INSTANT    0.102140000E-01   TIME STEP NUMBER           10214
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.542888517E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.554884873E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934913E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.177737862E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.843764008E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.815503516E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81205E-03   0.45845E-02 0.20031E+01 
c  Velocity[X]                                      0.13832E-03 
c  Velocity[Y]                                      0.12923E-03 
c  Velocity[Z]                                      0.43169E-02 
c  Pressure     0.36469E-04     132   0.92798E-02   0.25726E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.66390E-08   0.15884E-08 0.98660E-01 
c  r22          0.10851E-01      13   0.53874E-08   0.18019E-08 0.10117E+00 
c  r33          0.21857E-01      15   0.64705E-08   0.12223E-07 0.12644E+00 
c  r12          0.93848E-03      18   0.60991E-08   0.29917E-09 0.60722E+00 
c  r13          0.46671E-02      20   0.60426E-08   0.14787E-08 0.19937E+00 
c  r23          0.39971E-02      19   0.64868E-08   0.12582E-08 0.19746E+00 
c  epsilon      0.10970E+02      11   0.35352E-08   0.94899E-02 0.16295E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.84399E-02 0.43319E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61354       0.0052549       0.0015074
v  Velocity[Y]            -0.57345         0.54416       0.0030793      0.00087321
v  Velocity[Z]              1.5653          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4373          4.3406          4.3632
v  Pressure                -36.467          359.98          87.649          169.83
v  r11                   0.0010594        0.081894         0.01307        0.018284
v  r22                   0.0011109        0.082647         0.01335        0.018644
v  r33                   0.0016347         0.17425        0.027243        0.037203
v  r12                   -0.010663        0.013577     -0.00023377     -0.00030928
v  r13                   -0.045563        0.052812      9.2887e-05       0.0010136
v  r23                   -0.046703        0.051223      3.0165e-05      0.00057443
v  epsilon                0.068669          271.13          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9911e-05       0.0099175      0.00092452       0.0017425
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017884          5.2793         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8793         0.71349         0.85283


 TIME FOR THE TIME STEP            10214:        0.90761E+02

===============================================================


 INSTANT    0.102150000E-01   TIME STEP NUMBER           10215
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282203320E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.244407595E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.355379395E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.241391851E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.550844211E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81117E-03   0.45181E-02 0.19903E+01 
c  Velocity[X]                                      0.13903E-03 
c  Velocity[Y]                                      0.12895E-03 
c  Velocity[Z]                                      0.42502E-02 
c  Pressure     0.36221E-04     132   0.92227E-02   0.25550E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.67925E-08   0.16080E-08 0.98912E-01 
c  r22          0.10851E-01      13   0.51996E-08   0.18037E-08 0.10107E+00 
c  r33          0.21857E-01      15   0.64382E-08   0.12368E-07 0.12665E+00 
c  r12          0.93848E-03      18   0.61830E-08   0.29151E-09 0.60047E+00 
c  r13          0.46671E-02      20   0.55372E-08   0.14932E-08 0.20001E+00 
c  r23          0.39971E-02      19   0.64963E-08   0.12635E-08 0.19706E+00 
c  epsilon      0.10970E+02      11   0.35688E-08   0.98170E-02 0.16473E+00 
c  TempC        0.25716E+06      16   0.15100E-04   0.84567E-02 0.43364E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63377         0.61353       0.0052548       0.0015073
v  Velocity[Y]            -0.57363         0.54432       0.0030793       0.0008732
v  Velocity[Z]              1.5653          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4373          4.3406          4.3632
v  Pressure                -36.372          360.08          87.699          169.91
v  r11                   0.0010594          0.0819         0.01307        0.018284
v  r22                   0.0011109        0.082648         0.01335        0.018644
v  r33                   0.0016347         0.17428        0.027243        0.037203
v  r12                   -0.010661        0.013583     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052808      9.2889e-05       0.0010136
v  r23                   -0.046703        0.051203      3.0165e-05      0.00057444
v  epsilon                 0.06867          271.14          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9912e-05       0.0099175      0.00092452       0.0017425
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017884          5.2794         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8794         0.71349         0.85282


 TIME FOR THE TIME STEP            10215:        0.89835E+02

===============================================================


 INSTANT    0.102160000E-01   TIME STEP NUMBER           10216
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141240157E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.213785880E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182602151E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179194092E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.892156224E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81265E-03   0.45122E-02 0.19886E+01 
c  Velocity[X]                                      0.13808E-03 
c  Velocity[Y]                                      0.12934E-03 
c  Velocity[Z]                                      0.42448E-02 
c  Pressure     0.36718E-04     133   0.93458E-02   0.25901E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.66607E-08   0.16688E-08 0.10053E+00 
c  r22          0.10851E-01      13   0.55355E-08   0.18499E-08 0.10184E+00 
c  r33          0.21857E-01      15   0.57676E-08   0.12790E-07 0.12832E+00 
c  r12          0.93848E-03      19   0.57410E-08   0.30259E-09 0.60732E+00 
c  r13          0.46671E-02      19   0.71838E-08   0.15274E-08 0.20061E+00 
c  r23          0.39971E-02      19   0.54578E-08   0.13081E-08 0.20100E+00 
c  epsilon      0.10970E+02      11   0.35648E-08   0.10648E-01 0.17413E+00 
c  TempC        0.25716E+06      16   0.15166E-04   0.83737E-02 0.43219E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61351       0.0052549       0.0015074
v  Velocity[Y]            -0.57353         0.54444       0.0030793      0.00087322
v  Velocity[Z]              1.5654          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                -36.456          360.07          87.687          169.89
v  r11                   0.0010594        0.081907         0.01307        0.018284
v  r22                   0.0011109        0.082649        0.013351        0.018644
v  r33                   0.0016347          0.1743        0.027243        0.037203
v  r12                   -0.010657        0.013579     -0.00023377     -0.00030928
v  r13                   -0.045565        0.052808       9.289e-05       0.0010136
v  r23                   -0.046704        0.051183      3.0166e-05      0.00057444
v  epsilon                0.068671          271.16          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9912e-05       0.0099175      0.00092452       0.0017425
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017884          5.2792         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8792         0.71349         0.85283


 TIME FOR THE TIME STEP            10216:        0.91028E+02

===============================================================


 INSTANT    0.102170000E-01   TIME STEP NUMBER           10217
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106900921E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.301989202E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.759201635E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.177171276E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195526579E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81125E-03   0.45595E-02 0.20003E+01 
c  Velocity[X]                                      0.13915E-03 
c  Velocity[Y]                                      0.12940E-03 
c  Velocity[Z]                                      0.42909E-02 
c  Pressure     0.36661E-04     132   0.93279E-02   0.25861E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.65218E-08   0.16422E-08 0.99655E-01 
c  r22          0.10851E-01      13   0.54270E-08   0.18473E-08 0.10182E+00 
c  r33          0.21857E-01      15   0.53185E-08   0.12598E-07 0.12747E+00 
c  r12          0.93848E-03      19   0.58344E-08   0.29514E-09 0.60319E+00 
c  r13          0.46671E-02      20   0.58759E-08   0.15120E-08 0.20023E+00 
c  r23          0.39971E-02      19   0.61737E-08   0.12897E-08 0.19933E+00 
c  epsilon      0.10970E+02      11   0.33694E-08   0.10292E-01 0.16854E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.84040E-02 0.43288E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61353       0.0052549       0.0015074
v  Velocity[Y]             -0.5735         0.54423       0.0030794      0.00087325
v  Velocity[Z]              1.5656          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4373          4.3406          4.3632
v  Pressure                -36.419          360.04          87.658          169.86
v  r11                   0.0010594        0.081909         0.01307        0.018284
v  r22                   0.0011109        0.082649        0.013351        0.018644
v  r33                   0.0016347         0.17429        0.027243        0.037203
v  r12                   -0.010654        0.013575     -0.00023377     -0.00030928
v  r13                   -0.045563        0.052809      9.2891e-05       0.0010136
v  r23                   -0.046704        0.051204      3.0167e-05      0.00057444
v  epsilon                0.068672          271.18          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099175      0.00092452       0.0017425
v  CourantNb               0.44215             0.6         0.59908         0.59839
v  FourierNb             0.0017884          5.2798         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8798         0.71349         0.85283


 TIME FOR THE TIME STEP            10217:        0.87832E+02

===============================================================


 INSTANT    0.102180000E-01   TIME STEP NUMBER           10218
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.314616987E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.245607726E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934878E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.503756664E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.935353820E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162749375E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81309E-03   0.45516E-02 0.19975E+01 
c  Velocity[X]                                      0.13856E-03 
c  Velocity[Y]                                      0.13018E-03 
c  Velocity[Z]                                      0.42829E-02 
c  Pressure     0.36763E-04     134   0.93639E-02   0.25933E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.65358E-08   0.16292E-08 0.99872E-01 
c  r22          0.10851E-01      13   0.50189E-08   0.18163E-08 0.10150E+00 
c  r33          0.21857E-01      15   0.58217E-08   0.12427E-07 0.12708E+00 
c  r12          0.93848E-03      19   0.57959E-08   0.30555E-09 0.61363E+00 
c  r13          0.46671E-02      20   0.62633E-08   0.15076E-08 0.20064E+00 
c  r23          0.39971E-02      19   0.57901E-08   0.12669E-08 0.19845E+00 
c  epsilon      0.10970E+02      11   0.32241E-08   0.99142E-02 0.16494E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.84999E-02 0.43470E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61353       0.0052549       0.0015074
v  Velocity[Y]            -0.57348         0.54434       0.0030793      0.00087321
v  Velocity[Z]              1.5658          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4373          4.3406          4.3632
v  Pressure                -36.451          360.11          87.729          169.94
v  r11                   0.0010594        0.081907         0.01307        0.018284
v  r22                   0.0011109        0.082651        0.013351        0.018644
v  r33                   0.0016347         0.17427        0.027243        0.037203
v  r12                   -0.010651        0.013582     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052809      9.2892e-05       0.0010136
v  r23                   -0.046705        0.051194      3.0167e-05      0.00057444
v  epsilon                0.068673          271.15          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099176      0.00092452       0.0017425
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017883          5.2798         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8798         0.71349         0.85283


 TIME FOR THE TIME STEP            10218:        0.90576E+02

===============================================================


 INSTANT    0.102190000E-01   TIME STEP NUMBER           10219
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.942251672E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.862174806E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.905777133E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.102706946E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.635030250E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81256E-03   0.44999E-02 0.19880E+01 
c  Velocity[X]                                      0.13811E-03 
c  Velocity[Y]                                      0.12875E-03 
c  Velocity[Z]                                      0.42331E-02 
c  Pressure     0.36058E-04     133   0.91844E-02   0.25434E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.63542E-08   0.16250E-08 0.99274E-01 
c  r22          0.10851E-01      13   0.50535E-08   0.18143E-08 0.10114E+00 
c  r33          0.21857E-01      15   0.60788E-08   0.12417E-07 0.12644E+00 
c  r12          0.93848E-03      19   0.56460E-08   0.29736E-09 0.60516E+00 
c  r13          0.46671E-02      20   0.60796E-08   0.15147E-08 0.20031E+00 
c  r23          0.39971E-02      19   0.52692E-08   0.12680E-08 0.19763E+00 
c  epsilon      0.10970E+02      11   0.32307E-08   0.98974E-02 0.16470E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84251E-02 0.43290E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61353       0.0052549       0.0015073
v  Velocity[Y]            -0.57356         0.54403       0.0030793       0.0008732
v  Velocity[Z]              1.5656          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4373          4.3406          4.3632
v  Pressure                -36.384          360.09          87.687          169.91
v  r11                   0.0010594        0.081906         0.01307        0.018284
v  r22                   0.0011109        0.082647        0.013351        0.018644
v  r33                   0.0016347         0.17428        0.027243        0.037203
v  r12                   -0.010648        0.013581     -0.00023377     -0.00030928
v  r13                   -0.045563        0.052808      9.2894e-05       0.0010136
v  r23                   -0.046705         0.05118      3.0169e-05      0.00057444
v  epsilon                0.068674          271.17          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099177      0.00092453       0.0017425
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017883          5.2793         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8793         0.71349         0.85283


 TIME FOR THE TIME STEP            10219:        0.87876E+02

===============================================================


 INSTANT    0.102200000E-01   TIME STEP NUMBER           10220
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.193741828E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.947268242E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.124422607E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.414926023E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.703215291E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81117E-03   0.45331E-02 0.19938E+01 
c  Velocity[X]                                      0.13943E-03 
c  Velocity[Y]                                      0.12939E-03 
c  Velocity[Z]                                      0.42642E-02 
c  Pressure     0.36659E-04     133   0.93283E-02   0.25858E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.62800E-08   0.16197E-08 0.99012E-01 
c  r22          0.10851E-01      13   0.51093E-08   0.18341E-08 0.10152E+00 
c  r33          0.21857E-01      15   0.55493E-08   0.12524E-07 0.12692E+00 
c  r12          0.93848E-03      19   0.58831E-08   0.29260E-09 0.60072E+00 
c  r13          0.46671E-02      20   0.58542E-08   0.15102E-08 0.20042E+00 
c  r23          0.39971E-02      19   0.54265E-08   0.12759E-08 0.19775E+00 
c  epsilon      0.10970E+02      11   0.33783E-08   0.10158E-01 0.16821E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84075E-02 0.43234E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61356       0.0052548       0.0015073
v  Velocity[Y]            -0.57351         0.54409       0.0030793      0.00087321
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.398          360.01          87.664          169.86
v  r11                   0.0010594        0.081899         0.01307        0.018284
v  r22                   0.0011109        0.082648        0.013351        0.018644
v  r33                   0.0016347         0.17431        0.027243        0.037203
v  r12                   -0.010649         0.01358     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052809      9.2895e-05       0.0010136
v  r23                   -0.046705        0.051166       3.017e-05      0.00057444
v  epsilon                0.068675           271.2          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099177      0.00092453       0.0017425
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017883          5.2792         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8792         0.71349         0.85283


 TIME FOR THE TIME STEP            10220:        0.88757E+02

===============================================================


 INSTANT    0.102210000E-01   TIME STEP NUMBER           10221
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106482877E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.444704892E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153971394E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.262181306E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199692147E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81213E-03   0.45454E-02 0.19959E+01 
c  Velocity[X]                                      0.13998E-03 
c  Velocity[Y]                                      0.12911E-03 
c  Velocity[Z]                                      0.42763E-02 
c  Pressure     0.36596E-04     134   0.93184E-02   0.25816E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59064E-08   0.16449E-08 0.99575E-01 
c  r22          0.10851E-01      13   0.54133E-08   0.18288E-08 0.10146E+00 
c  r33          0.21857E-01      15   0.70583E-08   0.12512E-07 0.12709E+00 
c  r12          0.93848E-03      19   0.58978E-08   0.29844E-09 0.60478E+00 
c  r13          0.46671E-02      20   0.64477E-08   0.14946E-08 0.19977E+00 
c  r23          0.39971E-02      19   0.62729E-08   0.12965E-08 0.19873E+00 
c  epsilon      0.10970E+02      11   0.34543E-08   0.10016E-01 0.16613E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84414E-02 0.43357E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61357       0.0052548       0.0015073
v  Velocity[Y]            -0.57364         0.54423       0.0030794      0.00087327
v  Velocity[Z]              1.5651          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4374          4.3406          4.3632
v  Pressure                -36.386          360.05          87.695           169.9
v  r11                   0.0010594        0.081895         0.01307        0.018284
v  r22                   0.0011109        0.082649        0.013351        0.018644
v  r33                   0.0016347         0.17431        0.027243        0.037203
v  r12                   -0.010646        0.013582     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052808      9.2896e-05       0.0010136
v  r23                   -0.046704        0.051196      3.0171e-05      0.00057444
v  epsilon                0.068676          271.19          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099178      0.00092453       0.0017425
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017883          5.2786         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71349         0.85282


 TIME FOR THE TIME STEP            10221:        0.88064E+02

===============================================================


 INSTANT    0.102220000E-01   TIME STEP NUMBER           10222
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.456757013E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69792E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.120997063E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69792E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.277743967E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935016E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69792E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.136505952E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69792E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.234512423E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69792E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81309E-03   0.45373E-02 0.19922E+01 
c  Velocity[X]                                      0.13798E-03 
c  Velocity[Y]                                      0.12950E-03 
c  Velocity[Z]                                      0.42698E-02 
c  Pressure     0.36500E-04     133   0.92883E-02   0.25746E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.61958E-08   0.16339E-08 0.99539E-01 
c  r22          0.10851E-01      13   0.53280E-08   0.18418E-08 0.10208E+00 
c  r33          0.21857E-01      15   0.68053E-08   0.12564E-07 0.12767E+00 
c  r12          0.93848E-03      19   0.57297E-08   0.29546E-09 0.60535E+00 
c  r13          0.46671E-02      20   0.65058E-08   0.15100E-08 0.20103E+00 
c  r23          0.39971E-02      19   0.61192E-08   0.12846E-08 0.19888E+00 
c  epsilon      0.10970E+02      11   0.34628E-08   0.10005E-01 0.16610E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.83674E-02 0.43150E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63377         0.61355       0.0052548       0.0015073
v  Velocity[Y]            -0.57351         0.54441       0.0030794      0.00087326
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.467          360.04          87.669          169.87
v  r11                   0.0010594        0.081896         0.01307        0.018284
v  r22                   0.0011109         0.08265        0.013351        0.018644
v  r33                   0.0016347         0.17427        0.027243        0.037203
v  r12                   -0.010648         0.01358     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052808      9.2896e-05       0.0010136
v  r23                   -0.046703        0.051197      3.0171e-05      0.00057444
v  epsilon                0.068678          271.18          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05       0.0099177      0.00092453       0.0017425
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017882          5.2786         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71349         0.85283


 TIME FOR THE TIME STEP            10222:        0.86141E+02

===============================================================


 INSTANT    0.102230000E-01   TIME STEP NUMBER           10223
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.118463842E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227994006E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.297928187E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.457687581E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179165790E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81220E-03   0.45405E-02 0.19948E+01 
c  Velocity[X]                                      0.13764E-03 
c  Velocity[Y]                                      0.12917E-03 
c  Velocity[Z]                                      0.42737E-02 
c  Pressure     0.36308E-04     132   0.92406E-02   0.25612E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.62153E-08   0.16541E-08 0.10015E+00 
c  r22          0.10851E-01      13   0.52076E-08   0.18422E-08 0.10222E+00 
c  r33          0.21857E-01      15   0.61223E-08   0.12746E-07 0.12845E+00 
c  r12          0.93848E-03      18   0.67610E-08   0.29725E-09 0.60671E+00 
c  r13          0.46671E-02      20   0.56994E-08   0.15108E-08 0.20107E+00 
c  r23          0.39971E-02      19   0.55301E-08   0.13145E-08 0.20071E+00 
c  epsilon      0.10970E+02      11   0.33878E-08   0.10398E-01 0.17265E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.84592E-02 0.43435E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61357       0.0052549       0.0015073
v  Velocity[Y]            -0.57366         0.54408       0.0030794      0.00087328
v  Velocity[Z]              1.5656          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4374          4.3406          4.3632
v  Pressure                -36.412          359.97          87.608           169.8
v  r11                   0.0010594        0.081893         0.01307        0.018284
v  r22                   0.0011108        0.082649        0.013351        0.018644
v  r33                   0.0016347         0.17429        0.027243        0.037203
v  r12                   -0.010648        0.013586     -0.00023377     -0.00030928
v  r13                    -0.04556        0.052807      9.2897e-05       0.0010136
v  r23                   -0.046703        0.051184      3.0172e-05      0.00057444
v  epsilon                0.068679          271.17          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099176      0.00092453       0.0017425
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017882          5.2785         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71349         0.85283


 TIME FOR THE TIME STEP            10223:        0.86409E+02

===============================================================


 INSTANT    0.102240000E-01   TIME STEP NUMBER           10224
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.548248427E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.240894714E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.340020538E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.196552446E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.280735349E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69793E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81173E-03   0.45326E-02 0.19954E+01 
c  Velocity[X]                                      0.13877E-03 
c  Velocity[Y]                                      0.12930E-03 
c  Velocity[Z]                                      0.42646E-02 
c  Pressure     0.36870E-04     133   0.93930E-02   0.26008E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59251E-08   0.16443E-08 0.99932E-01 
c  r22          0.10851E-01      13   0.51585E-08   0.18512E-08 0.10216E+00 
c  r33          0.21857E-01      15   0.65011E-08   0.12619E-07 0.12774E+00 
c  r12          0.93848E-03      18   0.69857E-08   0.30212E-09 0.60718E+00 
c  r13          0.46671E-02      19   0.69232E-08   0.15072E-08 0.20062E+00 
c  r23          0.39971E-02      19   0.53947E-08   0.12900E-08 0.19912E+00 
c  epsilon      0.10970E+02      11   0.33803E-08   0.10016E-01 0.16530E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.84472E-02 0.43311E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63372         0.61355       0.0052549       0.0015073
v  Velocity[Y]            -0.57359         0.54409       0.0030794      0.00087325
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.445          360.03          87.664          169.86
v  r11                   0.0010594        0.081888        0.013071        0.018284
v  r22                   0.0011108         0.08265        0.013351        0.018644
v  r33                   0.0016346         0.17432        0.027244        0.037203
v  r12                   -0.010646        0.013583     -0.00023377     -0.00030928
v  r13                    -0.04556        0.052809      9.2898e-05       0.0010136
v  r23                   -0.046702        0.051202      3.0172e-05      0.00057444
v  epsilon                 0.06868          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099177      0.00092453       0.0017425
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017882           5.278         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85283


 TIME FOR THE TIME STEP            10224:        0.87394E+02

===============================================================


 INSTANT    0.102250000E-01   TIME STEP NUMBER           10225
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.358633555E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69792E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239110291E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69792E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.397966701E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69792E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184048898E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69792E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.699730504E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69792E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81177E-03   0.45130E-02 0.19889E+01 
c  Velocity[X]                                      0.13882E-03 
c  Velocity[Y]                                      0.12881E-03 
c  Velocity[Z]                                      0.42454E-02 
c  Pressure     0.36140E-04     133   0.92000E-02   0.25493E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58007E-08   0.16157E-08 0.99187E-01 
c  r22          0.10851E-01      13   0.52104E-08   0.17916E-08 0.10112E+00 
c  r33          0.21857E-01      15   0.64683E-08   0.12320E-07 0.12676E+00 
c  r12          0.93849E-03      18   0.68202E-08   0.29333E-09 0.60160E+00 
c  r13          0.46671E-02      20   0.61171E-08   0.14782E-08 0.19891E+00 
c  r23          0.39971E-02      19   0.56638E-08   0.12820E-08 0.19878E+00 
c  epsilon      0.10970E+02      11   0.33475E-08   0.95458E-02 0.16236E+00 
c  TempC        0.25716E+06      16   0.15106E-04   0.84079E-02 0.43254E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364         0.61355       0.0052548       0.0015073
v  Velocity[Y]            -0.57361         0.54424       0.0030794      0.00087325
v  Velocity[Z]              1.5656          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4374          4.3406          4.3632
v  Pressure                -36.408          360.12            87.7          169.93
v  r11                   0.0010594        0.081889        0.013071        0.018284
v  r22                   0.0011108        0.082647        0.013351        0.018644
v  r33                   0.0016346          0.1743        0.027244        0.037203
v  r12                   -0.010647         0.01359     -0.00023377     -0.00030928
v  r13                   -0.045564        0.052812      9.2899e-05       0.0010136
v  r23                   -0.046702        0.051186      3.0174e-05      0.00057444
v  epsilon                0.068681           271.2          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099178      0.00092453       0.0017425
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017882          5.2778          0.1144         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71349         0.85282


 TIME FOR THE TIME STEP            10225:        0.87010E+02

===============================================================


 INSTANT    0.102260000E-01   TIME STEP NUMBER           10226
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166777419E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.286976107E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.355633931E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158201478E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149124801E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81297E-03   0.45421E-02 0.19954E+01 
c  Velocity[X]                                      0.13835E-03 
c  Velocity[Y]                                      0.12983E-03 
c  Velocity[Z]                                      0.42740E-02 
c  Pressure     0.37044E-04     133   0.94265E-02   0.26131E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53272E-08   0.16460E-08 0.10031E+00 
c  r22          0.10851E-01      13   0.51357E-08   0.18369E-08 0.10227E+00 
c  r33          0.21857E-01      15   0.62033E-08   0.12579E-07 0.12830E+00 
c  r12          0.93849E-03      18   0.64228E-08   0.30264E-09 0.60731E+00 
c  r13          0.46671E-02      20   0.71912E-08   0.15147E-08 0.20139E+00 
c  r23          0.39971E-02      20   0.62122E-08   0.12900E-08 0.20057E+00 
c  epsilon      0.10970E+02      11   0.32699E-08   0.97222E-02 0.16407E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.84393E-02 0.43346E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61357       0.0052549       0.0015074
v  Velocity[Y]            -0.57363         0.54409       0.0030794      0.00087327
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.431          360.03          87.675          169.86
v  r11                   0.0010594         0.08188        0.013071        0.018284
v  r22                   0.0011108        0.082648        0.013351        0.018644
v  r33                   0.0016346         0.17428        0.027244        0.037203
v  r12                   -0.010651         0.01359     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052812      9.2899e-05       0.0010136
v  r23                   -0.046703        0.051178      3.0174e-05      0.00057444
v  epsilon                0.068682          271.16          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099179      0.00092453       0.0017425
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017881          5.2769         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71349         0.85283


 TIME FOR THE TIME STEP            10226:        0.86131E+02

===============================================================


 INSTANT    0.102270000E-01   TIME STEP NUMBER           10227
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.184170894E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.821916645E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232989107E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.841048261E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.352863096E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81215E-03   0.45474E-02 0.19964E+01 
c  Velocity[X]                                      0.13957E-03 
c  Velocity[Y]                                      0.12943E-03 
c  Velocity[Z]                                      0.42784E-02 
c  Pressure     0.36428E-04     131   0.92776E-02   0.25696E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54604E-08   0.16347E-08 0.99658E-01 
c  r22          0.10851E-01      13   0.51611E-08   0.18223E-08 0.10194E+00 
c  r33          0.21857E-01      15   0.51245E-08   0.12388E-07 0.12702E+00 
c  r12          0.93849E-03      18   0.59410E-08   0.29935E-09 0.60780E+00 
c  r13          0.46671E-02      20   0.58007E-08   0.14708E-08 0.19980E+00 
c  r23          0.39971E-02      20   0.59141E-08   0.12564E-08 0.19719E+00 
c  epsilon      0.10970E+02      11   0.33398E-08   0.97654E-02 0.16533E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.84732E-02 0.43436E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61356       0.0052549       0.0015073
v  Velocity[Y]            -0.57372         0.54421       0.0030796      0.00087333
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.341          360.08          87.691           169.9
v  r11                   0.0010594        0.081873        0.013071        0.018284
v  r22                   0.0011108        0.082651        0.013351        0.018644
v  r33                   0.0016346          0.1743        0.027244        0.037203
v  r12                   -0.010652        0.013596     -0.00023377     -0.00030928
v  r13                    -0.04556        0.052811        9.29e-05       0.0010136
v  r23                   -0.046703        0.051172      3.0175e-05      0.00057444
v  epsilon                0.068683          271.19          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099176      0.00092454       0.0017425
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017881          5.2759         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8759         0.71349         0.85283


 TIME FOR THE TIME STEP            10227:        0.86174E+02

===============================================================


 INSTANT    0.102280000E-01   TIME STEP NUMBER           10228
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.348851743E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232503681E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.387519335E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.286619022E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.504236008E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81289E-03   0.45174E-02 0.19918E+01 
c  Velocity[X]                                      0.13789E-03 
c  Velocity[Y]                                      0.12894E-03 
c  Velocity[Z]                                      0.42505E-02 
c  Pressure     0.36754E-04     133   0.93571E-02   0.25925E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56021E-08   0.16627E-08 0.10038E+00 
c  r22          0.10851E-01      13   0.55201E-08   0.18679E-08 0.10313E+00 
c  r33          0.21857E-01      15   0.60607E-08   0.12834E-07 0.12913E+00 
c  r12          0.93849E-03      18   0.55372E-08   0.30307E-09 0.60622E+00 
c  r13          0.46671E-02      19   0.75298E-08   0.15294E-08 0.20266E+00 
c  r23          0.39971E-02      20   0.57385E-08   0.13086E-08 0.20095E+00 
c  epsilon      0.10970E+02      11   0.35476E-08   0.10105E-01 0.16767E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.83877E-02 0.43263E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61356       0.0052548       0.0015073
v  Velocity[Y]            -0.57357         0.54437       0.0030795      0.00087329
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.422          360.05          87.677          169.88
v  r11                   0.0010594        0.081865        0.013071        0.018284
v  r22                   0.0011108        0.082652        0.013351        0.018644
v  r33                   0.0016346         0.17432        0.027244        0.037203
v  r12                   -0.010654        0.013604     -0.00023377     -0.00030928
v  r13                   -0.045563        0.052809        9.29e-05       0.0010136
v  r23                   -0.046705        0.051206      3.0176e-05      0.00057444
v  epsilon                0.068684          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099176      0.00092454       0.0017425
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017881          5.2759         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8759         0.71349         0.85283


 TIME FOR THE TIME STEP            10228:        0.83735E+02

===============================================================


 INSTANT    0.102290000E-01   TIME STEP NUMBER           10229
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.453637807E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.103285167E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.866446936E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.146028165E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154002589E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      40   0.81096E-03   0.45415E-02 0.19978E+01 
c  Velocity[X]                                      0.13826E-03 
c  Velocity[Y]                                      0.12935E-03 
c  Velocity[Z]                                      0.42739E-02 
c  Pressure     0.36444E-04     133   0.92789E-02   0.25708E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52606E-08   0.16350E-08 0.99802E-01 
c  r22          0.10851E-01      13   0.49679E-08   0.18456E-08 0.10259E+00 
c  r33          0.21857E-01      14   0.65476E-08   0.12544E-07 0.12779E+00 
c  r12          0.93849E-03      18   0.52699E-08   0.29724E-09 0.60488E+00 
c  r13          0.46671E-02      19   0.66336E-08   0.15124E-08 0.20165E+00 
c  r23          0.39971E-02      20   0.58429E-08   0.12867E-08 0.19939E+00 
c  epsilon      0.10970E+02      11   0.33455E-08   0.97486E-02 0.16244E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.83931E-02 0.43174E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63372         0.61357       0.0052549       0.0015073
v  Velocity[Y]            -0.57359          0.5441       0.0030796      0.00087332
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.373          360.03          87.663          169.87
v  r11                   0.0010594        0.081861        0.013071        0.018284
v  r22                   0.0011108        0.082653        0.013351        0.018644
v  r33                   0.0016346         0.17435        0.027244        0.037203
v  r12                   -0.010653        0.013613     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052807      9.2901e-05       0.0010136
v  r23                   -0.046707        0.051201      3.0177e-05      0.00057444
v  epsilon                0.068685          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099177      0.00092454       0.0017425
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017881          5.2763         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8763         0.71349         0.85282


 TIME FOR THE TIME STEP            10229:        0.83640E+02

===============================================================


 INSTANT    0.102300000E-01   TIME STEP NUMBER           10230
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.280210926E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.374550013E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.131002877E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.297212669E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.853671354E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81222E-03   0.45509E-02 0.19973E+01 
c  Velocity[X]                                      0.13910E-03 
c  Velocity[Y]                                      0.12974E-03 
c  Velocity[Z]                                      0.42820E-02 
c  Pressure     0.36729E-04     132   0.93524E-02   0.25908E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.48797E-08   0.16777E-08 0.10097E+00 
c  r22          0.10851E-01      13   0.47088E-08   0.18589E-08 0.10260E+00 
c  r33          0.21857E-01      14   0.69545E-08   0.12886E-07 0.12938E+00 
c  r12          0.93849E-03      18   0.52825E-08   0.30398E-09 0.60966E+00 
c  r13          0.46671E-02      19   0.62582E-08   0.15078E-08 0.20135E+00 
c  r23          0.39971E-02      19   0.68759E-08   0.13035E-08 0.20152E+00 
c  epsilon      0.10970E+02      11   0.32898E-08   0.10596E-01 0.17389E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.84403E-02 0.43302E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61355       0.0052548       0.0015073
v  Velocity[Y]            -0.57355         0.54417       0.0030795      0.00087331
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                 -36.45          360.03           87.68          169.87
v  r11                   0.0010594        0.081868        0.013071        0.018284
v  r22                   0.0011108        0.082654        0.013351        0.018644
v  r33                   0.0016346         0.17433        0.027244        0.037203
v  r12                   -0.010655         0.01361     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052808      9.2903e-05       0.0010136
v  r23                   -0.046709        0.051194      3.0178e-05      0.00057444
v  epsilon                0.068686           271.2          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9919e-05       0.0099177      0.00092454       0.0017425
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017881          5.2765         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765         0.71349         0.85283


 TIME FOR THE TIME STEP            10230:        0.83991E+02

===============================================================


 INSTANT    0.102310000E-01   TIME STEP NUMBER           10231
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.327136873E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.466995819E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200741932E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.101212994E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.386682189E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81239E-03   0.45119E-02 0.19883E+01 
c  Velocity[X]                                      0.13878E-03 
c  Velocity[Y]                                      0.12912E-03 
c  Velocity[Z]                                      0.42440E-02 
c  Pressure     0.35820E-04     134   0.91260E-02   0.25267E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.48759E-08   0.16446E-08 0.99985E-01 
c  r22          0.10851E-01      13   0.48962E-08   0.18461E-08 0.10209E+00 
c  r33          0.21857E-01      14   0.71061E-08   0.12590E-07 0.12747E+00 
c  r12          0.93849E-03      18   0.52551E-08   0.29489E-09 0.60197E+00 
c  r13          0.46671E-02      19   0.60197E-08   0.15087E-08 0.20084E+00 
c  r23          0.39971E-02      19   0.70230E-08   0.12768E-08 0.19879E+00 
c  epsilon      0.10970E+02      11   0.33498E-08   0.10175E-01 0.16723E+00 
c  TempC        0.25716E+06      16   0.15100E-04   0.84066E-02 0.43284E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361         0.61353       0.0052549       0.0015073
v  Velocity[Y]            -0.57359         0.54434       0.0030796      0.00087335
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.418          360.03          87.662          169.86
v  r11                   0.0010593        0.081871        0.013071        0.018284
v  r22                   0.0011108        0.082654        0.013351        0.018644
v  r33                   0.0016346          0.1743        0.027244        0.037203
v  r12                   -0.010656        0.013612     -0.00023377     -0.00030928
v  r13                   -0.045563        0.052809      9.2904e-05       0.0010136
v  r23                   -0.046711        0.051215      3.0179e-05      0.00057444
v  epsilon                0.068687          271.17          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099177      0.00092454       0.0017425
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb              0.001788          5.2775         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71349         0.85282


 TIME FOR THE TIME STEP            10231:        0.80715E+02

===============================================================


 INSTANT    0.102320000E-01   TIME STEP NUMBER           10232
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188997832E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.223337208E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.717203492E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201927810E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.129957155E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81204E-03   0.45167E-02 0.19923E+01 
c  Velocity[X]                                      0.13842E-03 
c  Velocity[Y]                                      0.12985E-03 
c  Velocity[Z]                                      0.42484E-02 
c  Pressure     0.36688E-04     132   0.93331E-02   0.25879E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54242E-08   0.16262E-08 0.99597E-01 
c  r22          0.10851E-01      13   0.54457E-08   0.18213E-08 0.10181E+00 
c  r33          0.21857E-01      14   0.71091E-08   0.12433E-07 0.12715E+00 
c  r12          0.93849E-03      18   0.56775E-08   0.30002E-09 0.60674E+00 
c  r13          0.46671E-02      19   0.65238E-08   0.15111E-08 0.20126E+00 
c  r23          0.39971E-02      19   0.69592E-08   0.12860E-08 0.19905E+00 
c  epsilon      0.10970E+02      11   0.33408E-08   0.96656E-02 0.16269E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.84232E-02 0.43333E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63363         0.61359       0.0052548       0.0015073
v  Velocity[Y]            -0.57347         0.54416       0.0030796      0.00087334
v  Velocity[Z]              1.5651          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4374          4.3406          4.3632
v  Pressure                 -36.45          360.03           87.67          169.87
v  r11                   0.0010593        0.081878        0.013071        0.018284
v  r22                   0.0011108        0.082655        0.013351        0.018644
v  r33                   0.0016346         0.17431        0.027244        0.037203
v  r12                   -0.010655        0.013615     -0.00023377     -0.00030928
v  r13                    -0.04556        0.052811      9.2904e-05       0.0010136
v  r23                   -0.046713        0.051204       3.018e-05      0.00057444
v  epsilon                0.068688          271.18          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099177      0.00092454       0.0017425
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb              0.001788          5.2778         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71349         0.85283


 TIME FOR THE TIME STEP            10232:        0.82243E+02

===============================================================


 INSTANT    0.102330000E-01   TIME STEP NUMBER           10233
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.403352884E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.624979775E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.179953136E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.286119150E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190015895E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      45   0.81141E-03   0.45480E-02 0.19968E+01 
c  Velocity[X]                                      0.13920E-03 
c  Velocity[Y]                                      0.12902E-03 
c  Velocity[Z]                                      0.42797E-02 
c  Pressure     0.36363E-04     132   0.92521E-02   0.25651E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52714E-08   0.16215E-08 0.99597E-01 
c  r22          0.10851E-01      13   0.52756E-08   0.18090E-08 0.10181E+00 
c  r33          0.21857E-01      14   0.69928E-08   0.12312E-07 0.12701E+00 
c  r12          0.93849E-03      18   0.51791E-08   0.29670E-09 0.60489E+00 
c  r13          0.46671E-02      19   0.54010E-08   0.14727E-08 0.20009E+00 
c  r23          0.39971E-02      19   0.62234E-08   0.12580E-08 0.19789E+00 
c  epsilon      0.10970E+02      11   0.32486E-08   0.95395E-02 0.16206E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.85106E-02 0.43511E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63366         0.61358       0.0052548       0.0015073
v  Velocity[Y]            -0.57361         0.54427       0.0030796      0.00087336
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.371           360.1          87.693          169.92
v  r11                   0.0010593         0.08188        0.013071        0.018284
v  r22                   0.0011108        0.082651        0.013351        0.018644
v  r33                   0.0016346         0.17435        0.027244        0.037203
v  r12                   -0.010654         0.01361     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052809      9.2906e-05       0.0010136
v  r23                   -0.046714        0.051198      3.0182e-05      0.00057444
v  epsilon                0.068689           271.2          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099176      0.00092454       0.0017425
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb              0.001788          5.2781         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71349         0.85282


 TIME FOR THE TIME STEP            10233:        0.87239E+02

===============================================================


 INSTANT    0.102340000E-01   TIME STEP NUMBER           10234
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.196628091E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.231749808E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.356101729E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136176836E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.356448536E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81259E-03   0.45344E-02 0.19933E+01 
c  Velocity[X]                                      0.13763E-03 
c  Velocity[Y]                                      0.12923E-03 
c  Velocity[Z]                                      0.42676E-02 
c  Pressure     0.36620E-04     133   0.93231E-02   0.25832E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.50272E-08   0.16226E-08 0.99611E-01 
c  r22          0.10851E-01      13   0.53653E-08   0.18144E-08 0.10163E+00 
c  r33          0.21857E-01      14   0.67807E-08   0.12529E-07 0.12770E+00 
c  r12          0.93849E-03      18   0.53356E-08   0.30312E-09 0.60673E+00 
c  r13          0.46671E-02      19   0.57575E-08   0.14961E-08 0.20035E+00 
c  r23          0.39971E-02      19   0.61726E-08   0.12916E-08 0.20048E+00 
c  epsilon      0.10970E+02      11   0.32726E-08   0.98140E-02 0.16454E+00 
c  TempC        0.25716E+06      16   0.15167E-04   0.84104E-02 0.43254E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61355       0.0052549       0.0015073
v  Velocity[Y]            -0.57343         0.54441       0.0030796      0.00087333
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.434          360.03           87.68          169.87
v  r11                   0.0010593        0.081885        0.013071        0.018284
v  r22                   0.0011108        0.082652        0.013351        0.018644
v  r33                   0.0016346         0.17431        0.027244        0.037203
v  r12                   -0.010655        0.013611     -0.00023377     -0.00030928
v  r13                   -0.045563        0.052809      9.2907e-05       0.0010136
v  r23                   -0.046715        0.051221      3.0182e-05      0.00057444
v  epsilon                 0.06869          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099176      0.00092454       0.0017425
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb              0.001788          5.2783         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71349         0.85283


 TIME FOR THE TIME STEP            10234:        0.85108E+02

===============================================================


 INSTANT    0.102350000E-01   TIME STEP NUMBER           10235
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.442010449E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267687291E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.261302618E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.290073944E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.940967558E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81183E-03   0.45314E-02 0.19939E+01 
c  Velocity[X]                                      0.13895E-03 
c  Velocity[Y]                                      0.13015E-03 
c  Velocity[Z]                                      0.42623E-02 
c  Pressure     0.36257E-04     132   0.92325E-02   0.25574E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51986E-08   0.16138E-08 0.99343E-01 
c  r22          0.10851E-01      13   0.50435E-08   0.18211E-08 0.10146E+00 
c  r33          0.21857E-01      15   0.54853E-08   0.12360E-07 0.12657E+00 
c  r12          0.93849E-03      18   0.49478E-08   0.29802E-09 0.60354E+00 
c  r13          0.46671E-02      19   0.55521E-08   0.15094E-08 0.19977E+00 
c  r23          0.39971E-02      19   0.57867E-08   0.12704E-08 0.19812E+00 
c  epsilon      0.10970E+02      11   0.32888E-08   0.96365E-02 0.16190E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.84068E-02 0.43237E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61363       0.0052548       0.0015073
v  Velocity[Y]            -0.57341          0.5441       0.0030797      0.00087339
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.384          360.05           87.68          169.88
v  r11                   0.0010593        0.081895        0.013071        0.018284
v  r22                   0.0011108        0.082652        0.013351        0.018644
v  r33                   0.0016346         0.17429        0.027244        0.037203
v  r12                   -0.010657        0.013619     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052807      9.2908e-05       0.0010136
v  r23                   -0.046715        0.051203      3.0183e-05      0.00057444
v  epsilon                0.068691          271.17          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099177      0.00092455       0.0017425
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb              0.001788          5.2784         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71349         0.85283


 TIME FOR THE TIME STEP            10235:        0.86799E+02

===============================================================


 INSTANT    0.102360000E-01   TIME STEP NUMBER           10236
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.323021705E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158628106E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.164320881E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.344367319E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.812603607E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81189E-03   0.45105E-02 0.19905E+01 
c  Velocity[X]                                      0.13957E-03 
c  Velocity[Y]                                      0.12897E-03 
c  Velocity[Z]                                      0.42420E-02 
c  Pressure     0.36476E-04     131   0.92871E-02   0.25731E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51929E-08   0.16413E-08 0.99535E-01 
c  r22          0.10851E-01      13   0.56437E-08   0.18340E-08 0.10207E+00 
c  r33          0.21857E-01      15   0.56396E-08   0.12606E-07 0.12769E+00 
c  r12          0.93849E-03      18   0.58508E-08   0.30436E-09 0.60621E+00 
c  r13          0.46671E-02      19   0.66958E-08   0.15113E-08 0.20156E+00 
c  r23          0.39971E-02      19   0.62541E-08   0.12931E-08 0.19965E+00 
c  epsilon      0.10970E+02      11   0.34167E-08   0.10053E-01 0.16569E+00 
c  TempC        0.25716E+06      16   0.15181E-04   0.84388E-02 0.43327E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373          0.6136       0.0052549       0.0015073
v  Velocity[Y]             -0.5734         0.54415       0.0030796      0.00087337
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.461          360.06          87.681          169.89
v  r11                   0.0010593          0.0819        0.013071        0.018284
v  r22                   0.0011108        0.082653        0.013351        0.018644
v  r33                   0.0016346          0.1743        0.027244        0.037203
v  r12                   -0.010657        0.013615     -0.00023377     -0.00030928
v  r13                    -0.04556        0.052808      9.2909e-05       0.0010136
v  r23                   -0.046716        0.051188      3.0184e-05      0.00057444
v  epsilon                0.068692           271.2          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099177      0.00092455       0.0017425
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017879          5.2772         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71349         0.85283


 TIME FOR THE TIME STEP            10236:        0.88184E+02

===============================================================


 INSTANT    0.102370000E-01   TIME STEP NUMBER           10237
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168173290E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.592263364E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.362094022E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.367435282E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.164839805E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      40   0.81216E-03   0.45086E-02 0.19889E+01 
c  Velocity[X]                                      0.13801E-03 
c  Velocity[Y]                                      0.12824E-03 
c  Velocity[Z]                                      0.42424E-02 
c  Pressure     0.35837E-04     131   0.91287E-02   0.25280E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.50109E-08   0.16753E-08 0.10048E+00 
c  r22          0.10851E-01      13   0.51301E-08   0.18295E-08 0.10178E+00 
c  r33          0.21857E-01      15   0.55740E-08   0.12658E-07 0.12805E+00 
c  r12          0.93849E-03      18   0.55556E-08   0.31073E-09 0.61094E+00 
c  r13          0.46671E-02      19   0.61371E-08   0.14876E-08 0.19977E+00 
c  r23          0.39971E-02      19   0.66551E-08   0.13012E-08 0.20051E+00 
c  epsilon      0.10970E+02      11   0.34147E-08   0.10366E-01 0.17179E+00 
c  TempC        0.25716E+06      16   0.15103E-04   0.83570E-02 0.43166E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61357       0.0052549       0.0015073
v  Velocity[Y]             -0.5734         0.54423       0.0030797      0.00087339
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.413          360.08          87.696          169.91
v  r11                   0.0010593        0.081903        0.013071        0.018284
v  r22                   0.0011108        0.082653        0.013351        0.018644
v  r33                   0.0016346         0.17432        0.027244        0.037203
v  r12                   -0.010655        0.013616     -0.00023377     -0.00030928
v  r13                   -0.045564        0.052807       9.291e-05       0.0010136
v  r23                   -0.046716        0.051222      3.0185e-05      0.00057444
v  epsilon                0.068694          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099177      0.00092455       0.0017425
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017879          5.2774         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71349         0.85283


 TIME FOR THE TIME STEP            10237:        0.86097E+02

===============================================================


 INSTANT    0.102380000E-01   TIME STEP NUMBER           10238
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.250710852E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.351527806E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.264970383E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.269236285E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155139846E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81211E-03   0.45432E-02 0.19961E+01 
c  Velocity[X]                                      0.13845E-03 
c  Velocity[Y]                                      0.13018E-03 
c  Velocity[Z]                                      0.42745E-02 
c  Pressure     0.36889E-04     131   0.93905E-02   0.26021E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.49362E-08   0.16384E-08 0.99789E-01 
c  r22          0.10851E-01      13   0.53470E-08   0.18424E-08 0.10224E+00 
c  r33          0.21857E-01      15   0.58058E-08   0.12603E-07 0.12791E+00 
c  r12          0.93849E-03      18   0.57979E-08   0.29909E-09 0.60385E+00 
c  r13          0.46671E-02      19   0.64408E-08   0.15228E-08 0.20121E+00 
c  r23          0.39971E-02      20   0.62824E-08   0.13055E-08 0.19994E+00 
c  epsilon      0.10970E+02      11   0.32243E-08   0.99762E-02 0.16514E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.84625E-02 0.43436E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364         0.61364       0.0052548       0.0015073
v  Velocity[Y]            -0.57332         0.54438       0.0030796      0.00087334
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.415          359.96          87.631          169.81
v  r11                   0.0010593        0.081902        0.013071        0.018284
v  r22                   0.0011108        0.082652        0.013351        0.018644
v  r33                   0.0016346         0.17434        0.027244        0.037203
v  r12                   -0.010656        0.013621     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052805       9.291e-05       0.0010136
v  r23                   -0.046716        0.051216      3.0185e-05      0.00057444
v  epsilon                0.068695          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099179      0.00092455       0.0017425
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017879          5.2773         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71349         0.85283


 TIME FOR THE TIME STEP            10238:        0.88061E+02

===============================================================


 INSTANT    0.102390000E-01   TIME STEP NUMBER           10239
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.710273586E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.174337228E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.318947998E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.777284679E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.192496688E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81286E-03   0.45536E-02 0.19996E+01 
c  Velocity[X]                                      0.13864E-03 
c  Velocity[Y]                                      0.12896E-03 
c  Velocity[Z]                                      0.42860E-02 
c  Pressure     0.36340E-04     133   0.92507E-02   0.25634E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51066E-08   0.16127E-08 0.99427E-01 
c  r22          0.10851E-01      13   0.52888E-08   0.18309E-08 0.10216E+00 
c  r33          0.21857E-01      15   0.59662E-08   0.12422E-07 0.12767E+00 
c  r12          0.93849E-03      18   0.53916E-08   0.29645E-09 0.60865E+00 
c  r13          0.46671E-02      19   0.58742E-08   0.15002E-08 0.20055E+00 
c  r23          0.39971E-02      20   0.55087E-08   0.12617E-08 0.19849E+00 
c  epsilon      0.10970E+02      11   0.33671E-08   0.94853E-02 0.16177E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.84725E-02 0.43380E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63359         0.61362       0.0052549       0.0015073
v  Velocity[Y]            -0.57349          0.5442       0.0030797      0.00087337
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.398          360.15          87.728          169.96
v  r11                   0.0010593          0.0819        0.013071        0.018284
v  r22                   0.0011108        0.082646        0.013351        0.018644
v  r33                   0.0016346         0.17432        0.027244        0.037203
v  r12                   -0.010657        0.013616     -0.00023377     -0.00030928
v  r13                   -0.045559        0.052806      9.2911e-05       0.0010136
v  r23                   -0.046715        0.051209      3.0186e-05      0.00057444
v  epsilon                0.068696          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099181      0.00092455       0.0017425
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017879           5.278         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85283


 TIME FOR THE TIME STEP            10239:        0.89829E+02

===============================================================


 INSTANT    0.102400000E-01   TIME STEP NUMBER           10240
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.173990545E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.194313576E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.534741680E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.120656640E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.112694235E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      45   0.81277E-03   0.44896E-02 0.19840E+01 
c  Velocity[X]                                      0.13821E-03 
c  Velocity[Y]                                      0.12914E-03 
c  Velocity[Z]                                      0.42222E-02 
c  Pressure     0.36478E-04     133   0.92856E-02   0.25730E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51139E-08   0.16408E-08 0.99651E-01 
c  r22          0.10851E-01      13   0.53152E-08   0.18447E-08 0.10189E+00 
c  r33          0.21857E-01      15   0.66406E-08   0.12650E-07 0.12774E+00 
c  r12          0.93849E-03      18   0.55661E-08   0.30040E-09 0.60529E+00 
c  r13          0.46671E-02      19   0.63056E-08   0.15055E-08 0.20052E+00 
c  r23          0.39971E-02      19   0.67462E-08   0.12882E-08 0.19963E+00 
c  epsilon      0.10970E+02      11   0.33723E-08   0.10081E-01 0.16649E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.83771E-02 0.43160E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63368         0.61358       0.0052549       0.0015073
v  Velocity[Y]            -0.57331          0.5443       0.0030797      0.00087337
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.458          360.04          87.661          169.87
v  r11                   0.0010593        0.081904        0.013071        0.018284
v  r22                   0.0011108        0.082647        0.013351        0.018644
v  r33                   0.0016346         0.17429        0.027244        0.037203
v  r12                   -0.010659        0.013616     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052807      9.2912e-05       0.0010136
v  r23                   -0.046715        0.051204      3.0187e-05      0.00057444
v  epsilon                0.068697           271.2          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099181      0.00092455       0.0017425
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017878           5.278         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85283


 TIME FOR THE TIME STEP            10240:        0.88310E+02

===============================================================


 INSTANT    0.102410000E-01   TIME STEP NUMBER           10241
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151350594E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.210934046E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.937900957E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.205421692E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.238749331E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81142E-03   0.45377E-02 0.19935E+01 
c  Velocity[X]                                      0.13848E-03 
c  Velocity[Y]                                      0.12955E-03 
c  Velocity[Z]                                      0.42697E-02 
c  Pressure     0.35932E-04     132   0.91455E-02   0.25346E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54730E-08   0.16298E-08 0.99700E-01 
c  r22          0.10851E-01      13   0.51502E-08   0.18322E-08 0.10190E+00 
c  r33          0.21858E-01      15   0.64688E-08   0.12496E-07 0.12763E+00 
c  r12          0.93849E-03      18   0.51744E-08   0.29264E-09 0.60363E+00 
c  r13          0.46671E-02      19   0.62819E-08   0.14949E-08 0.20033E+00 
c  r23          0.39971E-02      19   0.63554E-08   0.12689E-08 0.19889E+00 
c  epsilon      0.10970E+02      11   0.34028E-08   0.97415E-02 0.16362E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83537E-02 0.43129E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61365       0.0052549       0.0015073
v  Velocity[Y]            -0.57345         0.54444       0.0030798       0.0008734
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.372             360          87.641          169.83
v  r11                   0.0010593        0.081904        0.013071        0.018284
v  r22                   0.0011108        0.082648        0.013351        0.018644
v  r33                   0.0016346         0.17429        0.027244        0.037203
v  r12                   -0.010661        0.013616     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052805      9.2912e-05       0.0010136
v  r23                   -0.046715         0.05123      3.0189e-05      0.00057444
v  epsilon                0.068698          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9909e-05       0.0099177      0.00092455       0.0017425
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017878           5.278         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85283


 TIME FOR THE TIME STEP            10241:        0.88407E+02

===============================================================


 INSTANT    0.102420000E-01   TIME STEP NUMBER           10242
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.839132273E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.253153162E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.198293007E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.164368944E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.280149270E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81245E-03   0.45813E-02 0.20015E+01 
c  Velocity[X]                                      0.14028E-03 
c  Velocity[Y]                                      0.13012E-03 
c  Velocity[Z]                                      0.43109E-02 
c  Pressure     0.36716E-04     133   0.93523E-02   0.25899E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57984E-08   0.16217E-08 0.99531E-01 
c  r22          0.10851E-01      13   0.50365E-08   0.18177E-08 0.10162E+00 
c  r33          0.21858E-01      15   0.59213E-08   0.12484E-07 0.12730E+00 
c  r12          0.93849E-03      17   0.69687E-08   0.29320E-09 0.60538E+00 
c  r13          0.46671E-02      19   0.59852E-08   0.14910E-08 0.19994E+00 
c  r23          0.39971E-02      19   0.63573E-08   0.12800E-08 0.19909E+00 
c  epsilon      0.10970E+02      11   0.33785E-08   0.97483E-02 0.16301E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.84765E-02 0.43414E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63368         0.61361       0.0052549       0.0015073
v  Velocity[Y]            -0.57331          0.5441       0.0030797      0.00087337
v  Velocity[Z]              1.5652          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.466          360.05          87.682          169.88
v  r11                   0.0010593        0.081907        0.013071        0.018284
v  r22                   0.0011108        0.082648        0.013351        0.018644
v  r33                   0.0016346         0.17432        0.027244        0.037203
v  r12                    -0.01067        0.013612     -0.00023377     -0.00030928
v  r13                    -0.04556        0.052804      9.2913e-05       0.0010136
v  r23                   -0.046714        0.051222      3.0189e-05      0.00057444
v  epsilon                0.068699          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9903e-05       0.0099175      0.00092455       0.0017425
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017878          5.2781         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71349         0.85283


 TIME FOR THE TIME STEP            10242:        0.86903E+02

===============================================================


 INSTANT    0.102430000E-01   TIME STEP NUMBER           10243
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.728859604E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.309119458E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.268200679E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.121970582E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.220435231E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81218E-03   0.44834E-02 0.19836E+01 
c  Velocity[X]                                      0.13755E-03 
c  Velocity[Y]                                      0.12885E-03 
c  Velocity[Z]                                      0.42170E-02 
c  Pressure     0.36107E-04     132   0.91929E-02   0.25469E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.61088E-08   0.16510E-08 0.10032E+00 
c  r22          0.10851E-01      13   0.49347E-08   0.18369E-08 0.10218E+00 
c  r33          0.21858E-01      15   0.62660E-08   0.12700E-07 0.12855E+00 
c  r12          0.93849E-03      18   0.51666E-08   0.29625E-09 0.60559E+00 
c  r13          0.46671E-02      19   0.66961E-08   0.15214E-08 0.20130E+00 
c  r23          0.39971E-02      20   0.55074E-08   0.13094E-08 0.20128E+00 
c  epsilon      0.10970E+02      11   0.33772E-08   0.10198E-01 0.17132E+00 
c  TempC        0.25716E+06      16   0.15121E-04   0.84326E-02 0.43328E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369         0.61359       0.0052549       0.0015073
v  Velocity[Y]            -0.57354         0.54409       0.0030798       0.0008734
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.422          360.09          87.684          169.91
v  r11                   0.0010593        0.081904        0.013071        0.018284
v  r22                   0.0011108        0.082647        0.013351        0.018644
v  r33                   0.0016346          0.1743        0.027244        0.037203
v  r12                   -0.010669        0.013615     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052803      9.2915e-05       0.0010136
v  r23                   -0.046714        0.051217      3.0189e-05      0.00057444
v  epsilon                  0.0687          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9901e-05       0.0099175      0.00092456       0.0017425
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017878          5.2783         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71349         0.85283


 TIME FOR THE TIME STEP            10243:        0.89229E+02

===============================================================


 INSTANT    0.102440000E-01   TIME STEP NUMBER           10244
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.332724955E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.325492982E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136416262E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.468886639E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.416820206E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81180E-03   0.45511E-02 0.19984E+01 
c  Velocity[X]                                      0.13805E-03 
c  Velocity[Y]                                      0.12870E-03 
c  Velocity[Z]                                      0.42844E-02 
c  Pressure     0.36744E-04     131   0.93525E-02   0.25919E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55892E-08   0.16292E-08 0.99653E-01 
c  r22          0.10851E-01      13   0.52433E-08   0.18340E-08 0.10197E+00 
c  r33          0.21858E-01      14   0.68452E-08   0.12450E-07 0.12725E+00 
c  r12          0.93849E-03      18   0.55085E-08   0.29704E-09 0.60883E+00 
c  r13          0.46671E-02      19   0.56606E-08   0.14928E-08 0.19964E+00 
c  r23          0.39971E-02      19   0.69763E-08   0.12798E-08 0.19871E+00 
c  epsilon      0.10970E+02      11   0.31570E-08   0.98856E-02 0.16627E+00 
c  TempC        0.25716E+06      16   0.15174E-04   0.84221E-02 0.43333E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63377         0.61361       0.0052549       0.0015073
v  Velocity[Y]            -0.57362         0.54422       0.0030797      0.00087338
v  Velocity[Z]              1.5654          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                -36.452          359.97          87.619          169.81
v  r11                   0.0010593        0.081903        0.013071        0.018284
v  r22                   0.0011108        0.082645        0.013351        0.018644
v  r33                   0.0016346         0.17426        0.027244        0.037203
v  r12                   -0.010666         0.01361     -0.00023377     -0.00030928
v  r13                    -0.04556        0.052802      9.2916e-05       0.0010136
v  r23                   -0.046713        0.051241       3.019e-05      0.00057444
v  epsilon                0.068701          271.19          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9897e-05       0.0099175      0.00092456       0.0017425
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017878          5.2784         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71349         0.85283


 TIME FOR THE TIME STEP            10244:        0.87477E+02

===============================================================


 INSTANT    0.102450000E-01   TIME STEP NUMBER           10245
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.323841233E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.202551138E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.112519508E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.742053083E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168805610E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81165E-03   0.45615E-02 0.19984E+01 
c  Velocity[X]                                      0.13962E-03 
c  Velocity[Y]                                      0.12967E-03 
c  Velocity[Z]                                      0.42922E-02 
c  Pressure     0.36471E-04     133   0.92939E-02   0.25726E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52250E-08   0.16199E-08 0.99556E-01 
c  r22          0.10851E-01      13   0.52778E-08   0.18023E-08 0.10143E+00 
c  r33          0.21858E-01      14   0.64246E-08   0.12310E-07 0.12686E+00 
c  r12          0.93849E-03      18   0.57376E-08   0.29647E-09 0.60851E+00 
c  r13          0.46671E-02      19   0.63244E-08   0.14650E-08 0.19908E+00 
c  r23          0.39971E-02      20   0.63502E-08   0.12724E-08 0.19858E+00 
c  epsilon      0.10970E+02      10   0.53480E-08   0.94658E-02 0.16178E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.84562E-02 0.43392E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63366          0.6136       0.0052549       0.0015073
v  Velocity[Y]            -0.57375         0.54442       0.0030797      0.00087339
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.378          360.02          87.654          169.86
v  r11                   0.0010593        0.081907        0.013071        0.018284
v  r22                   0.0011108         0.08264        0.013351        0.018644
v  r33                   0.0016346         0.17429        0.027244        0.037203
v  r12                   -0.010661        0.013613     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052804      9.2917e-05       0.0010136
v  r23                   -0.046712        0.051236      3.0191e-05      0.00057444
v  epsilon                0.068702          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9894e-05       0.0099174      0.00092456       0.0017425
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017877          5.2788         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71349         0.85282


 TIME FOR THE TIME STEP            10245:        0.86376E+02

===============================================================


 INSTANT    0.102460000E-01   TIME STEP NUMBER           10246
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.167095971E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.612909210E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.438299274E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.152863696E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.442167923E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81313E-03   0.45353E-02 0.19941E+01 
c  Velocity[X]                                      0.13945E-03 
c  Velocity[Y]                                      0.13040E-03 
c  Velocity[Z]                                      0.42655E-02 
c  Pressure     0.36381E-04     133   0.92574E-02   0.25663E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53244E-08   0.16252E-08 0.99597E-01 
c  r22          0.10851E-01      13   0.51913E-08   0.18409E-08 0.10185E+00 
c  r33          0.21858E-01      14   0.68037E-08   0.12587E-07 0.12753E+00 
c  r12          0.93849E-03      18   0.52079E-08   0.30050E-09 0.60758E+00 
c  r13          0.46671E-02      19   0.55021E-08   0.15349E-08 0.20151E+00 
c  r23          0.39971E-02      19   0.68525E-08   0.12736E-08 0.19862E+00 
c  epsilon      0.10970E+02      11   0.30815E-08   0.10145E-01 0.16772E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.83985E-02 0.43248E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61355       0.0052549       0.0015073
v  Velocity[Y]            -0.57364         0.54412       0.0030797      0.00087337
v  Velocity[Z]              1.5655          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4373          4.3406          4.3632
v  Pressure                 -36.47          360.05          87.675          169.88
v  r11                   0.0010593        0.081914        0.013071        0.018284
v  r22                   0.0011108        0.082641        0.013351        0.018644
v  r33                   0.0016345         0.17432        0.027244        0.037203
v  r12                   -0.010661        0.013616     -0.00023377     -0.00030928
v  r13                   -0.045563        0.052806      9.2918e-05       0.0010136
v  r23                   -0.046711         0.05122      3.0192e-05      0.00057444
v  epsilon                0.068703          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9891e-05       0.0099176      0.00092456       0.0017425
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017877          5.2789         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71349         0.85283


 TIME FOR THE TIME STEP            10246:        0.85855E+02

===============================================================


 INSTANT    0.102470000E-01   TIME STEP NUMBER           10247
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.215333067E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.764079307E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.590297342E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.159396269E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199579807E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81159E-03   0.45217E-02 0.19937E+01 
c  Velocity[X]                                      0.13848E-03 
c  Velocity[Y]                                      0.12948E-03 
c  Velocity[Z]                                      0.42538E-02 
c  Pressure     0.36335E-04     131   0.92524E-02   0.25630E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55983E-08   0.16570E-08 0.10013E+00 
c  r22          0.10851E-01      13   0.50398E-08   0.18174E-08 0.10196E+00 
c  r33          0.21858E-01      14   0.70458E-08   0.12547E-07 0.12764E+00 
c  r12          0.93849E-03      18   0.50207E-08   0.29404E-09 0.60361E+00 
c  r13          0.46671E-02      19   0.56323E-08   0.14925E-08 0.20014E+00 
c  r23          0.39971E-02      19   0.61893E-08   0.12887E-08 0.19919E+00 
c  epsilon      0.10970E+02      11   0.32802E-08   0.98424E-02 0.16512E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.84374E-02 0.43338E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161986


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61364       0.0052549       0.0015073
v  Velocity[Y]            -0.57371         0.54416       0.0030798      0.00087342
v  Velocity[Z]              1.5653          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4373          4.3406          4.3632
v  Pressure                -36.387          360.02          87.651          169.85
v  r11                   0.0010593        0.081916        0.013071        0.018284
v  r22                   0.0011108        0.082641        0.013351        0.018644
v  r33                   0.0016345          0.1743        0.027244        0.037203
v  r12                   -0.010661        0.013613     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052803       9.292e-05       0.0010136
v  r23                    -0.04671        0.051238      3.0193e-05      0.00057444
v  epsilon                0.068704          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.989e-05       0.0099176      0.00092456       0.0017425
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017877          5.2779         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71349         0.85282


 TIME FOR THE TIME STEP            10247:        0.87651E+02

===============================================================


 INSTANT    0.102480000E-01   TIME STEP NUMBER           10248
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.504821331E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154551270E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.345987229E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162753226E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.927631397E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81257E-03   0.45307E-02 0.19930E+01 
c  Velocity[X]                                      0.13912E-03 
c  Velocity[Y]                                      0.12965E-03 
c  Velocity[Z]                                      0.42619E-02 
c  Pressure     0.36333E-04     133   0.92559E-02   0.25629E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58944E-08   0.16345E-08 0.99065E-01 
c  r22          0.10851E-01      13   0.54932E-08   0.18079E-08 0.10103E+00 
c  r33          0.21858E-01      15   0.53082E-08   0.12486E-07 0.12686E+00 
c  r12          0.93849E-03      18   0.62879E-08   0.29506E-09 0.60190E+00 
c  r13          0.46671E-02      19   0.57997E-08   0.14867E-08 0.19906E+00 
c  r23          0.39971E-02      19   0.59699E-08   0.13030E-08 0.19910E+00 
c  epsilon      0.10970E+02      11   0.34083E-08   0.99675E-02 0.16535E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.84389E-02 0.43309E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161985


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63372          0.6136       0.0052549       0.0015073
v  Velocity[Y]            -0.57373         0.54432       0.0030797      0.00087338
v  Velocity[Z]              1.5656          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4374          4.3406          4.3632
v  Pressure                -36.416          360.03          87.654          169.86
v  r11                   0.0010593        0.081919        0.013071        0.018284
v  r22                   0.0011108         0.08264        0.013351        0.018644
v  r33                   0.0016345         0.17427        0.027244        0.037203
v  r12                   -0.010661        0.013612     -0.00023377     -0.00030928
v  r13                    -0.04556          0.0528      9.2921e-05       0.0010136
v  r23                   -0.046709        0.051224      3.0194e-05      0.00057444
v  epsilon                0.068706          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9887e-05       0.0099176      0.00092456       0.0017425
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017877           5.278         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85282


 TIME FOR THE TIME STEP            10248:        0.88171E+02

===============================================================


 INSTANT    0.102490000E-01   TIME STEP NUMBER           10249
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.883872066E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154063943E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.139903006E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.330283575E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.156127862E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81185E-03   0.45291E-02 0.19919E+01 
c  Velocity[X]                                      0.13787E-03 
c  Velocity[Y]                                      0.12882E-03 
c  Velocity[Z]                                      0.42624E-02 
c  Pressure     0.36209E-04     131   0.92156E-02   0.25541E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57650E-08   0.16527E-08 0.99957E-01 
c  r22          0.10851E-01      13   0.54855E-08   0.18270E-08 0.10117E+00 
c  r33          0.21858E-01      14   0.65039E-08   0.12714E-07 0.12783E+00 
c  r12          0.93849E-03      18   0.60260E-08   0.30044E-09 0.60560E+00 
c  r13          0.46671E-02      19   0.57222E-08   0.15245E-08 0.20048E+00 
c  r23          0.39971E-02      19   0.57888E-08   0.13228E-08 0.20104E+00 
c  epsilon      0.10970E+02      11   0.34720E-08   0.10360E-01 0.17201E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.83914E-02 0.43258E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161981


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369         0.61357       0.0052549       0.0015073
v  Velocity[Y]            -0.57368         0.54448       0.0030797      0.00087336
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.424          360.03          87.647          169.86
v  r11                   0.0010593        0.081918        0.013071        0.018284
v  r22                   0.0011108        0.082639        0.013351        0.018644
v  r33                   0.0016345         0.17428        0.027244        0.037203
v  r12                   -0.010661        0.013617     -0.00023377     -0.00030928
v  r13                   -0.045564          0.0528      9.2921e-05       0.0010136
v  r23                   -0.046708        0.051218      3.0194e-05      0.00057444
v  epsilon                0.068707          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9887e-05       0.0099173      0.00092456       0.0017425
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017877          5.2782         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71349         0.85283


 TIME FOR THE TIME STEP            10249:        0.86326E+02

===============================================================


 INSTANT    0.102500000E-01   TIME STEP NUMBER           10250
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.245296178E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.495239102E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119295680E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.135852218E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136245318E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81265E-03   0.45343E-02 0.19946E+01 
c  Velocity[X]                                      0.13804E-03 
c  Velocity[Y]                                      0.12938E-03 
c  Velocity[Z]                                      0.42669E-02 
c  Pressure     0.36319E-04     132   0.92451E-02   0.25618E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57388E-08   0.16034E-08 0.98911E-01 
c  r22          0.10851E-01      13   0.49515E-08   0.17901E-08 0.10064E+00 
c  r33          0.21858E-01      14   0.67423E-08   0.12223E-07 0.12618E+00 
c  r12          0.93849E-03      18   0.55254E-08   0.29183E-09 0.60146E+00 
c  r13          0.46671E-02      19   0.70342E-08   0.14646E-08 0.19845E+00 
c  r23          0.39971E-02      19   0.66697E-08   0.12549E-08 0.19703E+00 
c  epsilon      0.10970E+02      11   0.32763E-08   0.94423E-02 0.16288E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84589E-02 0.43339E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63362         0.61361       0.0052548       0.0015073
v  Velocity[Y]            -0.57354         0.54415       0.0030797      0.00087335
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.437          359.99          87.649          169.83
v  r11                   0.0010593        0.081915        0.013071        0.018284
v  r22                   0.0011108        0.082638        0.013351        0.018644
v  r33                   0.0016345          0.1743        0.027244        0.037203
v  r12                   -0.010664        0.013621     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052802      9.2922e-05       0.0010136
v  r23                   -0.046707        0.051245      3.0195e-05      0.00057444
v  epsilon                0.068708          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9885e-05       0.0099174      0.00092456       0.0017425
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017876          5.2774         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71349         0.85283


 TIME FOR THE TIME STEP            10250:        0.88881E+02

===============================================================


 INSTANT    0.102510000E-01   TIME STEP NUMBER           10251
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.354072322E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.108042954E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.172003527E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.142192176E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.446237421E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81265E-03   0.45551E-02 0.19971E+01 
c  Velocity[X]                                      0.13956E-03 
c  Velocity[Y]                                      0.12985E-03 
c  Velocity[Z]                                      0.42857E-02 
c  Pressure     0.36645E-04     132   0.93268E-02   0.25849E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57630E-08   0.16162E-08 0.99442E-01 
c  r22          0.10851E-01      13   0.53482E-08   0.18055E-08 0.10123E+00 
c  r33          0.21858E-01      15   0.56076E-08   0.12361E-07 0.12698E+00 
c  r12          0.93849E-03      18   0.61241E-08   0.29048E-09 0.60045E+00 
c  r13          0.46671E-02      19   0.69655E-08   0.14748E-08 0.19921E+00 
c  r23          0.39971E-02      19   0.52895E-08   0.12610E-08 0.19840E+00 
c  epsilon      0.10970E+02      11   0.31778E-08   0.93986E-02 0.16100E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.84329E-02 0.43290E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364         0.61362       0.0052549       0.0015073
v  Velocity[Y]            -0.57365         0.54417       0.0030798      0.00087342
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.418          360.09          87.687          169.91
v  r11                   0.0010593        0.081915        0.013071        0.018284
v  r22                   0.0011108        0.082633        0.013351        0.018644
v  r33                   0.0016345         0.17429        0.027244        0.037203
v  r12                   -0.010663        0.013616     -0.00023377     -0.00030928
v  r13                    -0.04556        0.052802      9.2923e-05       0.0010136
v  r23                   -0.046706        0.051241      3.0196e-05      0.00057444
v  epsilon                0.068709          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9887e-05       0.0099176      0.00092456       0.0017425
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017876          5.2771         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71349         0.85283


 TIME FOR THE TIME STEP            10251:        0.86329E+02

===============================================================


 INSTANT    0.102520000E-01   TIME STEP NUMBER           10252
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.727590619E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.912165750E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.136568613E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200291145E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.109373468E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81203E-03   0.45191E-02 0.19900E+01 
c  Velocity[X]                                      0.13848E-03 
c  Velocity[Y]                                      0.12887E-03 
c  Velocity[Z]                                      0.42517E-02 
c  Pressure     0.36299E-04     133   0.92408E-02   0.25604E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56113E-08   0.16703E-08 0.10040E+00 
c  r22          0.10851E-01      13   0.54414E-08   0.18588E-08 0.10224E+00 
c  r33          0.21858E-01      15   0.56070E-08   0.12768E-07 0.12823E+00 
c  r12          0.93849E-03      18   0.52405E-08   0.30165E-09 0.60822E+00 
c  r13          0.46671E-02      19   0.60973E-08   0.15111E-08 0.20035E+00 
c  r23          0.39971E-02      19   0.50596E-08   0.12972E-08 0.20018E+00 
c  epsilon      0.10970E+02      11   0.33285E-08   0.10233E-01 0.16889E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.83733E-02 0.43197E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63362         0.61358       0.0052549       0.0015073
v  Velocity[Y]            -0.57352         0.54428       0.0030798      0.00087341
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.465          360.05          87.672          169.88
v  r11                   0.0010593        0.081916        0.013071        0.018284
v  r22                   0.0011108        0.082633        0.013351        0.018644
v  r33                   0.0016345         0.17427        0.027244        0.037203
v  r12                   -0.010671        0.013613     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052802      9.2924e-05       0.0010136
v  r23                   -0.046705        0.051232      3.0197e-05      0.00057444
v  epsilon                 0.06871          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9887e-05       0.0099178      0.00092457       0.0017425
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017876          5.2774         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71349         0.85283


 TIME FOR THE TIME STEP            10252:        0.86446E+02

===============================================================


 INSTANT    0.102530000E-01   TIME STEP NUMBER           10253
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.262817914E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.388086893E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.253102460E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.440932568E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.240524083E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81187E-03   0.45210E-02 0.19926E+01 
c  Velocity[X]                                      0.13823E-03 
c  Velocity[Y]                                      0.12984E-03 
c  Velocity[Z]                                      0.42529E-02 
c  Pressure     0.36411E-04     133   0.92695E-02   0.25683E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58137E-08   0.16545E-08 0.10032E+00 
c  r22          0.10851E-01      13   0.51187E-08   0.18593E-08 0.10235E+00 
c  r33          0.21858E-01      15   0.52175E-08   0.12717E-07 0.12829E+00 
c  r12          0.93850E-03      18   0.52325E-08   0.30131E-09 0.60745E+00 
c  r13          0.46671E-02      19   0.61861E-08   0.15057E-08 0.20057E+00 
c  r23          0.39971E-02      18   0.69395E-08   0.12788E-08 0.19878E+00 
c  epsilon      0.10970E+02      11   0.34196E-08   0.10072E-01 0.16758E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.84256E-02 0.43355E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61358       0.0052549       0.0015073
v  Velocity[Y]            -0.57372          0.5444       0.0030798      0.00087342
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.391          360.03          87.652          169.85
v  r11                   0.0010593        0.081915        0.013071        0.018284
v  r22                   0.0011108        0.082633        0.013351        0.018644
v  r33                   0.0016345         0.17428        0.027244        0.037203
v  r12                   -0.010674        0.013612     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052799      9.2926e-05       0.0010136
v  r23                   -0.046705        0.051254      3.0198e-05      0.00057444
v  epsilon                0.068711          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9889e-05       0.0099179      0.00092457       0.0017425
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017876          5.2779         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7404e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71349         0.85283


 TIME FOR THE TIME STEP            10253:        0.90381E+02

===============================================================


 INSTANT    0.102540000E-01   TIME STEP NUMBER           10254
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190983751E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.823242510E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.297427496E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.187329534E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.174420864E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81253E-03   0.45456E-02 0.19959E+01 
c  Velocity[X]                                      0.13858E-03 
c  Velocity[Y]                                      0.12959E-03 
c  Velocity[Z]                                      0.42774E-02 
c  Pressure     0.36070E-04     133   0.91860E-02   0.25443E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59810E-08   0.16525E-08 0.99954E-01 
c  r22          0.10851E-01      13   0.52392E-08   0.18242E-08 0.10116E+00 
c  r33          0.21858E-01      15   0.55531E-08   0.12599E-07 0.12707E+00 
c  r12          0.93850E-03      18   0.54951E-08   0.29999E-09 0.60613E+00 
c  r13          0.46671E-02      19   0.72154E-08   0.14860E-08 0.19863E+00 
c  r23          0.39972E-02      19   0.66764E-08   0.12859E-08 0.19843E+00 
c  epsilon      0.10970E+02      11   0.34182E-08   0.10035E-01 0.16550E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.84405E-02 0.43304E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61356       0.0052549       0.0015073
v  Velocity[Y]            -0.57366         0.54425       0.0030798      0.00087341
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.427          360.05          87.678          169.88
v  r11                   0.0010593        0.081925        0.013071        0.018284
v  r22                   0.0011108        0.082635        0.013351        0.018644
v  r33                   0.0016345         0.17432        0.027244        0.037203
v  r12                   -0.010671        0.013603     -0.00023377     -0.00030928
v  r13                    -0.04556        0.052799      9.2927e-05       0.0010136
v  r23                   -0.046706        0.051238      3.0199e-05      0.00057444
v  epsilon                0.068712          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9891e-05       0.0099179      0.00092457       0.0017425
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017876          5.2791         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71349         0.85282


 TIME FOR THE TIME STEP            10254:        0.88534E+02

===============================================================


 INSTANT    0.102550000E-01   TIME STEP NUMBER           10255
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.655886150E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.808320209E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.175401109E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173658098E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.149124631E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81217E-03   0.44907E-02 0.19849E+01 
c  Velocity[X]                                      0.13839E-03 
c  Velocity[Y]                                      0.12850E-03 
c  Velocity[Z]                                      0.42238E-02 
c  Pressure     0.36351E-04     132   0.92552E-02   0.25640E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59189E-08   0.16752E-08 0.10050E+00 
c  r22          0.10851E-01      13   0.48987E-08   0.18201E-08 0.10129E+00 
c  r33          0.21858E-01      15   0.65921E-08   0.12657E-07 0.12765E+00 
c  r12          0.93850E-03      18   0.53331E-08   0.29728E-09 0.60297E+00 
c  r13          0.46671E-02      20   0.58658E-08   0.14825E-08 0.19878E+00 
c  r23          0.39972E-02      19   0.64901E-08   0.13076E-08 0.20008E+00 
c  epsilon      0.10970E+02      11   0.35644E-08   0.10265E-01 0.17196E+00 
c  TempC        0.25716E+06      16   0.15104E-04   0.84240E-02 0.43250E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61356       0.0052548       0.0015072
v  Velocity[Y]            -0.57366         0.54418       0.0030799      0.00087344
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.399          360.04          87.665          169.87
v  r11                   0.0010593        0.081923        0.013071        0.018284
v  r22                   0.0011108        0.082635        0.013351        0.018644
v  r33                   0.0016345          0.1743        0.027244        0.037203
v  r12                   -0.010664        0.013598     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052797      9.2928e-05       0.0010136
v  r23                   -0.046707        0.051233      3.0199e-05      0.00057444
v  epsilon                0.068713          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9895e-05        0.009918      0.00092457       0.0017425
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017875          5.2791         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71349         0.85283


 TIME FOR THE TIME STEP            10255:        0.85140E+02

===============================================================


 INSTANT    0.102560000E-01   TIME STEP NUMBER           10256
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.243656765E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.155955086E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.406913603E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.124767978E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138185245E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81223E-03   0.45584E-02 0.20003E+01 
c  Velocity[X]                                      0.13827E-03 
c  Velocity[Y]                                      0.12936E-03 
c  Velocity[Z]                                      0.42908E-02 
c  Pressure     0.36729E-04     133   0.93487E-02   0.25907E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58832E-08   0.16429E-08 0.99842E-01 
c  r22          0.10851E-01      13   0.45082E-08   0.18166E-08 0.10153E+00 
c  r33          0.21858E-01      15   0.54749E-08   0.12463E-07 0.12732E+00 
c  r12          0.93850E-03      18   0.52495E-08   0.29116E-09 0.60096E+00 
c  r13          0.46671E-02      19   0.61231E-08   0.14816E-08 0.19936E+00 
c  r23          0.39972E-02      19   0.59735E-08   0.12703E-08 0.19824E+00 
c  epsilon      0.10970E+02      11   0.33524E-08   0.97130E-02 0.16484E+00 
c  TempC        0.25716E+06      16   0.15164E-04   0.84248E-02 0.43344E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63372         0.61357       0.0052548       0.0015072
v  Velocity[Y]             -0.5735         0.54423       0.0030798       0.0008734
v  Velocity[Z]              1.5656          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4374          4.3406          4.3632
v  Pressure                 -36.45          360.03          87.668          169.86
v  r11                   0.0010592        0.081918        0.013071        0.018284
v  r22                   0.0011108        0.082635        0.013351        0.018644
v  r33                   0.0016345         0.17426        0.027244        0.037203
v  r12                   -0.010662        0.013593     -0.00023377     -0.00030928
v  r13                    -0.04556        0.052798       9.293e-05       0.0010136
v  r23                   -0.046708        0.051228      3.0201e-05      0.00057444
v  epsilon                0.068715          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9898e-05        0.009918      0.00092457       0.0017425
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017875          5.2797         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8797         0.71349         0.85283


 TIME FOR THE TIME STEP            10256:        0.83762E+02

===============================================================


 INSTANT    0.102570000E-01   TIME STEP NUMBER           10257
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117706229E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.176945948E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.363630058E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285266316E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.170044416E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      45   0.81137E-03   0.45457E-02 0.19981E+01 
c  Velocity[X]                                      0.13905E-03 
c  Velocity[Y]                                      0.12895E-03 
c  Velocity[Z]                                      0.42777E-02 
c  Pressure     0.36766E-04     134   0.93603E-02   0.25934E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56622E-08   0.16195E-08 0.99371E-01 
c  r22          0.10851E-01      13   0.47346E-08   0.18576E-08 0.10217E+00 
c  r33          0.21858E-01      15   0.64586E-08   0.12599E-07 0.12769E+00 
c  r12          0.93850E-03      18   0.54501E-08   0.29462E-09 0.60363E+00 
c  r13          0.46671E-02      19   0.62990E-08   0.15188E-08 0.20125E+00 
c  r23          0.39972E-02      19   0.59676E-08   0.12648E-08 0.19853E+00 
c  epsilon      0.10970E+02      11   0.32306E-08   0.99648E-02 0.16581E+00 
c  TempC        0.25716E+06      16   0.15122E-04   0.84682E-02 0.43440E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63372         0.61355       0.0052548       0.0015072
v  Velocity[Y]            -0.57341         0.54434       0.0030798      0.00087342
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.416          360.12          87.695          169.92
v  r11                   0.0010592        0.081918        0.013071        0.018284
v  r22                   0.0011108         0.08263        0.013351        0.018644
v  r33                   0.0016345         0.17428        0.027244        0.037203
v  r12                   -0.010665        0.013589     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052799      9.2931e-05       0.0010136
v  r23                   -0.046708        0.051252      3.0202e-05      0.00057444
v  epsilon                0.068716          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9901e-05        0.009918      0.00092457       0.0017425
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017875          5.2798         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8798         0.71349         0.85283


 TIME FOR THE TIME STEP            10257:        0.85348E+02

===============================================================


 INSTANT    0.102580000E-01   TIME STEP NUMBER           10258
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.251025911E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.719821475E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.281586092E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.177078447E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.188892218E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81314E-03   0.45236E-02 0.19915E+01 
c  Velocity[X]                                      0.13905E-03 
c  Velocity[Y]                                      0.12937E-03 
c  Velocity[Z]                                      0.42552E-02 
c  Pressure     0.36030E-04     132   0.91722E-02   0.25416E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60006E-08   0.16836E-08 0.10078E+00 
c  r22          0.10851E-01      12   0.65550E-08   0.18254E-08 0.10133E+00 
c  r33          0.21858E-01      15   0.66221E-08   0.12706E-07 0.12810E+00 
c  r12          0.93850E-03      18   0.52475E-08   0.30128E-09 0.60702E+00 
c  r13          0.46671E-02      19   0.65185E-08   0.15051E-08 0.20004E+00 
c  r23          0.39972E-02      19   0.55497E-08   0.13042E-08 0.20119E+00 
c  epsilon      0.10970E+02      11   0.33709E-08   0.10050E-01 0.16705E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.83769E-02 0.43176E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369         0.61353       0.0052548       0.0015073
v  Velocity[Y]            -0.57328         0.54412       0.0030798      0.00087339
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.454          360.02          87.651          169.85
v  r11                   0.0010592        0.081922        0.013071        0.018284
v  r22                   0.0011108        0.082631        0.013351        0.018644
v  r33                   0.0016345         0.17431        0.027244        0.037203
v  r12                   -0.010664        0.013591     -0.00023377     -0.00030928
v  r13                   -0.045563        0.052799      9.2931e-05       0.0010136
v  r23                   -0.046708        0.051241      3.0202e-05      0.00057444
v  epsilon                0.068717          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9903e-05        0.009918      0.00092457       0.0017425
v  CourantNb               0.44261             0.6         0.59908         0.59839
v  FourierNb             0.0017875          5.2799         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8799         0.71349         0.85283


 TIME FOR THE TIME STEP            10258:        0.83629E+02

===============================================================


 INSTANT    0.102590000E-01   TIME STEP NUMBER           10259
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.247244063E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.218243100E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.644222811E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.172928718E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108060809E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81128E-03   0.45250E-02 0.19922E+01 
c  Velocity[X]                                      0.13829E-03 
c  Velocity[Y]                                      0.12906E-03 
c  Velocity[Z]                                      0.42576E-02 
c  Pressure     0.36339E-04     132   0.92508E-02   0.25633E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57983E-08   0.16145E-08 0.99134E-01 
c  r22          0.10851E-01      13   0.47333E-08   0.17984E-08 0.10106E+00 
c  r33          0.21858E-01      15   0.68361E-08   0.12223E-07 0.12646E+00 
c  r12          0.93850E-03      18   0.55955E-08   0.28917E-09 0.60017E+00 
c  r13          0.46671E-02      20   0.64619E-08   0.14564E-08 0.19853E+00 
c  r23          0.39972E-02      19   0.52927E-08   0.12565E-08 0.19738E+00 
c  epsilon      0.10970E+02      11   0.34779E-08   0.94634E-02 0.16240E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84300E-02 0.43296E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361         0.61356       0.0052549       0.0015072
v  Velocity[Y]            -0.57338         0.54424       0.0030798      0.00087342
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                 -36.39          359.95          87.618           169.8
v  r11                   0.0010592        0.081924        0.013071        0.018284
v  r22                   0.0011108        0.082632        0.013351        0.018644
v  r33                   0.0016345         0.17429        0.027244        0.037203
v  r12                   -0.010661         0.01359     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052797      9.2933e-05       0.0010136
v  r23                   -0.046707        0.051226      3.0203e-05      0.00057444
v  epsilon                0.068718          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9905e-05       0.0099176      0.00092457       0.0017425
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017874          5.2795         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8795         0.71349         0.85282


 TIME FOR THE TIME STEP            10259:        0.83952E+02

===============================================================


 INSTANT    0.102600000E-01   TIME STEP NUMBER           10260
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239807880E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.470008972E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.966281146E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.289826467E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.103534057E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81246E-03   0.45372E-02 0.19937E+01 
c  Velocity[X]                                      0.13951E-03 
c  Velocity[Y]                                      0.12925E-03 
c  Velocity[Z]                                      0.42684E-02 
c  Pressure     0.36473E-04     133   0.92863E-02   0.25727E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59653E-08   0.16798E-08 0.10102E+00 
c  r22          0.10851E-01      13   0.48553E-08   0.18601E-08 0.10212E+00 
c  r33          0.21858E-01      15   0.55669E-08   0.12749E-07 0.12855E+00 
c  r12          0.93850E-03      18   0.56917E-08   0.29733E-09 0.60581E+00 
c  r13          0.46671E-02      19   0.65821E-08   0.15057E-08 0.20058E+00 
c  r23          0.39972E-02      18   0.69272E-08   0.12921E-08 0.20044E+00 
c  epsilon      0.10970E+02      11   0.33734E-08   0.10234E-01 0.16832E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.84858E-02 0.43458E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63365         0.61358       0.0052549       0.0015072
v  Velocity[Y]            -0.57333         0.54437       0.0030798      0.00087343
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.424          360.02          87.654          169.85
v  r11                   0.0010592         0.08193        0.013071        0.018284
v  r22                   0.0011108        0.082632        0.013351        0.018644
v  r33                   0.0016345         0.17426        0.027244        0.037203
v  r12                   -0.010658        0.013596     -0.00023377     -0.00030928
v  r13                   -0.045559        0.052797      9.2934e-05       0.0010136
v  r23                   -0.046708        0.051235      3.0204e-05      0.00057445
v  epsilon                0.068719          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9906e-05       0.0099175      0.00092458       0.0017425
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017874          5.2788         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71349         0.85283


 TIME FOR THE TIME STEP            10260:        0.81466E+02

===============================================================


 INSTANT    0.102610000E-01   TIME STEP NUMBER           10261
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.278464270E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.196750708E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.760389489E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.355913194E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.367274560E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81206E-03   0.45117E-02 0.19882E+01 
c  Velocity[X]                                      0.13830E-03 
c  Velocity[Y]                                      0.12939E-03 
c  Velocity[Z]                                      0.42440E-02 
c  Pressure     0.36620E-04     132   0.93211E-02   0.25831E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.50668E-08   0.16440E-08 0.10041E+00 
c  r22          0.10851E-01      13   0.47526E-08   0.18458E-08 0.10252E+00 
c  r33          0.21858E-01      15   0.53017E-08   0.12636E-07 0.12899E+00 
c  r12          0.93850E-03      18   0.56449E-08   0.30037E-09 0.60906E+00 
c  r13          0.46671E-02      19   0.56940E-08   0.15188E-08 0.20182E+00 
c  r23          0.39972E-02      19   0.59680E-08   0.12996E-08 0.20220E+00 
c  epsilon      0.10970E+02      11   0.32228E-08   0.99653E-02 0.17013E+00 
c  TempC        0.25716E+06      16   0.15142E-04   0.83721E-02 0.43185E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63366         0.61356       0.0052548       0.0015072
v  Velocity[Y]            -0.57333         0.54443       0.0030799      0.00087343
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.409          360.07          87.675          169.89
v  r11                   0.0010592        0.081928        0.013071        0.018284
v  r22                   0.0011108        0.082633        0.013351        0.018644
v  r33                   0.0016345         0.17428        0.027244        0.037203
v  r12                   -0.010656        0.013596     -0.00023377     -0.00030928
v  r13                   -0.045564        0.052798      9.2935e-05       0.0010136
v  r23                   -0.046708        0.051228      3.0205e-05      0.00057445
v  epsilon                 0.06872          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9906e-05       0.0099174      0.00092458       0.0017425
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017874          5.2786         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71349         0.85283


 TIME FOR THE TIME STEP            10261:        0.83581E+02

===============================================================


 INSTANT    0.102620000E-01   TIME STEP NUMBER           10262
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.273728061E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69792E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.168004737E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69792E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.207385733E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69792E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.900627879E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69792E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.279028277E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69792E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81222E-03   0.45519E-02 0.19980E+01 
c  Velocity[X]                                      0.13817E-03 
c  Velocity[Y]                                      0.12944E-03 
c  Velocity[Z]                                      0.42843E-02 
c  Pressure     0.36472E-04     133   0.92870E-02   0.25726E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53847E-08   0.16701E-08 0.10068E+00 
c  r22          0.10851E-01      13   0.49846E-08   0.18684E-08 0.10327E+00 
c  r33          0.21858E-01      14   0.69855E-08   0.12774E-07 0.12927E+00 
c  r12          0.93850E-03      18   0.59892E-08   0.30073E-09 0.60911E+00 
c  r13          0.46671E-02      18   0.69438E-08   0.14976E-08 0.20164E+00 
c  r23          0.39972E-02      18   0.63414E-08   0.12985E-08 0.20078E+00 
c  epsilon      0.10970E+02      11   0.32322E-08   0.10001E-01 0.16631E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.83855E-02 0.43204E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162019


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61357       0.0052549       0.0015072
v  Velocity[Y]            -0.57317         0.54423       0.0030798       0.0008734
v  Velocity[Z]              1.5656          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4374          4.3406          4.3632
v  Pressure                -36.446          360.04          87.662          169.87
v  r11                   0.0010592        0.081926        0.013071        0.018284
v  r22                   0.0011108        0.082634        0.013351        0.018644
v  r33                   0.0016345          0.1743        0.027244        0.037203
v  r12                   -0.010656        0.013594     -0.00023377     -0.00030928
v  r13                   -0.045561          0.0528      9.2935e-05       0.0010136
v  r23                   -0.046709        0.051219      3.0205e-05      0.00057445
v  epsilon                0.068721          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9906e-05       0.0099176      0.00092458       0.0017425
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017874          5.2783         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71349         0.85283


 TIME FOR THE TIME STEP            10262:        0.84291E+02

===============================================================


 INSTANT    0.102630000E-01   TIME STEP NUMBER           10263
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.862283805E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.613738900E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.739132707E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.233719734E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.170980675E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81171E-03   0.45365E-02 0.19958E+01 
c  Velocity[X]                                      0.13973E-03 
c  Velocity[Y]                                      0.12903E-03 
c  Velocity[Z]                                      0.42677E-02 
c  Pressure     0.36381E-04     133   0.92667E-02   0.25662E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55433E-08   0.16296E-08 0.99737E-01 
c  r22          0.10851E-01      13   0.51322E-08   0.18325E-08 0.10194E+00 
c  r33          0.21858E-01      15   0.58484E-08   0.12411E-07 0.12728E+00 
c  r12          0.93850E-03      18   0.61481E-08   0.29710E-09 0.60405E+00 
c  r13          0.46671E-02      19   0.61007E-08   0.14785E-08 0.19951E+00 
c  r23          0.39972E-02      19   0.57117E-08   0.12645E-08 0.19807E+00 
c  epsilon      0.10970E+02      11   0.32961E-08   0.96416E-02 0.16260E+00 
c  TempC        0.25716E+06      16   0.15114E-04   0.85216E-02 0.43523E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369         0.61359       0.0052549       0.0015072
v  Velocity[Y]            -0.57305         0.54423       0.0030799      0.00087347
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.425           360.1          87.699          169.92
v  r11                   0.0010592        0.081924        0.013071        0.018284
v  r22                   0.0011108        0.082629        0.013351        0.018644
v  r33                   0.0016345         0.17429        0.027244        0.037203
v  r12                   -0.010653        0.013595     -0.00023377     -0.00030928
v  r13                    -0.04556        0.052797      9.2936e-05       0.0010136
v  r23                   -0.046709        0.051213      3.0206e-05      0.00057445
v  epsilon                0.068723          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9905e-05       0.0099177      0.00092458       0.0017425
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017874          5.2785         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71349         0.85283


 TIME FOR THE TIME STEP            10263:        0.86608E+02

===============================================================


 INSTANT    0.102640000E-01   TIME STEP NUMBER           10264
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.354496513E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.272495261E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.152871966E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106576531E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.219417272E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81246E-03   0.45100E-02 0.19891E+01 
c  Velocity[X]                                      0.13861E-03 
c  Velocity[Y]                                      0.12894E-03 
c  Velocity[Z]                                      0.42424E-02 
c  Pressure     0.36366E-04     133   0.92597E-02   0.25651E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58541E-08   0.16477E-08 0.10003E+00 
c  r22          0.10851E-01      13   0.53921E-08   0.18420E-08 0.10186E+00 
c  r33          0.21858E-01      15   0.56084E-08   0.12605E-07 0.12760E+00 
c  r12          0.93850E-03      18   0.71443E-08   0.29518E-09 0.60289E+00 
c  r13          0.46671E-02      19   0.72077E-08   0.15019E-08 0.19983E+00 
c  r23          0.39972E-02      19   0.61263E-08   0.12741E-08 0.19857E+00 
c  epsilon      0.10970E+02      11   0.33728E-08   0.99770E-02 0.16561E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.83959E-02 0.43272E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369         0.61358       0.0052549       0.0015072
v  Velocity[Y]            -0.57301         0.54424       0.0030799      0.00087343
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                 -36.43          360.03          87.652          169.85
v  r11                   0.0010592        0.081926        0.013071        0.018284
v  r22                   0.0011108        0.082631        0.013351        0.018644
v  r33                   0.0016345         0.17427        0.027244        0.037203
v  r12                   -0.010654        0.013589     -0.00023377     -0.00030928
v  r13                   -0.045563        0.052798      9.2937e-05       0.0010136
v  r23                   -0.046709        0.051239      3.0207e-05      0.00057445
v  epsilon                0.068724          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9904e-05       0.0099177      0.00092458       0.0017425
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017873          5.2791         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791          0.7135         0.85284


 TIME FOR THE TIME STEP            10264:        0.89965E+02

===============================================================


 INSTANT    0.102650000E-01   TIME STEP NUMBER           10265
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.186936540E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.623141356E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.211810707E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.501546852E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.542945349E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81189E-03   0.45494E-02 0.19989E+01 
c  Velocity[X]                                      0.13844E-03 
c  Velocity[Y]                                      0.12902E-03 
c  Velocity[Z]                                      0.42819E-02 
c  Pressure     0.36190E-04     133   0.92098E-02   0.25528E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55948E-08   0.16553E-08 0.10005E+00 
c  r22          0.10851E-01      13   0.55888E-08   0.18400E-08 0.10180E+00 
c  r33          0.21858E-01      15   0.52375E-08   0.12579E-07 0.12746E+00 
c  r12          0.93850E-03      18   0.71483E-08   0.30295E-09 0.60756E+00 
c  r13          0.46671E-02      19   0.75794E-08   0.15033E-08 0.19928E+00 
c  r23          0.39972E-02      19   0.59179E-08   0.12936E-08 0.19951E+00 
c  epsilon      0.10970E+02      11   0.35430E-08   0.99520E-02 0.16624E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.83916E-02 0.43157E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369          0.6136       0.0052549       0.0015072
v  Velocity[Y]            -0.57311         0.54435       0.0030799      0.00087346
v  Velocity[Z]              1.5656          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4374          4.3406          4.3632
v  Pressure                -36.412             360          87.628          169.82
v  r11                   0.0010592        0.081924        0.013071        0.018284
v  r22                   0.0011108        0.082633        0.013351        0.018644
v  r33                   0.0016345         0.17428        0.027244        0.037203
v  r12                   -0.010653         0.01359     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052798      9.2938e-05       0.0010136
v  r23                   -0.046708        0.051232      3.0208e-05      0.00057445
v  epsilon                0.068725          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9902e-05       0.0099175      0.00092458       0.0017425
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017873          5.2796         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8796          0.7135         0.85283


 TIME FOR THE TIME STEP            10265:        0.90719E+02

===============================================================


 INSTANT    0.102660000E-01   TIME STEP NUMBER           10266
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.135803364E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169006570E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.310934616E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.256952924E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.240363895E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81256E-03   0.45316E-02 0.19951E+01 
c  Velocity[X]                                      0.13951E-03 
c  Velocity[Y]                                      0.12985E-03 
c  Velocity[Z]                                      0.42623E-02 
c  Pressure     0.36509E-04     133   0.93014E-02   0.25753E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57280E-08   0.16482E-08 0.10010E+00 
c  r22          0.10851E-01      13   0.52952E-08   0.18697E-08 0.10239E+00 
c  r33          0.21858E-01      14   0.68054E-08   0.12709E-07 0.12846E+00 
c  r12          0.93850E-03      18   0.70764E-08   0.30256E-09 0.60769E+00 
c  r13          0.46671E-02      19   0.72469E-08   0.15318E-08 0.20114E+00 
c  r23          0.39972E-02      19   0.56240E-08   0.12919E-08 0.19996E+00 
c  epsilon      0.10970E+02      11   0.34380E-08   0.10097E-01 0.16637E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84832E-02 0.43457E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61358       0.0052549       0.0015072
v  Velocity[Y]            -0.57302         0.54416       0.0030799      0.00087346
v  Velocity[Z]              1.5656          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4374          4.3406          4.3632
v  Pressure                -36.431          359.96          87.618           169.8
v  r11                   0.0010592        0.081924        0.013071        0.018284
v  r22                   0.0011108        0.082634        0.013351        0.018644
v  r33                   0.0016345         0.17431        0.027244        0.037203
v  r12                   -0.010657        0.013582     -0.00023377     -0.00030928
v  r13                    -0.04556        0.052799       9.294e-05       0.0010137
v  r23                   -0.046708        0.051221      3.0209e-05      0.00057445
v  epsilon                0.068726          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9899e-05       0.0099176      0.00092458       0.0017425
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017873          5.2799         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8799         0.71349         0.85283


 TIME FOR THE TIME STEP            10266:        0.90910E+02

===============================================================


 INSTANT    0.102670000E-01   TIME STEP NUMBER           10267
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.128270861E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162529835E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934910E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.581055330E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.580311150E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.808892362E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81203E-03   0.45121E-02 0.19882E+01 
c  Velocity[X]                                      0.13861E-03 
c  Velocity[Y]                                      0.12871E-03 
c  Velocity[Z]                                      0.42447E-02 
c  Pressure     0.36561E-04     131   0.93098E-02   0.25789E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53358E-08   0.16609E-08 0.10075E+00 
c  r22          0.10851E-01      13   0.50405E-08   0.18080E-08 0.10162E+00 
c  r33          0.21858E-01      15   0.57819E-08   0.12497E-07 0.12829E+00 
c  r12          0.93850E-03      18   0.67130E-08   0.29181E-09 0.60181E+00 
c  r13          0.46671E-02      19   0.56521E-08   0.14868E-08 0.19989E+00 
c  r23          0.39972E-02      19   0.58008E-08   0.12988E-08 0.20120E+00 
c  epsilon      0.10970E+02      11   0.33901E-08   0.99911E-02 0.17132E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.84216E-02 0.43307E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63366         0.61355       0.0052548       0.0015072
v  Velocity[Y]            -0.57318         0.54424         0.00308      0.00087349
v  Velocity[Z]              1.5656          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4374          4.3406          4.3632
v  Pressure                -36.392           360.1           87.71          169.92
v  r11                   0.0010592        0.081923        0.013071        0.018284
v  r22                   0.0011108        0.082634        0.013351        0.018644
v  r33                   0.0016345         0.17429        0.027244        0.037203
v  r12                   -0.010657        0.013575     -0.00023377     -0.00030928
v  r13                   -0.045562        0.052797      9.2941e-05       0.0010137
v  r23                   -0.046707        0.051253       3.021e-05      0.00057445
v  epsilon                0.068727          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc               5.99e-05       0.0099176      0.00092458       0.0017425
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017873          5.2795         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8795         0.71349         0.85283


 TIME FOR THE TIME STEP            10267:        0.87642E+02

===============================================================


 INSTANT    0.102680000E-01   TIME STEP NUMBER           10268
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.494060580E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.311988858E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.330876608E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129099726E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.350673940E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69791E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81201E-03   0.45473E-02 0.19960E+01 
c  Velocity[X]                                      0.13847E-03 
c  Velocity[Y]                                      0.12923E-03 
c  Velocity[Z]                                      0.42796E-02 
c  Pressure     0.36423E-04     131   0.92717E-02   0.25692E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52815E-08   0.16451E-08 0.99843E-01 
c  r22          0.10851E-01      13   0.47868E-08   0.18437E-08 0.10185E+00 
c  r33          0.21858E-01      15   0.55867E-08   0.12643E-07 0.12798E+00 
c  r12          0.93850E-03      18   0.64137E-08   0.30573E-09 0.60908E+00 
c  r13          0.46671E-02      19   0.66464E-08   0.14833E-08 0.19915E+00 
c  r23          0.39972E-02      19   0.67208E-08   0.12957E-08 0.20005E+00 
c  epsilon      0.10970E+02      11   0.34003E-08   0.98683E-02 0.16630E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.84416E-02 0.43339E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369         0.61355       0.0052548       0.0015072
v  Velocity[Y]            -0.57317         0.54441       0.0030799      0.00087347
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                 -36.45          360.02          87.668          169.86
v  r11                   0.0010592         0.08193        0.013071        0.018284
v  r22                   0.0011108        0.082634        0.013351        0.018644
v  r33                   0.0016345         0.17426        0.027244        0.037203
v  r12                   -0.010659        0.013577     -0.00023377     -0.00030928
v  r13                    -0.04556        0.052796      9.2942e-05       0.0010137
v  r23                   -0.046707        0.051242      3.0211e-05      0.00057445
v  epsilon                0.068729          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9898e-05       0.0099176      0.00092459       0.0017425
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017873           5.279         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71349         0.85283


 TIME FOR THE TIME STEP            10268:        0.87515E+02

===============================================================


 INSTANT    0.102690000E-01   TIME STEP NUMBER           10269
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.280152049E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.308914811E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.502484388E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.288439396E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.476661882E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81142E-03   0.45336E-02 0.19924E+01 
c  Velocity[X]                                      0.13863E-03 
c  Velocity[Y]                                      0.12869E-03 
c  Velocity[Z]                                      0.42662E-02 
c  Pressure     0.36418E-04     133   0.92683E-02   0.25689E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53176E-08   0.16160E-08 0.99274E-01 
c  r22          0.10851E-01      13   0.55687E-08   0.18183E-08 0.10131E+00 
c  r33          0.21858E-01      15   0.55493E-08   0.12392E-07 0.12713E+00 
c  r12          0.93850E-03      19   0.56701E-08   0.30313E-09 0.60879E+00 
c  r13          0.46671E-02      20   0.57434E-08   0.14892E-08 0.19955E+00 
c  r23          0.39972E-02      19   0.72981E-08   0.12642E-08 0.19792E+00 
c  epsilon      0.10970E+02      11   0.34142E-08   0.95228E-02 0.16228E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.84724E-02 0.43432E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61357       0.0052548       0.0015072
v  Velocity[Y]            -0.57326         0.54434         0.00308      0.00087346
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.393          360.07           87.66          169.88
v  r11                   0.0010592         0.08193        0.013071        0.018284
v  r22                   0.0011108        0.082633        0.013351        0.018644
v  r33                   0.0016345         0.17428        0.027244        0.037203
v  r12                    -0.01066        0.013572     -0.00023377     -0.00030928
v  r13                   -0.045561        0.052796      9.2943e-05       0.0010137
v  r23                   -0.046707        0.051231      3.0213e-05      0.00057445
v  epsilon                 0.06873          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9895e-05       0.0099177      0.00092459       0.0017425
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017872          5.2778         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778          0.7135         0.85283


 TIME FOR THE TIME STEP            10269:        0.91231E+02

===============================================================


 INSTANT    0.102700000E-01   TIME STEP NUMBER           10270
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.148611331E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.440488377E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.366478177E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.219675107E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.213089259E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69790E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81274E-03   0.45201E-02 0.19915E+01 
c  Velocity[X]                                      0.13886E-03 
c  Velocity[Y]                                      0.12924E-03 
c  Velocity[Z]                                      0.42520E-02 
c  Pressure     0.36298E-04     133   0.92463E-02   0.25603E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.48734E-08   0.16550E-08 0.99903E-01 
c  r22          0.10851E-01      13   0.54501E-08   0.18328E-08 0.10193E+00 
c  r33          0.21858E-01      15   0.63213E-08   0.12639E-07 0.12799E+00 
c  r12          0.93850E-03      18   0.60795E-08   0.29986E-09 0.61006E+00 
c  r13          0.46671E-02      18   0.71355E-08   0.14925E-08 0.20001E+00 
c  r23          0.39972E-02      19   0.51685E-08   0.12801E-08 0.19820E+00 
c  epsilon      0.10970E+02      11   0.35357E-08   0.98382E-02 0.16500E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.83307E-02 0.43042E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361         0.61354       0.0052548       0.0015072
v  Velocity[Y]            -0.57326         0.54422       0.0030799      0.00087341
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.482          360.07           87.69          169.89
v  r11                   0.0010592        0.081938        0.013071        0.018284
v  r22                   0.0011108        0.082632        0.013351        0.018644
v  r33                   0.0016345         0.17431        0.027244        0.037203
v  r12                   -0.010666        0.013574     -0.00023378     -0.00030928
v  r13                   -0.045562        0.052797      9.2944e-05       0.0010137
v  r23                   -0.046707        0.051245      3.0213e-05      0.00057445
v  epsilon                0.068731          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9895e-05       0.0099178      0.00092459       0.0017425
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017872          5.2777         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777          0.7135         0.85283


 TIME FOR THE TIME STEP            10270:        0.91795E+02

===============================================================


 INSTANT    0.102710000E-01   TIME STEP NUMBER           10271
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.330967926E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130444668E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.933373453E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.167810660E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178973534E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69789E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81226E-03   0.45480E-02 0.19978E+01 
c  Velocity[X]                                      0.13899E-03 
c  Velocity[Y]                                      0.12947E-03 
c  Velocity[Z]                                      0.42796E-02 
c  Pressure     0.36827E-04     131   0.93695E-02   0.25976E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.50680E-08   0.16411E-08 0.99863E-01 
c  r22          0.10851E-01      13   0.51596E-08   0.18476E-08 0.10217E+00 
c  r33          0.21858E-01      15   0.63209E-08   0.12665E-07 0.12823E+00 
c  r12          0.93850E-03      18   0.57211E-08   0.29847E-09 0.60668E+00 
c  r13          0.46671E-02      19   0.59667E-08   0.14969E-08 0.20015E+00 
c  r23          0.39972E-02      19   0.68654E-08   0.12908E-08 0.19953E+00 
c  epsilon      0.10970E+02      11   0.32833E-08   0.99674E-02 0.16635E+00 
c  TempC        0.25716E+06      16   0.15114E-04   0.83925E-02 0.43234E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63357         0.61359       0.0052548       0.0015072
v  Velocity[Y]            -0.57334         0.54429         0.00308      0.00087342
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.413          360.05          87.688          169.88
v  r11                   0.0010592         0.08194        0.013071        0.018284
v  r22                   0.0011108        0.082627        0.013351        0.018644
v  r33                   0.0016345         0.17429        0.027244        0.037203
v  r12                   -0.010667        0.013572     -0.00023377     -0.00030928
v  r13                    -0.04556        0.052799      9.2946e-05       0.0010137
v  r23                   -0.046707        0.051241      3.0214e-05      0.00057445
v  epsilon                0.068732          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9897e-05       0.0099178      0.00092459       0.0017425
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017872          5.2776         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71349         0.85283


 TIME FOR THE TIME STEP            10271:        0.12600E+03

===============================================================


 INSTANT    0.102720000E-01   TIME STEP NUMBER           10272
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.639601274E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.610878462E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181110716E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935029E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.603670675E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232006631E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69788E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81212E-03   0.45293E-02 0.19900E+01 
c  Velocity[X]                                      0.13804E-03 
c  Velocity[Y]                                      0.12901E-03 
c  Velocity[Z]                                      0.42622E-02 
c  Pressure     0.36715E-04     132   0.93497E-02   0.25898E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55196E-08   0.16559E-08 0.10059E+00 
c  r22          0.10851E-01      13   0.49887E-08   0.18350E-08 0.10211E+00 
c  r33          0.21858E-01      15   0.61274E-08   0.12633E-07 0.12846E+00 
c  r12          0.93850E-03      18   0.55414E-08   0.30391E-09 0.60912E+00 
c  r13          0.46671E-02      19   0.58313E-08   0.15049E-08 0.20098E+00 
c  r23          0.39972E-02      19   0.70093E-08   0.12959E-08 0.20046E+00 
c  epsilon      0.10970E+02      11   0.34835E-08   0.99618E-02 0.16739E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.84458E-02 0.43355E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162017


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361         0.61355       0.0052548       0.0015072
v  Velocity[Y]            -0.57328         0.54437       0.0030799      0.00087338
v  Velocity[Z]              1.5657          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4374          4.3406          4.3632
v  Pressure                -36.432          359.99          87.624          169.82
v  r11                   0.0010592        0.081944        0.013071        0.018284
v  r22                   0.0011108        0.082628        0.013351        0.018644
v  r33                   0.0016345         0.17427        0.027244        0.037203
v  r12                   -0.010666        0.013567     -0.00023377     -0.00030928
v  r13                   -0.045559          0.0528      9.2946e-05       0.0010137
v  r23                   -0.046706        0.051236      3.0215e-05      0.00057445
v  epsilon                0.068733          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9896e-05       0.0099175      0.00092459       0.0017425
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb             0.0017872          5.2779         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71349         0.85283


 TIME FOR THE TIME STEP            10272:        0.91729E+02

===============================================================


 INSTANT    0.102730000E-01   TIME STEP NUMBER           10273
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.380272794E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.229987431E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229353515E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.418435349E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.720267342E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81144E-03   0.45203E-02 0.19919E+01 
c  Velocity[X]                                      0.13852E-03 
c  Velocity[Y]                                      0.12870E-03 
c  Velocity[Z]                                      0.42531E-02 
c  Pressure     0.36364E-04     133   0.92554E-02   0.25651E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56655E-08   0.16317E-08 0.10005E+00 
c  r22          0.10851E-01      13   0.54203E-08   0.18358E-08 0.10210E+00 
c  r33          0.21858E-01      15   0.57147E-08   0.12520E-07 0.12824E+00 
c  r12          0.93850E-03      18   0.58371E-08   0.29854E-09 0.60711E+00 
c  r13          0.46672E-02      19   0.57722E-08   0.14941E-08 0.20072E+00 
c  r23          0.39972E-02      20   0.57181E-08   0.12853E-08 0.20063E+00 
c  epsilon      0.10970E+02      11   0.35189E-08   0.97550E-02 0.16467E+00 
c  TempC        0.25716E+06      16   0.15095E-04   0.83881E-02 0.43212E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63362         0.61358       0.0052549       0.0015072
v  Velocity[Y]            -0.57328         0.54445         0.00308      0.00087344
v  Velocity[Z]              1.5656          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.438          360.09           87.67          169.89
v  r11                   0.0010592        0.081953        0.013071        0.018284
v  r22                   0.0011108        0.082629        0.013351        0.018644
v  r33                   0.0016345         0.17429        0.027244        0.037203
v  r12                   -0.010664        0.013568     -0.00023377     -0.00030928
v  r13                   -0.045563        0.052798      9.2947e-05       0.0010137
v  r23                   -0.046707        0.051257      3.0215e-05      0.00057445
v  epsilon                0.068735          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9897e-05       0.0099173      0.00092459       0.0017425
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017871          5.2775         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71349         0.85283


 TIME FOR THE TIME STEP            10273:        0.96298E+02

===============================================================


 INSTANT    0.102740000E-01   TIME STEP NUMBER           10274
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.204374701E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237736718E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.748908727E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.219104213E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.232776398E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81213E-03   0.45567E-02 0.20008E+01 
c  Velocity[X]                                      0.13956E-03 
c  Velocity[Y]                                      0.12991E-03 
c  Velocity[Z]                                      0.42872E-02 
c  Pressure     0.36441E-04     133   0.92771E-02   0.25706E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56361E-08   0.16459E-08 0.10014E+00 
c  r22          0.10851E-01      13   0.49953E-08   0.18143E-08 0.10132E+00 
c  r33          0.21858E-01      15   0.56697E-08   0.12548E-07 0.12790E+00 
c  r12          0.93850E-03      18   0.56651E-08   0.30034E-09 0.60885E+00 
c  r13          0.46672E-02      19   0.62026E-08   0.14959E-08 0.19995E+00 
c  r23          0.39972E-02      19   0.74345E-08   0.12830E-08 0.20040E+00 
c  epsilon      0.10970E+02      11   0.33733E-08   0.99983E-02 0.17011E+00 
c  TempC        0.25716E+06      16   0.15179E-04   0.85371E-02 0.43560E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162019


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63371         0.61356       0.0052549       0.0015072
v  Velocity[Y]            -0.57322         0.54425       0.0030799      0.00087337
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.451          360.01          87.656          169.84
v  r11                   0.0010592        0.081957        0.013071        0.018284
v  r22                   0.0011108        0.082631        0.013351        0.018644
v  r33                   0.0016345         0.17431        0.027245        0.037203
v  r12                   -0.010662        0.013568     -0.00023378     -0.00030928
v  r13                    -0.04556        0.052801      9.2948e-05       0.0010137
v  r23                   -0.046708        0.051241      3.0216e-05      0.00057445
v  epsilon                0.068736          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9898e-05       0.0099173      0.00092459       0.0017425
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017871          5.2775         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71349         0.85283


 TIME FOR THE TIME STEP            10274:        0.96771E+02

===============================================================


 INSTANT    0.102750000E-01   TIME STEP NUMBER           10275
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.217789039E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.702956909E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.230922203E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.408665825E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294341647E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81246E-03   0.45132E-02 0.19886E+01 
c  Velocity[X]                                      0.13985E-03 
c  Velocity[Y]                                      0.12863E-03 
c  Velocity[Z]                                      0.42448E-02 
c  Pressure     0.36383E-04     133   0.92624E-02   0.25664E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.62459E-08   0.16268E-08 0.99130E-01 
c  r22          0.10851E-01      13   0.49243E-08   0.18118E-08 0.10092E+00 
c  r33          0.21858E-01      15   0.55250E-08   0.12374E-07 0.12657E+00 
c  r12          0.93850E-03      18   0.59309E-08   0.29787E-09 0.60305E+00 
c  r13          0.46672E-02      20   0.66288E-08   0.14862E-08 0.19914E+00 
c  r23          0.39972E-02      20   0.56929E-08   0.12598E-08 0.19686E+00 
c  epsilon      0.10970E+02      11   0.33190E-08   0.97789E-02 0.16472E+00 
c  TempC        0.25716E+06      16   0.15103E-04   0.84745E-02 0.43389E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162017


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63365         0.61353       0.0052549       0.0015072
v  Velocity[Y]            -0.57335         0.54433       0.0030799      0.00087339
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.418          360.11          87.694          169.92
v  r11                   0.0010592        0.081958        0.013071        0.018284
v  r22                   0.0011108        0.082633        0.013351        0.018645
v  r33                   0.0016345         0.17435        0.027245        0.037203
v  r12                   -0.010662        0.013564     -0.00023378     -0.00030928
v  r13                   -0.045559        0.052799      9.2948e-05       0.0010137
v  r23                   -0.046709        0.051231      3.0216e-05      0.00057445
v  epsilon                0.068737          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9901e-05       0.0099173      0.00092459       0.0017425
v  CourantNb               0.44257             0.6         0.59908         0.59839
v  FourierNb             0.0017871           5.278         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878          0.7135         0.85283


 TIME FOR THE TIME STEP            10275:        0.25545E+03

===============================================================


 INSTANT    0.102760000E-01   TIME STEP NUMBER           10276
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.275119575E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.652201825E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.423464921E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.304059689E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.333233878E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81307E-03   0.45008E-02 0.19876E+01 
c  Velocity[X]                                      0.13830E-03 
c  Velocity[Y]                                      0.12855E-03 
c  Velocity[Z]                                      0.42340E-02 
c  Pressure     0.36607E-04     131   0.93207E-02   0.25822E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57694E-08   0.16363E-08 0.99304E-01 
c  r22          0.10851E-01      13   0.48859E-08   0.18360E-08 0.10143E+00 
c  r33          0.21858E-01      15   0.53549E-08   0.12602E-07 0.12731E+00 
c  r12          0.93850E-03      18   0.57071E-08   0.30508E-09 0.60504E+00 
c  r13          0.46672E-02      20   0.59201E-08   0.15097E-08 0.20029E+00 
c  r23          0.39972E-02      19   0.68817E-08   0.12911E-08 0.19872E+00 
c  epsilon      0.10970E+02      11   0.32300E-08   0.10099E-01 0.16668E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.83569E-02 0.43160E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162015


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63368         0.61358        0.005255       0.0015072
v  Velocity[Y]            -0.57336         0.54446       0.0030799      0.00087338
v  Velocity[Z]              1.5658          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4374          4.3406          4.3632
v  Pressure                -36.442          360.02          87.656          169.85
v  r11                   0.0010592        0.081954        0.013071        0.018285
v  r22                   0.0011108        0.082634        0.013351        0.018645
v  r33                   0.0016345         0.17433        0.027245        0.037203
v  r12                   -0.010664        0.013561     -0.00023378     -0.00030928
v  r13                   -0.045561        0.052799      9.2949e-05       0.0010137
v  r23                    -0.04671        0.051226      3.0217e-05      0.00057445
v  epsilon                0.068738           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc               5.99e-05       0.0099174       0.0009246       0.0017425
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017871          5.2784         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784          0.7135         0.85283


 TIME FOR THE TIME STEP            10276:        0.93464E+02

===============================================================


 INSTANT    0.102770000E-01   TIME STEP NUMBER           10277
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.197620281E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.412059550E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.482417033E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.416976137E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.878628089E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81135E-03   0.45229E-02 0.19941E+01 
c  Velocity[X]                                      0.13807E-03 
c  Velocity[Y]                                      0.12932E-03 
c  Velocity[Z]                                      0.42555E-02 
c  Pressure     0.36425E-04     131   0.92673E-02   0.25694E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59783E-08   0.16300E-08 0.99234E-01 
c  r22          0.10851E-01      13   0.47457E-08   0.18245E-08 0.10108E+00 
c  r33          0.21858E-01      15   0.54546E-08   0.12560E-07 0.12713E+00 
c  r12          0.93850E-03      18   0.61250E-08   0.29647E-09 0.60313E+00 
c  r13          0.46672E-02      20   0.57082E-08   0.15116E-08 0.20001E+00 
c  r23          0.39972E-02      19   0.60228E-08   0.12909E-08 0.19924E+00 
c  epsilon      0.10970E+02      11   0.33630E-08   0.10141E-01 0.16669E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.83713E-02 0.43214E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63371         0.61355       0.0052549       0.0015072
v  Velocity[Y]            -0.57328         0.54431       0.0030798      0.00087331
v  Velocity[Z]              1.5659          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5797          5.4374          4.3406          4.3632
v  Pressure                 -36.42          360.01          87.651          169.84
v  r11                   0.0010592         0.08195        0.013071        0.018285
v  r22                   0.0011108        0.082635        0.013351        0.018645
v  r33                   0.0016345         0.17429        0.027245        0.037203
v  r12                   -0.010665        0.013557     -0.00023378     -0.00030928
v  r13                    -0.04556          0.0528       9.295e-05       0.0010137
v  r23                   -0.046711        0.051258      3.0217e-05      0.00057445
v  epsilon                0.068739          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9899e-05       0.0099175       0.0009246       0.0017425
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017871          5.2785         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71349         0.85283


 TIME FOR THE TIME STEP            10277:        0.13382E+03

===============================================================


 INSTANT    0.102780000E-01   TIME STEP NUMBER           10278
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242731311E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.977716235E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195686970E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.990427439E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.186718414E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81213E-03   0.45308E-02 0.19913E+01 
c  Velocity[X]                                      0.13895E-03 
c  Velocity[Y]                                      0.13013E-03 
c  Velocity[Z]                                      0.42618E-02 
c  Pressure     0.36577E-04     132   0.93114E-02   0.25800E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59634E-08   0.16712E-08 0.10032E+00 
c  r22          0.10851E-01      13   0.49615E-08   0.18479E-08 0.10157E+00 
c  r33          0.21858E-01      15   0.70038E-08   0.12710E-07 0.12776E+00 
c  r12          0.93850E-03      18   0.59055E-08   0.29890E-09 0.60627E+00 
c  r13          0.46672E-02      20   0.58239E-08   0.15028E-08 0.20025E+00 
c  r23          0.39972E-02      19   0.61711E-08   0.12940E-08 0.19963E+00 
c  epsilon      0.10970E+02      11   0.36322E-08   0.10293E-01 0.16739E+00 
c  TempC        0.25716E+06      16   0.15125E-04   0.84559E-02 0.43330E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61353       0.0052549       0.0015072
v  Velocity[Y]            -0.57306         0.54424       0.0030799      0.00087334
v  Velocity[Z]              1.5656          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4374          4.3406          4.3632
v  Pressure                -36.419             360          87.648          169.84
v  r11                   0.0010592        0.081954        0.013071        0.018285
v  r22                   0.0011108        0.082637        0.013351        0.018645
v  r33                   0.0016345         0.17431        0.027245        0.037203
v  r12                   -0.010661        0.013557     -0.00023378     -0.00030928
v  r13                   -0.045559        0.052801      9.2952e-05       0.0010137
v  r23                   -0.046711         0.05125      3.0219e-05      0.00057446
v  epsilon                0.068741          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9899e-05       0.0099176       0.0009246       0.0017425
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017871          5.2784         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71349         0.85283


 TIME FOR THE TIME STEP            10278:        0.10162E+03

===============================================================


 INSTANT    0.102790000E-01   TIME STEP NUMBER           10279
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.137870704E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.251852886E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.588755874E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133257800E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.634561740E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81227E-03   0.45531E-02 0.19972E+01 
c  Velocity[X]                                      0.13882E-03 
c  Velocity[Y]                                      0.12850E-03 
c  Velocity[Z]                                      0.42858E-02 
c  Pressure     0.36993E-04     133   0.94159E-02   0.26095E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56481E-08   0.16350E-08 0.99710E-01 
c  r22          0.10851E-01      13   0.51021E-08   0.18546E-08 0.10240E+00 
c  r33          0.21858E-01      15   0.57705E-08   0.12530E-07 0.12768E+00 
c  r12          0.93850E-03      18   0.57187E-08   0.30436E-09 0.61256E+00 
c  r13          0.46672E-02      19   0.71231E-08   0.15082E-08 0.20133E+00 
c  r23          0.39972E-02      19   0.71356E-08   0.12799E-08 0.19890E+00 
c  epsilon      0.10970E+02      11   0.34799E-08   0.97120E-02 0.16318E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.83897E-02 0.43170E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61358       0.0052549       0.0015072
v  Velocity[Y]            -0.57306          0.5443       0.0030799      0.00087332
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.437          360.09          87.694          169.91
v  r11                   0.0010592        0.081956        0.013071        0.018285
v  r22                   0.0011108        0.082633        0.013351        0.018645
v  r33                   0.0016345         0.17433        0.027245        0.037203
v  r12                   -0.010657        0.013566     -0.00023378     -0.00030928
v  r13                   -0.045561        0.052801      9.2953e-05       0.0010137
v  r23                   -0.046711        0.051239       3.022e-05      0.00057446
v  epsilon                0.068742          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9901e-05       0.0099177       0.0009246       0.0017425
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb              0.001787           5.278         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85283


 TIME FOR THE TIME STEP            10279:        0.10180E+03

===============================================================


 INSTANT    0.102800000E-01   TIME STEP NUMBER           10280
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.105181904E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.342707886E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.377609898E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.799801194E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.259084261E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81163E-03   0.45664E-02 0.20032E+01 
c  Velocity[X]                                      0.13930E-03 
c  Velocity[Y]                                      0.12917E-03 
c  Velocity[Z]                                      0.42979E-02 
c  Pressure     0.36780E-04     133   0.93620E-02   0.25945E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59815E-08   0.16811E-08 0.10097E+00 
c  r22          0.10851E-01      13   0.52339E-08   0.18633E-08 0.10225E+00 
c  r33          0.21858E-01      15   0.60729E-08   0.12933E-07 0.12912E+00 
c  r12          0.93850E-03      18   0.62967E-08   0.30571E-09 0.61153E+00 
c  r13          0.46672E-02      20   0.72365E-08   0.15401E-08 0.20195E+00 
c  r23          0.39972E-02      19   0.73449E-08   0.13222E-08 0.20198E+00 
c  epsilon      0.10970E+02      11   0.34729E-08   0.10538E-01 0.17408E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.84394E-02 0.43369E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162015


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63357         0.61355        0.005255       0.0015072
v  Velocity[Y]              -0.573          0.5444       0.0030798      0.00087329
v  Velocity[Z]              1.5656          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4374          4.3406          4.3632
v  Pressure                -36.484          360.08          87.702          169.91
v  r11                   0.0010592        0.081963        0.013071        0.018285
v  r22                   0.0011108        0.082633        0.013351        0.018645
v  r33                   0.0016345         0.17431        0.027245        0.037203
v  r12                   -0.010657        0.013572     -0.00023378     -0.00030928
v  r13                   -0.045558        0.052801      9.2953e-05       0.0010137
v  r23                   -0.046711        0.051248       3.022e-05      0.00057446
v  epsilon                0.068743          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9901e-05       0.0099178       0.0009246       0.0017425
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb              0.001787          5.2779         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71349         0.85283


 TIME FOR THE TIME STEP            10280:        0.10142E+03

===============================================================


 INSTANT    0.102810000E-01   TIME STEP NUMBER           10281
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.733904373E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.762596992E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.271898718E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.415452445E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267528149E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81191E-03   0.45324E-02 0.19968E+01 
c  Velocity[X]                                      0.13929E-03 
c  Velocity[Y]                                      0.12872E-03 
c  Velocity[Z]                                      0.42644E-02 
c  Pressure     0.35921E-04     133   0.91435E-02   0.25339E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.65219E-08   0.16627E-08 0.10009E+00 
c  r22          0.10851E-01      13   0.53108E-08   0.18294E-08 0.10160E+00 
c  r33          0.21858E-01      15   0.52060E-08   0.12586E-07 0.12766E+00 
c  r12          0.93851E-03      18   0.60633E-08   0.29758E-09 0.60537E+00 
c  r13          0.46672E-02      20   0.67175E-08   0.14837E-08 0.19951E+00 
c  r23          0.39972E-02      19   0.70611E-08   0.12883E-08 0.19933E+00 
c  epsilon      0.10970E+02      11   0.33956E-08   0.99139E-02 0.16534E+00 
c  TempC        0.25716E+06      16   0.15122E-04   0.84737E-02 0.43472E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61352        0.005255       0.0015072
v  Velocity[Y]            -0.57299          0.5445       0.0030799      0.00087331
v  Velocity[Z]              1.5657          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4374          4.3406          4.3632
v  Pressure                -36.417          360.06          87.674          169.89
v  r11                   0.0010592         0.08196        0.013071        0.018285
v  r22                   0.0011108        0.082635        0.013351        0.018645
v  r33                   0.0016345         0.17427        0.027245        0.037203
v  r12                   -0.010658        0.013572     -0.00023378     -0.00030928
v  r13                   -0.045559          0.0528      9.2954e-05       0.0010137
v  r23                   -0.046712        0.051225      3.0221e-05      0.00057446
v  epsilon                0.068744          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc               5.99e-05       0.0099178       0.0009246       0.0017425
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb              0.001787           5.278         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85283


 TIME FOR THE TIME STEP            10281:        0.15974E+03

===============================================================


 INSTANT    0.102820000E-01   TIME STEP NUMBER           10282
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.795585783E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.581997418E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.131023800E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122394781E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232119952E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69787E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81201E-03   0.44870E-02 0.19842E+01 
c  Velocity[X]                                      0.13770E-03 
c  Velocity[Y]                                      0.12897E-03 
c  Velocity[Z]                                      0.42203E-02 
c  Pressure     0.36208E-04     133   0.92195E-02   0.25540E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.64759E-08   0.16553E-08 0.99362E-01 
c  r22          0.10851E-01      13   0.57840E-08   0.18584E-08 0.10176E+00 
c  r33          0.21858E-01      14   0.68658E-08   0.12729E-07 0.12747E+00 
c  r12          0.93851E-03      18   0.63054E-08   0.29861E-09 0.60328E+00 
c  r13          0.46672E-02      20   0.61187E-08   0.15057E-08 0.19962E+00 
c  r23          0.39972E-02      20   0.58514E-08   0.13070E-08 0.19945E+00 
c  epsilon      0.10970E+02      11   0.33046E-08   0.10377E-01 0.16809E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.84153E-02 0.43244E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63363         0.61357       0.0052549       0.0015072
v  Velocity[Y]              -0.573         0.54426       0.0030798      0.00087327
v  Velocity[Z]              1.5656          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4374          4.3406          4.3632
v  Pressure                -36.427          360.03          87.669          169.86
v  r11                   0.0010592        0.081956        0.013071        0.018285
v  r22                   0.0011108        0.082636        0.013351        0.018645
v  r33                   0.0016345         0.17429        0.027245        0.037203
v  r12                   -0.010661        0.013578     -0.00023378     -0.00030928
v  r13                   -0.045561        0.052803      9.2956e-05       0.0010137
v  r23                   -0.046712        0.051207      3.0222e-05      0.00057446
v  epsilon                0.068746          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9902e-05       0.0099178       0.0009246       0.0017425
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017869          5.2782         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71349         0.85283


 TIME FOR THE TIME STEP            10282:        0.19247E+03

===============================================================


 INSTANT    0.102830000E-01   TIME STEP NUMBER           10283
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157940027E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249226508E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.296881380E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171512356E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208524814E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81232E-03   0.45422E-02 0.19971E+01 
c  Velocity[X]                                      0.13973E-03 
c  Velocity[Y]                                      0.12967E-03 
c  Velocity[Z]                                      0.42728E-02 
c  Pressure     0.36800E-04     132   0.93705E-02   0.25958E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58868E-08   0.16415E-08 0.99236E-01 
c  r22          0.10851E-01      13   0.57477E-08   0.18345E-08 0.10139E+00 
c  r33          0.21858E-01      15   0.50057E-08   0.12504E-07 0.12684E+00 
c  r12          0.93851E-03      18   0.63908E-08   0.30600E-09 0.60708E+00 
c  r13          0.46672E-02      20   0.63958E-08   0.14874E-08 0.19925E+00 
c  r23          0.39972E-02      20   0.69556E-08   0.12696E-08 0.19737E+00 
c  epsilon      0.10970E+02      11   0.33007E-08   0.99721E-02 0.16573E+00 
c  TempC        0.25716E+06      16   0.15110E-04   0.83813E-02 0.43190E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63365         0.61356       0.0052549       0.0015072
v  Velocity[Y]            -0.57301         0.54432       0.0030798      0.00087328
v  Velocity[Z]              1.5658          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4374          4.3406          4.3632
v  Pressure                -36.418          360.03          87.651          169.85
v  r11                   0.0010592        0.081949        0.013071        0.018285
v  r22                   0.0011108        0.082637        0.013351        0.018645
v  r33                   0.0016345         0.17432        0.027245        0.037203
v  r12                   -0.010661        0.013581     -0.00023378     -0.00030928
v  r13                   -0.045559        0.052801      9.2956e-05       0.0010137
v  r23                   -0.046713        0.051185      3.0222e-05      0.00057446
v  epsilon                0.068747          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9905e-05       0.0099178       0.0009246       0.0017425
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017869          5.2786         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786          0.7135         0.85283


 TIME FOR THE TIME STEP            10283:        0.30669E+03

===============================================================


 INSTANT    0.102840000E-01   TIME STEP NUMBER           10284
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.307194374E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.142815624E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.357164472E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.121867842E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.238058655E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81230E-03   0.45247E-02 0.19917E+01 
c  Velocity[X]                                      0.13862E-03 
c  Velocity[Y]                                      0.12974E-03 
c  Velocity[Z]                                      0.42564E-02 
c  Pressure     0.36180E-04     133   0.92162E-02   0.25520E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55866E-08   0.16503E-08 0.99615E-01 
c  r22          0.10851E-01      13   0.55916E-08   0.18437E-08 0.10112E+00 
c  r33          0.21858E-01      15   0.57196E-08   0.12593E-07 0.12669E+00 
c  r12          0.93851E-03      18   0.60428E-08   0.30089E-09 0.60769E+00 
c  r13          0.46672E-02      20   0.57591E-08   0.15140E-08 0.19964E+00 
c  r23          0.39972E-02      20   0.63213E-08   0.12831E-08 0.19822E+00 
c  epsilon      0.10970E+02      11   0.33603E-08   0.10160E-01 0.16616E+00 
c  TempC        0.25716E+06      16   0.15171E-04   0.84570E-02 0.43374E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63372         0.61353       0.0052548       0.0015071
v  Velocity[Y]            -0.57301         0.54449       0.0030798      0.00087325
v  Velocity[Z]              1.5657          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4374          4.3406          4.3632
v  Pressure                -36.401          360.09          87.701          169.91
v  r11                   0.0010592        0.081942        0.013071        0.018285
v  r22                   0.0011108        0.082637        0.013351        0.018645
v  r33                   0.0016345          0.1743        0.027245        0.037203
v  r12                   -0.010663        0.013585     -0.00023378     -0.00030928
v  r13                   -0.045557        0.052801      9.2957e-05       0.0010137
v  r23                   -0.046713        0.051202      3.0223e-05      0.00057446
v  epsilon                0.068748          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9906e-05       0.0099177      0.00092461       0.0017425
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017869          5.2782         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71349         0.85282


 TIME FOR THE TIME STEP            10284:        0.37307E+03

===============================================================


 INSTANT    0.102850000E-01   TIME STEP NUMBER           10285
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.281538621E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.395398288E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.241847446E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.196270029E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.745534468E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69786E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81132E-03   0.45086E-02 0.19883E+01 
c  Velocity[X]                                      0.13795E-03 
c  Velocity[Y]                                      0.12882E-03 
c  Velocity[Z]                                      0.42418E-02 
c  Pressure     0.36213E-04     133   0.92188E-02   0.25544E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57520E-08   0.16120E-08 0.98764E-01 
c  r22          0.10851E-01      13   0.57886E-08   0.18073E-08 0.10070E+00 
c  r33          0.21858E-01      15   0.52525E-08   0.12353E-07 0.12618E+00 
c  r12          0.93851E-03      18   0.62368E-08   0.29252E-09 0.59832E+00 
c  r13          0.46672E-02      20   0.63269E-08   0.14868E-08 0.19831E+00 
c  r23          0.39972E-02      20   0.54972E-08   0.12610E-08 0.19705E+00 
c  epsilon      0.10970E+02      11   0.34740E-08   0.97985E-02 0.16515E+00 
c  TempC        0.25716E+06      16   0.15112E-04   0.83735E-02 0.43178E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61361       0.0052549       0.0015071
v  Velocity[Y]            -0.57302         0.54424       0.0030798      0.00087324
v  Velocity[Z]              1.5658          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4374          4.3406          4.3632
v  Pressure                -36.383          360.15          87.726          169.96
v  r11                   0.0010592        0.081931        0.013071        0.018285
v  r22                   0.0011107        0.082637        0.013351        0.018645
v  r33                   0.0016345         0.17428        0.027245        0.037203
v  r12                   -0.010662        0.013594     -0.00023378     -0.00030928
v  r13                    -0.04556        0.052799      9.2958e-05       0.0010137
v  r23                   -0.046713        0.051203      3.0224e-05      0.00057446
v  epsilon                0.068749          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9907e-05       0.0099176      0.00092461       0.0017425
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017869          5.2771         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71349         0.85283


 TIME FOR THE TIME STEP            10285:        0.26230E+03

===============================================================


 INSTANT    0.102860000E-01   TIME STEP NUMBER           10286
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.344393883E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182364374E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208131571E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.305716945E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.404780732E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81220E-03   0.45652E-02 0.20023E+01 
c  Velocity[X]                                      0.13926E-03 
c  Velocity[Y]                                      0.12946E-03 
c  Velocity[Z]                                      0.42965E-02 
c  Pressure     0.36531E-04     131   0.92985E-02   0.25768E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57138E-08   0.16435E-08 0.99853E-01 
c  r22          0.10851E-01      13   0.56666E-08   0.18110E-08 0.10114E+00 
c  r33          0.21858E-01      15   0.57972E-08   0.12498E-07 0.12741E+00 
c  r12          0.93851E-03      18   0.56969E-08   0.29713E-09 0.60303E+00 
c  r13          0.46672E-02      19   0.63824E-08   0.14950E-08 0.19954E+00 
c  r23          0.39972E-02      20   0.59270E-08   0.12916E-08 0.19981E+00 
c  epsilon      0.10970E+02      11   0.34902E-08   0.10107E-01 0.17135E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.83828E-02 0.43200E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6336         0.61358       0.0052549       0.0015071
v  Velocity[Y]            -0.57301         0.54422       0.0030798      0.00087325
v  Velocity[Z]              1.5659          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4374          4.3406          4.3632
v  Pressure                -36.428          359.96           87.63           169.8
v  r11                   0.0010592        0.081918        0.013071        0.018285
v  r22                   0.0011107        0.082636        0.013351        0.018645
v  r33                   0.0016345         0.17429        0.027245        0.037203
v  r12                   -0.010663        0.013594     -0.00023378     -0.00030928
v  r13                   -0.045558        0.052799      9.2959e-05       0.0010137
v  r23                   -0.046713        0.051196      3.0225e-05      0.00057446
v  epsilon                 0.06875          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9909e-05       0.0099175      0.00092461       0.0017425
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017869          5.2777         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71349         0.85283


 TIME FOR THE TIME STEP            10286:        0.27500E+03

===============================================================


 INSTANT    0.102870000E-01   TIME STEP NUMBER           10287
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.622623004E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.118416703E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.301455921E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.255931157E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158842040E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69785E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      40   0.81230E-03   0.45486E-02 0.19984E+01 
c  Velocity[X]                                      0.13884E-03 
c  Velocity[Y]                                      0.12887E-03 
c  Velocity[Z]                                      0.42809E-02 
c  Pressure     0.36299E-04     133   0.92391E-02   0.25604E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54659E-08   0.16489E-08 0.99490E-01 
c  r22          0.10851E-01      13   0.55647E-08   0.18339E-08 0.10108E+00 
c  r33          0.21858E-01      15   0.56761E-08   0.12582E-07 0.12665E+00 
c  r12          0.93851E-03      18   0.55893E-08   0.29894E-09 0.60357E+00 
c  r13          0.46672E-02      19   0.63814E-08   0.14810E-08 0.19859E+00 
c  r23          0.39972E-02      20   0.60450E-08   0.12811E-08 0.19786E+00 
c  epsilon      0.10970E+02      11   0.35274E-08   0.10254E-01 0.16703E+00 
c  TempC        0.25716E+06      16   0.15104E-04   0.84483E-02 0.43399E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63357         0.61356       0.0052549       0.0015071
v  Velocity[Y]            -0.57309         0.54435       0.0030799      0.00087331
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.414          360.05           87.68          169.88
v  r11                   0.0010592        0.081913        0.013071        0.018285
v  r22                   0.0011107         0.08263        0.013351        0.018645
v  r33                   0.0016345         0.17432        0.027245        0.037203
v  r12                   -0.010663        0.013588     -0.00023378     -0.00030928
v  r13                   -0.045557        0.052799       9.296e-05       0.0010137
v  r23                   -0.046713        0.051223      3.0226e-05      0.00057446
v  epsilon                0.068751          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9912e-05       0.0099175      0.00092461       0.0017425
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017869          5.2781         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781          0.7135         0.85283


 TIME FOR THE TIME STEP            10287:        0.18676E+03

===============================================================


 INSTANT    0.102880000E-01   TIME STEP NUMBER           10288
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.911722302E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.122687062E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.444334958E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.321248736E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.591136775E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69784E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81311E-03   0.44936E-02 0.19852E+01 
c  Velocity[X]                                      0.13845E-03 
c  Velocity[Y]                                      0.12874E-03 
c  Velocity[Z]                                      0.42264E-02 
c  Pressure     0.36452E-04     131   0.92773E-02   0.25712E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53426E-08   0.16486E-08 0.99578E-01 
c  r22          0.10851E-01      13   0.53476E-08   0.18471E-08 0.10116E+00 
c  r33          0.21858E-01      15   0.57950E-08   0.12712E-07 0.12715E+00 
c  r12          0.93851E-03      18   0.55755E-08   0.30452E-09 0.60543E+00 
c  r13          0.46672E-02      19   0.63476E-08   0.15178E-08 0.19954E+00 
c  r23          0.39972E-02      20   0.55564E-08   0.12955E-08 0.19926E+00 
c  epsilon      0.10970E+02      11   0.34424E-08   0.10193E-01 0.16708E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.84145E-02 0.43316E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61362       0.0052549       0.0015071
v  Velocity[Y]            -0.57297         0.54448       0.0030798      0.00087325
v  Velocity[Z]              1.5657          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4374          4.3406          4.3632
v  Pressure                -36.435           360.1          87.713          169.93
v  r11                   0.0010592        0.081916        0.013071        0.018285
v  r22                   0.0011107         0.08263        0.013351        0.018645
v  r33                   0.0016345         0.17429        0.027245        0.037203
v  r12                   -0.010669         0.01359     -0.00023378     -0.00030928
v  r13                   -0.045559        0.052799      9.2961e-05       0.0010137
v  r23                   -0.046712         0.05122      3.0227e-05      0.00057446
v  epsilon                0.068753          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099177      0.00092461       0.0017425
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017868          5.2781         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71349         0.85283


 TIME FOR THE TIME STEP            10288:        0.85562E+02

===============================================================


 INSTANT    0.102890000E-01   TIME STEP NUMBER           10289
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285837619E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.658409200E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.720831452E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.228478870E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.351402075E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69783E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81126E-03   0.45391E-02 0.19958E+01 
c  Velocity[X]                                      0.13914E-03 
c  Velocity[Y]                                      0.12913E-03 
c  Velocity[Z]                                      0.42709E-02 
c  Pressure     0.36599E-04     131   0.93106E-02   0.25817E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53069E-08   0.16431E-08 0.99949E-01 
c  r22          0.10851E-01      13   0.53845E-08   0.18570E-08 0.10241E+00 
c  r33          0.21858E-01      15   0.57428E-08   0.12676E-07 0.12843E+00 
c  r12          0.93851E-03      18   0.59018E-08   0.30064E-09 0.60723E+00 
c  r13          0.46672E-02      19   0.66022E-08   0.15119E-08 0.20095E+00 
c  r23          0.39972E-02      20   0.55955E-08   0.12972E-08 0.20087E+00 
c  epsilon      0.10970E+02      11   0.33252E-08   0.10016E-01 0.16659E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84295E-02 0.43259E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367          0.6136       0.0052549       0.0015071
v  Velocity[Y]            -0.57305         0.54425       0.0030798      0.00087321
v  Velocity[Z]              1.5658          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4374          4.3406          4.3632
v  Pressure                -36.389          360.04          87.673          169.88
v  r11                   0.0010591        0.081922        0.013071        0.018285
v  r22                   0.0011107        0.082632        0.013351        0.018645
v  r33                   0.0016345         0.17427        0.027245        0.037204
v  r12                   -0.010669        0.013586     -0.00023378     -0.00030928
v  r13                   -0.045559        0.052799      9.2961e-05       0.0010137
v  r23                    -0.04671          0.0512      3.0228e-05      0.00057446
v  epsilon                0.068754          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9919e-05       0.0099177      0.00092461       0.0017425
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017868          5.2782         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71349         0.85283


 TIME FOR THE TIME STEP            10289:        0.85899E+02

===============================================================


 INSTANT    0.102900000E-01   TIME STEP NUMBER           10290
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.111182319E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.471341765E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.492701920E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249054711E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.376095993E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81130E-03   0.45454E-02 0.19967E+01 
c  Velocity[X]                                      0.13945E-03 
c  Velocity[Y]                                      0.13014E-03 
c  Velocity[Z]                                      0.42758E-02 
c  Pressure     0.36336E-04     131   0.92534E-02   0.25629E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52023E-08   0.16786E-08 0.10138E+00 
c  r22          0.10851E-01      13   0.53438E-08   0.18415E-08 0.10229E+00 
c  r33          0.21858E-01      15   0.56241E-08   0.12602E-07 0.12853E+00 
c  r12          0.93851E-03      18   0.60113E-08   0.30561E-09 0.61151E+00 
c  r13          0.46672E-02      19   0.69759E-08   0.15013E-08 0.20062E+00 
c  r23          0.39972E-02      19   0.71898E-08   0.12974E-08 0.20225E+00 
c  epsilon      0.10970E+02      11   0.32788E-08   0.97612E-02 0.16485E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.84632E-02 0.43397E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61357       0.0052548       0.0015071
v  Velocity[Y]            -0.57299         0.54433       0.0030797      0.00087319
v  Velocity[Z]              1.5658          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4374          4.3406          4.3632
v  Pressure                -36.448          360.03          87.658          169.85
v  r11                   0.0010591        0.081923        0.013071        0.018285
v  r22                   0.0011107        0.082633        0.013351        0.018645
v  r33                   0.0016345         0.17429        0.027245        0.037204
v  r12                   -0.010667         0.01359     -0.00023378     -0.00030928
v  r13                   -0.045557        0.052798      9.2963e-05       0.0010137
v  r23                   -0.046709        0.051192      3.0229e-05      0.00057446
v  epsilon                0.068755          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099176      0.00092461       0.0017425
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017868          5.2783         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71349         0.85283


 TIME FOR THE TIME STEP            10290:        0.86900E+02

===============================================================


 INSTANT    0.102910000E-01   TIME STEP NUMBER           10291
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.246808212E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.388010695E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239218824E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133171315E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.495421694E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81369E-03   0.45430E-02 0.19937E+01 
c  Velocity[X]                                      0.13889E-03 
c  Velocity[Y]                                      0.12918E-03 
c  Velocity[Z]                                      0.42749E-02 
c  Pressure     0.36622E-04     131   0.93179E-02   0.25834E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52424E-08   0.16621E-08 0.10127E+00 
c  r22          0.10851E-01      13   0.51020E-08   0.18272E-08 0.10207E+00 
c  r33          0.21858E-01      14   0.68897E-08   0.12516E-07 0.12855E+00 
c  r12          0.93851E-03      18   0.61842E-08   0.30365E-09 0.61027E+00 
c  r13          0.46672E-02      19   0.71741E-08   0.15012E-08 0.20039E+00 
c  r23          0.39972E-02      19   0.68005E-08   0.13026E-08 0.20337E+00 
c  epsilon      0.10970E+02      11   0.31615E-08   0.94818E-02 0.16294E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.83921E-02 0.43253E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63362         0.61361       0.0052549       0.0015071
v  Velocity[Y]            -0.57301         0.54446       0.0030798      0.00087324
v  Velocity[Z]              1.5657          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4374          4.3406          4.3632
v  Pressure                -36.406          360.05          87.684          169.88
v  r11                   0.0010591         0.08192        0.013071        0.018285
v  r22                   0.0011107        0.082633        0.013351        0.018645
v  r33                   0.0016344         0.17431        0.027245        0.037204
v  r12                    -0.01067        0.013581     -0.00023378     -0.00030928
v  r13                   -0.045559        0.052793      9.2964e-05       0.0010137
v  r23                   -0.046708        0.051215       3.023e-05      0.00057446
v  epsilon                0.068756          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099174      0.00092461       0.0017425
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017868          5.2778         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71349         0.85282


 TIME FOR THE TIME STEP            10291:        0.86117E+02

===============================================================


 INSTANT    0.102920000E-01   TIME STEP NUMBER           10292
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.466543817E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.321557987E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117652182E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.323901956E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.103288444E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69782E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81172E-03   0.45334E-02 0.19944E+01 
c  Velocity[X]                                      0.13898E-03 
c  Velocity[Y]                                      0.12904E-03 
c  Velocity[Z]                                      0.42654E-02 
c  Pressure     0.36155E-04     132   0.92032E-02   0.25502E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52605E-08   0.17640E-08 0.10337E+00 
c  r22          0.10851E-01      13   0.54435E-08   0.18771E-08 0.10279E+00 
c  r33          0.21858E-01      14   0.68177E-08   0.13281E-07 0.13116E+00 
c  r12          0.93851E-03      18   0.67323E-08   0.31211E-09 0.61860E+00 
c  r13          0.46672E-02      19   0.59221E-08   0.15324E-08 0.20200E+00 
c  r23          0.39972E-02      19   0.60633E-08   0.13773E-08 0.20852E+00 
c  epsilon      0.10970E+02      11   0.31936E-08   0.10576E-01 0.17396E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.84198E-02 0.43308E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63368         0.61357       0.0052548       0.0015071
v  Velocity[Y]            -0.57288         0.54416       0.0030797      0.00087319
v  Velocity[Z]              1.5656          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4374          4.3406          4.3632
v  Pressure                -36.426          359.97          87.633          169.82
v  r11                   0.0010591         0.08192        0.013071        0.018285
v  r22                   0.0011107        0.082631        0.013351        0.018645
v  r33                   0.0016344          0.1743        0.027245        0.037204
v  r12                    -0.01067        0.013575     -0.00023378     -0.00030928
v  r13                   -0.045557        0.052791      9.2964e-05       0.0010137
v  r23                   -0.046706        0.051209      3.0231e-05      0.00057446
v  epsilon                0.068757          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099175      0.00092462       0.0017425
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017868          5.2773         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71349         0.85282


 TIME FOR THE TIME STEP            10292:        0.86077E+02

===============================================================


 INSTANT    0.102930000E-01   TIME STEP NUMBER           10293
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.401986109E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.567714569E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.199018505E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.144193371E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105316659E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81182E-03   0.45208E-02 0.19916E+01 
c  Velocity[X]                                      0.13908E-03 
c  Velocity[Y]                                      0.12904E-03 
c  Velocity[Z]                                      0.42526E-02 
c  Pressure     0.36196E-04     134   0.92157E-02   0.25532E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56107E-08   0.16285E-08 0.10022E+00 
c  r22          0.10851E-01      13   0.54961E-08   0.18076E-08 0.10158E+00 
c  r33          0.21858E-01      15   0.55392E-08   0.12353E-07 0.12751E+00 
c  r12          0.93851E-03      18   0.67284E-08   0.29556E-09 0.60747E+00 
c  r13          0.46672E-02      19   0.57691E-08   0.14839E-08 0.19984E+00 
c  r23          0.39972E-02      19   0.70671E-08   0.12607E-08 0.19890E+00 
c  epsilon      0.10970E+02      11   0.32728E-08   0.95793E-02 0.16364E+00 
c  TempC        0.25716E+06      16   0.15127E-04   0.84289E-02 0.43306E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364         0.61354       0.0052549       0.0015072
v  Velocity[Y]            -0.57303         0.54415       0.0030798      0.00087322
v  Velocity[Z]              1.5657          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4374          4.3406          4.3632
v  Pressure                 -36.44          360.13          87.714          169.94
v  r11                   0.0010591        0.081921        0.013071        0.018285
v  r22                   0.0011108        0.082629        0.013351        0.018645
v  r33                   0.0016344         0.17427        0.027245        0.037204
v  r12                   -0.010666        0.013573     -0.00023378     -0.00030928
v  r13                   -0.045558         0.05279      9.2965e-05       0.0010137
v  r23                   -0.046705        0.051202      3.0232e-05      0.00057446
v  epsilon                0.068759          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099175      0.00092462       0.0017425
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017867           5.277         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71349         0.85283


 TIME FOR THE TIME STEP            10293:        0.82654E+02

===============================================================


 INSTANT    0.102940000E-01   TIME STEP NUMBER           10294
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.338499377E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.136851535E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150936336E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.217545464E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.462252781E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      40   0.81282E-03   0.45245E-02 0.19914E+01 
c  Velocity[X]                                      0.13826E-03 
c  Velocity[Y]                                      0.12891E-03 
c  Velocity[Z]                                      0.42573E-02 
c  Pressure     0.36609E-04     131   0.93232E-02   0.25823E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60750E-08   0.16920E-08 0.10183E+00 
c  r22          0.10851E-01      13   0.54163E-08   0.18240E-08 0.10185E+00 
c  r33          0.21858E-01      15   0.52317E-08   0.12699E-07 0.12907E+00 
c  r12          0.93851E-03      18   0.68879E-08   0.29671E-09 0.60913E+00 
c  r13          0.46672E-02      19   0.61194E-08   0.14943E-08 0.19964E+00 
c  r23          0.39972E-02      19   0.74076E-08   0.13243E-08 0.20369E+00 
c  epsilon      0.10970E+02      11   0.31988E-08   0.96556E-02 0.16276E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.83912E-02 0.43212E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63366         0.61359       0.0052549       0.0015071
v  Velocity[Y]            -0.57295         0.54428       0.0030797      0.00087315
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.475          360.04           87.67          169.88
v  r11                   0.0010591        0.081926        0.013071        0.018285
v  r22                   0.0011108        0.082628        0.013351        0.018645
v  r33                   0.0016344         0.17428        0.027245        0.037204
v  r12                   -0.010666        0.013581     -0.00023378     -0.00030928
v  r13                    -0.04556        0.052792      9.2965e-05       0.0010137
v  r23                   -0.046704        0.051199      3.0233e-05      0.00057446
v  epsilon                 0.06876          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099175      0.00092462       0.0017425
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017867          5.2765         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765          0.7135         0.85283


 TIME FOR THE TIME STEP            10294:        0.86572E+02

===============================================================


 INSTANT    0.102950000E-01   TIME STEP NUMBER           10295
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.197448507E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.573868485E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294142668E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.347796535E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.126564788E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81292E-03   0.45468E-02 0.19962E+01 
c  Velocity[X]                                      0.13856E-03 
c  Velocity[Y]                                      0.12967E-03 
c  Velocity[Z]                                      0.42786E-02 
c  Pressure     0.36615E-04     134   0.93189E-02   0.25828E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59398E-08   0.16501E-08 0.10082E+00 
c  r22          0.10851E-01      13   0.56408E-08   0.18474E-08 0.10273E+00 
c  r33          0.21858E-01      15   0.63331E-08   0.12558E-07 0.12853E+00 
c  r12          0.93851E-03      18   0.70452E-08   0.29874E-09 0.60599E+00 
c  r13          0.46672E-02      19   0.72077E-08   0.15169E-08 0.20205E+00 
c  r23          0.39972E-02      20   0.61291E-08   0.12847E-08 0.20037E+00 
c  epsilon      0.10970E+02      11   0.33774E-08   0.98426E-02 0.16443E+00 
c  TempC        0.25716E+06      16   0.15108E-04   0.84423E-02 0.43360E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61355       0.0052549       0.0015072
v  Velocity[Y]            -0.57304          0.5444       0.0030798      0.00087319
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.422          360.03          87.662          169.86
v  r11                   0.0010591        0.081925        0.013071        0.018285
v  r22                   0.0011108        0.082623        0.013351        0.018645
v  r33                   0.0016344         0.17431        0.027245        0.037204
v  r12                   -0.010668        0.013581     -0.00023378     -0.00030928
v  r13                   -0.045557         0.05279      9.2967e-05       0.0010137
v  r23                   -0.046703        0.051222      3.0234e-05      0.00057446
v  epsilon                0.068761          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099176      0.00092462       0.0017425
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017867          5.2765         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765          0.7135         0.85283


 TIME FOR THE TIME STEP            10295:        0.10871E+03

===============================================================


 INSTANT    0.102960000E-01   TIME STEP NUMBER           10296
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.170223766E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.962551867E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.813748318E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.973833418E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.209603064E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81186E-03   0.45261E-02 0.19933E+01 
c  Velocity[X]                                      0.13950E-03 
c  Velocity[Y]                                      0.13021E-03 
c  Velocity[Z]                                      0.42564E-02 
c  Pressure     0.36968E-04     131   0.94123E-02   0.26076E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56655E-08   0.17171E-08 0.10235E+00 
c  r22          0.10851E-01      13   0.53239E-08   0.18622E-08 0.10292E+00 
c  r33          0.21858E-01      15   0.62103E-08   0.12937E-07 0.12986E+00 
c  r12          0.93851E-03      18   0.62789E-08   0.31094E-09 0.61590E+00 
c  r13          0.46672E-02      19   0.72192E-08   0.15331E-08 0.20243E+00 
c  r23          0.39972E-02      20   0.55753E-08   0.13273E-08 0.20309E+00 
c  epsilon      0.10970E+02      11   0.34589E-08   0.10291E-01 0.16787E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.84221E-02 0.43321E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61352       0.0052549       0.0015072
v  Velocity[Y]            -0.57297         0.54421       0.0030797      0.00087318
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.469          360.01          87.638          169.84
v  r11                   0.0010591        0.081928        0.013071        0.018285
v  r22                   0.0011108        0.082623        0.013351        0.018645
v  r33                   0.0016344         0.17429        0.027245        0.037204
v  r12                    -0.01067        0.013587     -0.00023378     -0.00030928
v  r13                   -0.045556        0.052788      9.2968e-05       0.0010137
v  r23                   -0.046702        0.051212      3.0236e-05      0.00057446
v  epsilon                0.068762          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099177      0.00092462       0.0017425
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017867          5.2772         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772          0.7135         0.85283


 TIME FOR THE TIME STEP            10296:        0.11665E+03

===============================================================


 INSTANT    0.102970000E-01   TIME STEP NUMBER           10297
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182418543E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276845439E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.524804615E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.441659337E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.125324697E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81200E-03   0.45145E-02 0.19925E+01 
c  Velocity[X]                                      0.13746E-03 
c  Velocity[Y]                                      0.12826E-03 
c  Velocity[Z]                                      0.42487E-02 
c  Pressure     0.36109E-04     133   0.91888E-02   0.25470E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59056E-08   0.16373E-08 0.10039E+00 
c  r22          0.10851E-01      13   0.51683E-08   0.18177E-08 0.10170E+00 
c  r33          0.21858E-01      15   0.74326E-08   0.12341E-07 0.12751E+00 
c  r12          0.93851E-03      18   0.59798E-08   0.29618E-09 0.60466E+00 
c  r13          0.46672E-02      20   0.61216E-08   0.14789E-08 0.19977E+00 
c  r23          0.39972E-02      19   0.67758E-08   0.12765E-08 0.19947E+00 
c  epsilon      0.10970E+02      11   0.35344E-08   0.95744E-02 0.16257E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.84080E-02 0.43264E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61357        0.005255       0.0015072
v  Velocity[Y]            -0.57302         0.54414       0.0030798      0.00087321
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.456           360.1          87.697          169.92
v  r11                   0.0010591        0.081926        0.013071        0.018285
v  r22                   0.0011108        0.082623        0.013351        0.018645
v  r33                   0.0016344         0.17427        0.027245        0.037204
v  r12                   -0.010668        0.013586     -0.00023378     -0.00030928
v  r13                    -0.04556        0.052785      9.2969e-05       0.0010137
v  r23                   -0.046702        0.051211      3.0236e-05      0.00057446
v  epsilon                0.068763          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099175      0.00092462       0.0017425
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017867           5.277         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71349         0.85283


 TIME FOR THE TIME STEP            10297:        0.11922E+03

===============================================================


 INSTANT    0.102980000E-01   TIME STEP NUMBER           10298
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.344345666E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249157207E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.280292002E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.118929607E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.342397488E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81229E-03   0.45458E-02 0.19973E+01 
c  Velocity[X]                                      0.13838E-03 
c  Velocity[Y]                                      0.12922E-03 
c  Velocity[Z]                                      0.42782E-02 
c  Pressure     0.36586E-04     133   0.93109E-02   0.25807E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53625E-08   0.16828E-08 0.10175E+00 
c  r22          0.10851E-01      13   0.50587E-08   0.18241E-08 0.10202E+00 
c  r33          0.21858E-01      15   0.55978E-08   0.12727E-07 0.12932E+00 
c  r12          0.93851E-03      18   0.61544E-08   0.29692E-09 0.60908E+00 
c  r13          0.46672E-02      19   0.63030E-08   0.15058E-08 0.20114E+00 
c  r23          0.39972E-02      19   0.63095E-08   0.13207E-08 0.20349E+00 
c  epsilon      0.10970E+02      11   0.34561E-08   0.10119E-01 0.17013E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84228E-02 0.43308E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61355       0.0052549       0.0015071
v  Velocity[Y]            -0.57291          0.5442       0.0030797      0.00087317
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.431          360.03          87.685          169.87
v  r11                   0.0010591        0.081927        0.013071        0.018285
v  r22                   0.0011108        0.082623        0.013351        0.018645
v  r33                   0.0016344         0.17428        0.027245        0.037204
v  r12                    -0.01067        0.013583     -0.00023378     -0.00030928
v  r13                   -0.045557        0.052784       9.297e-05       0.0010137
v  r23                   -0.046702        0.051232      3.0237e-05      0.00057447
v  epsilon                0.068765          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099176      0.00092462       0.0017425
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017866          5.2775         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71349         0.85283


 TIME FOR THE TIME STEP            10298:        0.10204E+03

===============================================================


 INSTANT    0.102990000E-01   TIME STEP NUMBER           10299
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123686407E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173079206E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.211942299E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935021E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.233647004E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.295682074E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      40   0.81249E-03   0.45717E-02 0.20019E+01 
c  Velocity[X]                                      0.13990E-03 
c  Velocity[Y]                                      0.12924E-03 
c  Velocity[Z]                                      0.43025E-02 
c  Pressure     0.36736E-04     131   0.93524E-02   0.25912E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55095E-08   0.16335E-08 0.10021E+00 
c  r22          0.10851E-01      13   0.48944E-08   0.18162E-08 0.10186E+00 
c  r33          0.21858E-01      15   0.54043E-08   0.12441E-07 0.12783E+00 
c  r12          0.93851E-03      18   0.59208E-08   0.29467E-09 0.60704E+00 
c  r13          0.46672E-02      19   0.64014E-08   0.14879E-08 0.20056E+00 
c  r23          0.39972E-02      19   0.71438E-08   0.12721E-08 0.19977E+00 
c  epsilon      0.10970E+02      11   0.33698E-08   0.96768E-02 0.16322E+00 
c  TempC        0.25716E+06      16   0.15120E-04   0.84706E-02 0.43362E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338         0.61351        0.005255       0.0015072
v  Velocity[Y]            -0.57317         0.54432       0.0030797      0.00087316
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                  -36.4          360.06          87.669          169.88
v  r11                   0.0010591        0.081931        0.013071        0.018285
v  r22                   0.0011108        0.082621        0.013351        0.018645
v  r33                   0.0016344         0.17431        0.027245        0.037204
v  r12                   -0.010668        0.013582     -0.00023378     -0.00030928
v  r13                   -0.045556        0.052783      9.2971e-05       0.0010137
v  r23                   -0.046701        0.051223      3.0239e-05      0.00057447
v  epsilon                0.068766          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099179      0.00092462       0.0017425
v  CourantNb               0.44262             0.6         0.59908         0.59839
v  FourierNb             0.0017866          5.2773         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773          0.7135         0.85283


 TIME FOR THE TIME STEP            10299:        0.10067E+03

===============================================================


 INSTANT    0.103000000E-01   TIME STEP NUMBER           10300
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.291753646E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.216108952E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.931152411E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.287134541E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.434112745E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81313E-03   0.45046E-02 0.19874E+01 
c  Velocity[X]                                      0.13879E-03 
c  Velocity[Y]                                      0.12838E-03 
c  Velocity[Z]                                      0.42374E-02 
c  Pressure     0.36114E-04     133   0.91947E-02   0.25474E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54362E-08   0.16465E-08 0.10055E+00 
c  r22          0.10851E-01      13   0.48584E-08   0.18362E-08 0.10177E+00 
c  r33          0.21858E-01      15   0.56243E-08   0.12529E-07 0.12765E+00 
c  r12          0.93851E-03      18   0.64293E-08   0.29541E-09 0.60506E+00 
c  r13          0.46672E-02      19   0.62042E-08   0.15061E-08 0.20060E+00 
c  r23          0.39972E-02      19   0.68507E-08   0.12725E-08 0.19999E+00 
c  epsilon      0.10970E+02      11   0.33941E-08   0.98005E-02 0.16285E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.83621E-02 0.43155E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61356       0.0052549       0.0015072
v  Velocity[Y]            -0.57306         0.54412       0.0030798      0.00087318
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.465          360.02          87.656          169.86
v  r11                   0.0010591        0.081925        0.013071        0.018285
v  r22                   0.0011108        0.082622        0.013351        0.018645
v  r33                   0.0016344         0.17434        0.027245        0.037204
v  r12                   -0.010675        0.013575     -0.00023378     -0.00030928
v  r13                   -0.045558        0.052786      9.2972e-05       0.0010137
v  r23                   -0.046702        0.051204      3.0239e-05      0.00057447
v  epsilon                0.068767          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05        0.009918      0.00092462       0.0017425
v  CourantNb               0.44264             0.6         0.59908         0.59839
v  FourierNb             0.0017866          5.2776         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71349         0.85283


 TIME FOR THE TIME STEP            10300:        0.12908E+03

===============================================================


 INSTANT    0.103010000E-01   TIME STEP NUMBER           10301
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.885942049E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.380616510E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.181263263E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.400810645E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.426891133E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81108E-03   0.45429E-02 0.19954E+01 
c  Velocity[X]                                      0.13815E-03 
c  Velocity[Y]                                      0.12909E-03 
c  Velocity[Z]                                      0.42757E-02 
c  Pressure     0.36280E-04     132   0.92400E-02   0.25591E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53783E-08   0.16252E-08 0.99997E-01 
c  r22          0.10851E-01      13   0.46206E-08   0.18288E-08 0.10211E+00 
c  r33          0.21858E-01      15   0.53468E-08   0.12451E-07 0.12777E+00 
c  r12          0.93851E-03      18   0.60897E-08   0.29605E-09 0.60461E+00 
c  r13          0.46672E-02      19   0.65520E-08   0.14963E-08 0.20080E+00 
c  r23          0.39972E-02      20   0.58718E-08   0.12889E-08 0.20033E+00 
c  epsilon      0.10970E+02      11   0.32655E-08   0.97447E-02 0.16492E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.84035E-02 0.43256E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63377         0.61352        0.005255       0.0015072
v  Velocity[Y]             -0.5731         0.54423       0.0030798      0.00087318
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                  -36.4          360.04          87.651          169.86
v  r11                   0.0010591        0.081926        0.013071        0.018285
v  r22                   0.0011108        0.082623        0.013351        0.018645
v  r33                   0.0016344         0.17433        0.027245        0.037204
v  r12                   -0.010675        0.013576     -0.00023378     -0.00030928
v  r13                   -0.045558        0.052785      9.2973e-05       0.0010137
v  r23                   -0.046702        0.051219       3.024e-05      0.00057447
v  epsilon                0.068768           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099178      0.00092463       0.0017425
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017866          5.2782         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782          0.7135         0.85284


 TIME FOR THE TIME STEP            10301:        0.99980E+02

===============================================================


 INSTANT    0.103020000E-01   TIME STEP NUMBER           10302
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.338860981E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205282907E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.357860024E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.574242836E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.266707936E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81188E-03   0.45486E-02 0.19957E+01 
c  Velocity[X]                                      0.13856E-03 
c  Velocity[Y]                                      0.13002E-03 
c  Velocity[Z]                                      0.42801E-02 
c  Pressure     0.36691E-04     131   0.93438E-02   0.25879E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52029E-08   0.16428E-08 0.10010E+00 
c  r22          0.10851E-01      13   0.50992E-08   0.18213E-08 0.10152E+00 
c  r33          0.21858E-01      14   0.70413E-08   0.12575E-07 0.12779E+00 
c  r12          0.93851E-03      18   0.67229E-08   0.29244E-09 0.60353E+00 
c  r13          0.46672E-02      19   0.63745E-08   0.14819E-08 0.20007E+00 
c  r23          0.39972E-02      19   0.65756E-08   0.12794E-08 0.19957E+00 
c  epsilon      0.10970E+02      11   0.33722E-08   0.10001E-01 0.16753E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84952E-02 0.43490E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61348       0.0052549       0.0015071
v  Velocity[Y]            -0.57303         0.54442       0.0030798      0.00087318
v  Velocity[Z]              1.5652          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.433          360.01          87.657          169.84
v  r11                   0.0010591        0.081921        0.013071        0.018285
v  r22                   0.0011108        0.082623        0.013351        0.018645
v  r33                   0.0016345         0.17429        0.027245        0.037204
v  r12                   -0.010674         0.01357     -0.00023378     -0.00030928
v  r13                   -0.045556        0.052787      9.2973e-05       0.0010137
v  r23                   -0.046703        0.051209      3.0241e-05      0.00057447
v  epsilon                0.068769          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099177      0.00092463       0.0017425
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017866          5.2789         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789          0.7135         0.85283


 TIME FOR THE TIME STEP            10302:        0.10500E+03

===============================================================


 INSTANT    0.103030000E-01   TIME STEP NUMBER           10303
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.171005980E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.434560040E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151039617E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.677993836E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.527576111E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81312E-03   0.44953E-02 0.19871E+01 
c  Velocity[X]                                      0.13797E-03 
c  Velocity[Y]                                      0.12898E-03 
c  Velocity[Z]                                      0.42284E-02 
c  Pressure     0.36318E-04     134   0.92425E-02   0.25617E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.50917E-08   0.16483E-08 0.10007E+00 
c  r22          0.10851E-01      13   0.51104E-08   0.18152E-08 0.10112E+00 
c  r33          0.21858E-01      15   0.52726E-08   0.12491E-07 0.12698E+00 
c  r12          0.93851E-03      19   0.55393E-08   0.29622E-09 0.60270E+00 
c  r13          0.46672E-02      19   0.68238E-08   0.14912E-08 0.19946E+00 
c  r23          0.39972E-02      19   0.59994E-08   0.12878E-08 0.19945E+00 
c  epsilon      0.10970E+02      11   0.35152E-08   0.10069E-01 0.16758E+00 
c  TempC        0.25716E+06      16   0.15078E-04   0.83836E-02 0.43163E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61356       0.0052549       0.0015071
v  Velocity[Y]            -0.57306         0.54409       0.0030798       0.0008732
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.407          360.09          87.688           169.9
v  r11                   0.0010591        0.081919        0.013071        0.018285
v  r22                   0.0011108        0.082618        0.013351        0.018645
v  r33                   0.0016344          0.1743        0.027245        0.037204
v  r12                   -0.010667        0.013563     -0.00023378     -0.00030928
v  r13                   -0.045559        0.052785      9.2974e-05       0.0010137
v  r23                   -0.046704        0.051205      3.0242e-05      0.00057447
v  epsilon                0.068771          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099177      0.00092463       0.0017425
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017865          5.2785         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785          0.7135         0.85283


 TIME FOR THE TIME STEP            10303:        0.11883E+03

===============================================================


 INSTANT    0.103040000E-01   TIME STEP NUMBER           10304
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.275059940E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.206891557E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.942781245E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935016E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.142756980E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.153675742E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81216E-03   0.45420E-02 0.19967E+01 
c  Velocity[X]                                      0.13829E-03 
c  Velocity[Y]                                      0.12934E-03 
c  Velocity[Z]                                      0.42743E-02 
c  Pressure     0.36859E-04     131   0.93827E-02   0.26001E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52870E-08   0.16665E-08 0.10072E+00 
c  r22          0.10851E-01      13   0.50807E-08   0.18911E-08 0.10285E+00 
c  r33          0.21858E-01      15   0.53970E-08   0.12958E-07 0.12945E+00 
c  r12          0.93851E-03      19   0.60608E-08   0.31287E-09 0.61534E+00 
c  r13          0.46672E-02      19   0.65418E-08   0.15440E-08 0.20253E+00 
c  r23          0.39972E-02      19   0.58108E-08   0.13450E-08 0.20457E+00 
c  epsilon      0.10970E+02      11   0.33524E-08   0.10510E-01 0.17307E+00 
c  TempC        0.25716E+06      16   0.15186E-04   0.84462E-02 0.43334E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61352       0.0052549       0.0015071
v  Velocity[Y]            -0.57291         0.54415       0.0030798      0.00087321
v  Velocity[Z]              1.5651          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4374          4.3406          4.3632
v  Pressure                -36.435          360.01          87.644          169.84
v  r11                   0.0010591        0.081917        0.013071        0.018285
v  r22                   0.0011108        0.082617        0.013351        0.018645
v  r33                   0.0016344         0.17433        0.027245        0.037204
v  r12                   -0.010665        0.013565     -0.00023378     -0.00030928
v  r13                   -0.045557        0.052786      9.2975e-05       0.0010137
v  r23                   -0.046705        0.051222      3.0243e-05      0.00057447
v  epsilon                0.068772          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099178      0.00092463       0.0017425
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017865          5.2773         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71349         0.85283


 TIME FOR THE TIME STEP            10304:        0.11226E+03

===============================================================


 INSTANT    0.103050000E-01   TIME STEP NUMBER           10305
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.169629539E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.270133511E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153216096E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.343628390E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.307097889E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81102E-03   0.45514E-02 0.19998E+01 
c  Velocity[X]                                      0.13932E-03 
c  Velocity[Y]                                      0.12891E-03 
c  Velocity[Z]                                      0.42832E-02 
c  Pressure     0.36552E-04     133   0.93020E-02   0.25783E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53965E-08   0.16921E-08 0.10128E+00 
c  r22          0.10851E-01      13   0.49765E-08   0.19034E-08 0.10358E+00 
c  r33          0.21858E-01      15   0.58289E-08   0.12999E-07 0.13015E+00 
c  r12          0.93851E-03      19   0.55541E-08   0.30700E-09 0.61522E+00 
c  r13          0.46672E-02      19   0.64839E-08   0.15093E-08 0.20142E+00 
c  r23          0.39972E-02      19   0.54622E-08   0.13346E-08 0.20396E+00 
c  epsilon      0.10970E+02      11   0.33671E-08   0.99386E-02 0.16551E+00 
c  TempC        0.25716E+06      16   0.15118E-04   0.84441E-02 0.43357E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367          0.6135        0.005255       0.0015071
v  Velocity[Y]            -0.57305         0.54428       0.0030799      0.00087327
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.398          360.08          87.683           169.9
v  r11                   0.0010591        0.081915        0.013071        0.018285
v  r22                   0.0011108        0.082618        0.013351        0.018645
v  r33                   0.0016344         0.17431        0.027245        0.037204
v  r12                   -0.010664        0.013561     -0.00023378     -0.00030928
v  r13                   -0.045557        0.052787      9.2976e-05       0.0010137
v  r23                   -0.046705        0.051208      3.0244e-05      0.00057447
v  epsilon                0.068773          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099178      0.00092463       0.0017425
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017865          5.2776         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776          0.7135         0.85284


 TIME FOR THE TIME STEP            10305:        0.12939E+03

===============================================================


 INSTANT    0.103060000E-01   TIME STEP NUMBER           10306
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.412119538E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.206638841E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151901780E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935014E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.121474458E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.192888107E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81318E-03   0.45259E-02 0.19914E+01 
c  Velocity[X]                                      0.13831E-03 
c  Velocity[Y]                                      0.12953E-03 
c  Velocity[Z]                                      0.42581E-02 
c  Pressure     0.36311E-04     133   0.92466E-02   0.25612E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51221E-08   0.16839E-08 0.10099E+00 
c  r22          0.10851E-01      13   0.48842E-08   0.18499E-08 0.10207E+00 
c  r33          0.21858E-01      15   0.59357E-08   0.12794E-07 0.12862E+00 
c  r12          0.93851E-03      18   0.69937E-08   0.29531E-09 0.60645E+00 
c  r13          0.46672E-02      19   0.66069E-08   0.14979E-08 0.20012E+00 
c  r23          0.39972E-02      19   0.55883E-08   0.12984E-08 0.20126E+00 
c  epsilon      0.10970E+02      11   0.34121E-08   0.98603E-02 0.16613E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84105E-02 0.43286E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63372         0.61354       0.0052549       0.0015071
v  Velocity[Y]            -0.57298         0.54441       0.0030799      0.00087322
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                 -36.45          360.05          87.677          169.88
v  r11                   0.0010591         0.08191        0.013071        0.018285
v  r22                   0.0011108        0.082621        0.013351        0.018645
v  r33                   0.0016344         0.17429        0.027245        0.037204
v  r12                   -0.010662        0.013559     -0.00023378     -0.00030929
v  r13                   -0.045559         0.05279      9.2977e-05       0.0010137
v  r23                   -0.046706        0.051202      3.0244e-05      0.00057447
v  epsilon                0.068774          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099179      0.00092463       0.0017425
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017865          5.2777         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71349         0.85283


 TIME FOR THE TIME STEP            10306:        0.12575E+03

===============================================================


 INSTANT    0.103070000E-01   TIME STEP NUMBER           10307
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.393333208E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.146103161E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.431435459E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.109564121E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.731838873E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81218E-03   0.45365E-02 0.19936E+01 
c  Velocity[X]                                      0.13870E-03 
c  Velocity[Y]                                      0.12916E-03 
c  Velocity[Z]                                      0.42687E-02 
c  Pressure     0.36033E-04     131   0.91732E-02   0.25416E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52787E-08   0.17037E-08 0.10165E+00 
c  r22          0.10851E-01      13   0.48859E-08   0.18922E-08 0.10322E+00 
c  r33          0.21858E-01      15   0.58482E-08   0.12964E-07 0.12967E+00 
c  r12          0.93851E-03      18   0.72051E-08   0.31029E-09 0.61305E+00 
c  r13          0.46672E-02      19   0.68703E-08   0.15144E-08 0.20126E+00 
c  r23          0.39972E-02      19   0.51554E-08   0.13378E-08 0.20399E+00 
c  epsilon      0.10970E+02      11   0.32576E-08   0.10077E-01 0.16791E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.83843E-02 0.43257E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61351        0.005255       0.0015071
v  Velocity[Y]            -0.57301         0.54421       0.0030799      0.00087327
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.389          360.02          87.677          169.87
v  r11                   0.0010591        0.081907        0.013071        0.018285
v  r22                   0.0011108        0.082621        0.013351        0.018645
v  r33                   0.0016344          0.1743        0.027245        0.037204
v  r12                   -0.010661        0.013554     -0.00023378     -0.00030929
v  r13                   -0.045557        0.052788      9.2978e-05       0.0010137
v  r23                   -0.046707        0.051218      3.0244e-05      0.00057447
v  epsilon                0.068775          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099179      0.00092463       0.0017425
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017865          5.2774         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71349         0.85283


 TIME FOR THE TIME STEP            10307:        0.10958E+03

===============================================================


 INSTANT    0.103080000E-01   TIME STEP NUMBER           10308
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.264728009E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.222326710E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.787713077E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.356742597E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.508126331E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81212E-03   0.45255E-02 0.19923E+01 
c  Velocity[X]                                      0.13914E-03 
c  Velocity[Y]                                      0.12857E-03 
c  Velocity[Z]                                      0.42578E-02 
c  Pressure     0.37017E-04     133   0.94191E-02   0.26111E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52873E-08   0.16907E-08 0.10174E+00 
c  r22          0.10851E-01      13   0.47170E-08   0.18681E-08 0.10289E+00 
c  r33          0.21858E-01      15   0.52605E-08   0.12814E-07 0.12945E+00 
c  r12          0.93852E-03      18   0.71589E-08   0.29895E-09 0.60892E+00 
c  r13          0.46672E-02      19   0.68296E-08   0.15077E-08 0.20111E+00 
c  r23          0.39972E-02      19   0.60844E-08   0.13057E-08 0.20187E+00 
c  epsilon      0.10970E+02      11   0.32341E-08   0.99067E-02 0.16555E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.84640E-02 0.43434E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61354        0.005255       0.0015072
v  Velocity[Y]             -0.5729          0.5443       0.0030799      0.00087322
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.456          360.01          87.644          169.85
v  r11                   0.0010591        0.081898        0.013071        0.018285
v  r22                   0.0011108        0.082621        0.013351        0.018645
v  r33                   0.0016344         0.17432        0.027245        0.037204
v  r12                   -0.010662        0.013555     -0.00023378     -0.00030929
v  r13                   -0.045556         0.05279      9.2979e-05       0.0010137
v  r23                   -0.046707        0.051212      3.0245e-05      0.00057447
v  epsilon                0.068777          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099177      0.00092463       0.0017425
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017864           5.278         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878          0.7135         0.85283


 TIME FOR THE TIME STEP            10308:        0.14925E+03

===============================================================


 INSTANT    0.103090000E-01   TIME STEP NUMBER           10309
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.321581660E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.318907234E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.245782480E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.870637806E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.193033628E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81261E-03   0.45166E-02 0.19895E+01 
c  Velocity[X]                                      0.13832E-03 
c  Velocity[Y]                                      0.12921E-03 
c  Velocity[Z]                                      0.42491E-02 
c  Pressure     0.36034E-04     133   0.91744E-02   0.25418E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52949E-08   0.16753E-08 0.10101E+00 
c  r22          0.10851E-01      13   0.51892E-08   0.18437E-08 0.10262E+00 
c  r33          0.21858E-01      15   0.56791E-08   0.12590E-07 0.12836E+00 
c  r12          0.93852E-03      18   0.70933E-08   0.30301E-09 0.60962E+00 
c  r13          0.46672E-02      20   0.60120E-08   0.14794E-08 0.20032E+00 
c  r23          0.39972E-02      19   0.60554E-08   0.12916E-08 0.20056E+00 
c  epsilon      0.10970E+02      11   0.32458E-08   0.96234E-02 0.16390E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.84402E-02 0.43316E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63377         0.61352        0.005255       0.0015072
v  Velocity[Y]            -0.57307         0.54404       0.0030799      0.00087321
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.413          360.15          87.725          169.96
v  r11                   0.0010591        0.081899        0.013071        0.018285
v  r22                   0.0011108        0.082619        0.013351        0.018645
v  r33                   0.0016344         0.17435        0.027245        0.037204
v  r12                   -0.010659        0.013562     -0.00023378     -0.00030929
v  r13                    -0.04556        0.052794      9.2979e-05       0.0010137
v  r23                   -0.046708        0.051201      3.0245e-05      0.00057447
v  epsilon                0.068778          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099177      0.00092464       0.0017425
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017864          5.2772         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71349         0.85283


 TIME FOR THE TIME STEP            10309:        0.33854E+03

===============================================================


 INSTANT    0.103100000E-01   TIME STEP NUMBER           10310
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123608226E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191695236E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.272047626E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.187671397E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.514870627E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81213E-03   0.45601E-02 0.19988E+01 
c  Velocity[X]                                      0.13927E-03 
c  Velocity[Y]                                      0.12858E-03 
c  Velocity[Z]                                      0.42922E-02 
c  Pressure     0.36652E-04     133   0.93329E-02   0.25853E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55624E-08   0.16694E-08 0.10067E+00 
c  r22          0.10851E-01      13   0.50439E-08   0.18781E-08 0.10290E+00 
c  r33          0.21858E-01      15   0.53950E-08   0.12867E-07 0.12910E+00 
c  r12          0.93852E-03      19   0.56639E-08   0.29732E-09 0.60692E+00 
c  r13          0.46672E-02      19   0.74566E-08   0.15050E-08 0.20113E+00 
c  r23          0.39972E-02      19   0.70992E-08   0.12936E-08 0.20097E+00 
c  epsilon      0.10970E+02      11   0.31468E-08   0.10324E-01 0.16751E+00 
c  TempC        0.25716E+06      16   0.15122E-04   0.84127E-02 0.43235E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61348        0.005255       0.0015072
v  Velocity[Y]            -0.57295         0.54412       0.0030798      0.00087319
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.402             360          87.653          169.84
v  r11                   0.0010591        0.081893        0.013071        0.018285
v  r22                   0.0011108        0.082622        0.013351        0.018645
v  r33                   0.0016344         0.17434        0.027245        0.037204
v  r12                   -0.010657         0.01357     -0.00023378     -0.00030929
v  r13                   -0.045556        0.052797      9.2979e-05       0.0010137
v  r23                   -0.046709        0.051216      3.0245e-05      0.00057447
v  epsilon                0.068779          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099177      0.00092464       0.0017425
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2766         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766          0.7135         0.85283


 TIME FOR THE TIME STEP            10310:        0.22211E+03

===============================================================


 INSTANT    0.103110000E-01   TIME STEP NUMBER           10311
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.338798799E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.605859623E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.244107898E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.281781866E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184741630E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81205E-03   0.45344E-02 0.19959E+01 
c  Velocity[X]                                      0.13950E-03 
c  Velocity[Y]                                      0.12966E-03 
c  Velocity[Z]                                      0.42653E-02 
c  Pressure     0.36521E-04     132   0.93024E-02   0.25760E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.50037E-08   0.16697E-08 0.10075E+00 
c  r22          0.10851E-01      13   0.48022E-08   0.18353E-08 0.10195E+00 
c  r33          0.21858E-01      14   0.69438E-08   0.12682E-07 0.12860E+00 
c  r12          0.93852E-03      18   0.67546E-08   0.30182E-09 0.61006E+00 
c  r13          0.46672E-02      19   0.63523E-08   0.14912E-08 0.20016E+00 
c  r23          0.39973E-02      19   0.69828E-08   0.13070E-08 0.20215E+00 
c  epsilon      0.10970E+02      11   0.32664E-08   0.10209E-01 0.17108E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.84315E-02 0.43327E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61353       0.0052551       0.0015072
v  Velocity[Y]            -0.57307         0.54431       0.0030799      0.00087325
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.461          360.06          87.671          169.88
v  r11                   0.0010591        0.081885        0.013071        0.018285
v  r22                   0.0011108        0.082625        0.013351        0.018645
v  r33                   0.0016344          0.1743        0.027245        0.037204
v  r12                   -0.010657        0.013574     -0.00023378     -0.00030929
v  r13                   -0.045556        0.052796       9.298e-05       0.0010137
v  r23                    -0.04671        0.051201      3.0246e-05      0.00057447
v  epsilon                0.068781          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099178      0.00092464       0.0017425
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017864          5.2758         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8758         0.71349         0.85283


 TIME FOR THE TIME STEP            10311:        0.26452E+03

===============================================================


 INSTANT    0.103120000E-01   TIME STEP NUMBER           10312
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.939584701E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158471660E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.317132473E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.298091376E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169352236E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81253E-03   0.45132E-02 0.19901E+01 
c  Velocity[X]                                      0.13706E-03 
c  Velocity[Y]                                      0.12868E-03 
c  Velocity[Z]                                      0.42475E-02 
c  Pressure     0.36388E-04     132   0.92672E-02   0.25667E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54045E-08   0.16869E-08 0.10119E+00 
c  r22          0.10851E-01      13   0.47530E-08   0.18649E-08 0.10251E+00 
c  r33          0.21858E-01      15   0.56693E-08   0.12773E-07 0.12873E+00 
c  r12          0.93852E-03      18   0.62004E-08   0.30149E-09 0.61104E+00 
c  r13          0.46672E-02      19   0.71938E-08   0.15067E-08 0.20004E+00 
c  r23          0.39973E-02      19   0.59332E-08   0.12911E-08 0.20083E+00 
c  epsilon      0.10970E+02      11   0.32386E-08   0.10162E-01 0.16725E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.83749E-02 0.43215E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61351       0.0052551       0.0015072
v  Velocity[Y]            -0.57301         0.54443       0.0030799      0.00087323
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.456          360.01           87.64          169.84
v  r11                   0.0010591        0.081872        0.013071        0.018285
v  r22                   0.0011108        0.082626        0.013351        0.018645
v  r33                   0.0016344          0.1743        0.027245        0.037204
v  r12                   -0.010658        0.013579     -0.00023378     -0.00030929
v  r13                   -0.045558        0.052793       9.298e-05       0.0010137
v  r23                    -0.04671        0.051198      3.0246e-05      0.00057447
v  epsilon                0.068782          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099176      0.00092464       0.0017425
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2751         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8751          0.7135         0.85283


 TIME FOR THE TIME STEP            10312:        0.23133E+03

===============================================================


 INSTANT    0.103130000E-01   TIME STEP NUMBER           10313
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227101907E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33839E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.476316405E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33839E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.212091562E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33839E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.550494252E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33839E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.271376451E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33839E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81210E-03   0.45384E-02 0.19935E+01 
c  Velocity[X]                                      0.13940E-03 
c  Velocity[Y]                                      0.12938E-03 
c  Velocity[Z]                                      0.42696E-02 
c  Pressure     0.36125E-04     133   0.91881E-02   0.25482E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58191E-08   0.16621E-08 0.10038E+00 
c  r22          0.10851E-01      13   0.50368E-08   0.18396E-08 0.10196E+00 
c  r33          0.21858E-01      15   0.54298E-08   0.12654E-07 0.12810E+00 
c  r12          0.93852E-03      18   0.64258E-08   0.30015E-09 0.61031E+00 
c  r13          0.46672E-02      20   0.60933E-08   0.14967E-08 0.19978E+00 
c  r23          0.39973E-02      19   0.55738E-08   0.13099E-08 0.20096E+00 
c  epsilon      0.10970E+02      11   0.33163E-08   0.98772E-02 0.16417E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.84388E-02 0.43325E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61348       0.0052552       0.0015072
v  Velocity[Y]             -0.5731         0.54428       0.0030799      0.00087324
v  Velocity[Z]              1.5659          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4374          4.3406          4.3632
v  Pressure                -36.425          359.97          87.611          169.81
v  r11                   0.0010591        0.081863        0.013071        0.018285
v  r22                   0.0011108        0.082627        0.013351        0.018645
v  r33                   0.0016344         0.17433        0.027245        0.037204
v  r12                   -0.010659        0.013583     -0.00023378     -0.00030929
v  r13                   -0.045557        0.052795      9.2981e-05       0.0010137
v  r23                    -0.04671        0.051222      3.0247e-05      0.00057447
v  epsilon                0.068783          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099175      0.00092464       0.0017425
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2755         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8755         0.71349         0.85282


 TIME FOR THE TIME STEP            10313:        0.29142E+03

===============================================================


 INSTANT    0.103140000E-01   TIME STEP NUMBER           10314
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.392197820E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.644784766E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.414614472E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.483761221E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.375321627E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33839E+00
   Friction velocity        uk    :  0.11551E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81212E-03   0.45475E-02 0.19965E+01 
c  Velocity[X]                                      0.13839E-03 
c  Velocity[Y]                                      0.12949E-03 
c  Velocity[Z]                                      0.42796E-02 
c  Pressure     0.36379E-04     133   0.92598E-02   0.25661E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58651E-08   0.16463E-08 0.10020E+00 
c  r22          0.10851E-01      13   0.53304E-08   0.18562E-08 0.10215E+00 
c  r33          0.21858E-01      15   0.63144E-08   0.12673E-07 0.12841E+00 
c  r12          0.93852E-03      18   0.63761E-08   0.30099E-09 0.61499E+00 
c  r13          0.46672E-02      20   0.61714E-08   0.15087E-08 0.20057E+00 
c  r23          0.39973E-02      19   0.61712E-08   0.12846E-08 0.20028E+00 
c  epsilon      0.10970E+02      11   0.33738E-08   0.98209E-02 0.16531E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84768E-02 0.43394E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63368          0.6135       0.0052551       0.0015072
v  Velocity[Y]            -0.57301          0.5444       0.0030799      0.00087318
v  Velocity[Z]              1.5658          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4374          4.3406          4.3632
v  Pressure                -36.484          360.02          87.661          169.86
v  r11                   0.0010591        0.081863        0.013071        0.018285
v  r22                   0.0011108        0.082629        0.013351        0.018645
v  r33                   0.0016344          0.1743        0.027245        0.037204
v  r12                   -0.010658        0.013585     -0.00023378     -0.00030929
v  r13                   -0.045556        0.052798      9.2982e-05       0.0010137
v  r23                    -0.04671        0.051216      3.0248e-05      0.00057447
v  epsilon                0.068784          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099177      0.00092464       0.0017425
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017863           5.276         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.876         0.71349         0.85283


 TIME FOR THE TIME STEP            10314:        0.82659E+02

===============================================================


 INSTANT    0.103150000E-01   TIME STEP NUMBER           10315
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.121158667E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.127576004E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.325283611E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.146420719E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.508358554E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      40   0.81169E-03   0.45116E-02 0.19890E+01 
c  Velocity[X]                                      0.13825E-03 
c  Velocity[Y]                                      0.12812E-03 
c  Velocity[Z]                                      0.42452E-02 
c  Pressure     0.36474E-04     136   0.92852E-02   0.25727E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55250E-08   0.16468E-08 0.99959E-01 
c  r22          0.10851E-01      13   0.54411E-08   0.18348E-08 0.10190E+00 
c  r33          0.21858E-01      15   0.68507E-08   0.12593E-07 0.12777E+00 
c  r12          0.93852E-03      18   0.61528E-08   0.30073E-09 0.60821E+00 
c  r13          0.46672E-02      19   0.73372E-08   0.15036E-08 0.19967E+00 
c  r23          0.39973E-02      20   0.55510E-08   0.12951E-08 0.19957E+00 
c  epsilon      0.10970E+02      11   0.33976E-08   0.96672E-02 0.16429E+00 
c  TempC        0.25716E+06      16   0.15100E-04   0.84021E-02 0.43239E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376          0.6135       0.0052551       0.0015072
v  Velocity[Y]            -0.57316          0.5441       0.0030799       0.0008732
v  Velocity[Z]              1.5658          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4374          4.3406          4.3632
v  Pressure                -36.427          360.05           87.65          169.86
v  r11                   0.0010591        0.081862        0.013071        0.018285
v  r22                   0.0011108        0.082626        0.013351        0.018645
v  r33                   0.0016344         0.17428        0.027245        0.037204
v  r12                   -0.010656        0.013583     -0.00023378     -0.00030929
v  r13                   -0.045558        0.052799      9.2984e-05       0.0010137
v  r23                   -0.046711        0.051207       3.025e-05      0.00057448
v  epsilon                0.068786          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099177      0.00092464       0.0017425
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2766         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766          0.7135         0.85283


 TIME FOR THE TIME STEP            10315:        0.87077E+02

===============================================================


 INSTANT    0.103160000E-01   TIME STEP NUMBER           10316
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.352273148E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183546406E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934909E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.331417465E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.141784345E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934913E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150516897E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81305E-03   0.45420E-02 0.19975E+01 
c  Velocity[X]                                      0.13920E-03 
c  Velocity[Y]                                      0.12928E-03 
c  Velocity[Z]                                      0.42735E-02 
c  Pressure     0.36285E-04     132   0.92359E-02   0.25596E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55767E-08   0.16742E-08 0.10013E+00 
c  r22          0.10851E-01      13   0.54996E-08   0.18917E-08 0.10249E+00 
c  r33          0.21858E-01      15   0.68721E-08   0.13015E-07 0.12881E+00 
c  r12          0.93852E-03      18   0.61184E-08   0.30312E-09 0.60467E+00 
c  r13          0.46672E-02      20   0.64578E-08   0.15413E-08 0.20137E+00 
c  r23          0.39973E-02      20   0.55964E-08   0.13087E-08 0.20053E+00 
c  epsilon      0.10970E+02      11   0.33312E-08   0.10472E-01 0.16864E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.83990E-02 0.43338E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338         0.61345       0.0052552       0.0015072
v  Velocity[Y]             -0.5731         0.54418       0.0030799      0.00087318
v  Velocity[Z]              1.5655          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4373          4.3406          4.3632
v  Pressure                -36.443          360.08          87.695           169.9
v  r11                   0.0010591        0.081875        0.013071        0.018285
v  r22                   0.0011108        0.082627        0.013351        0.018645
v  r33                   0.0016345         0.17429        0.027245        0.037204
v  r12                   -0.010658        0.013589     -0.00023378     -0.00030929
v  r13                   -0.045556        0.052801      9.2984e-05       0.0010137
v  r23                   -0.046711        0.051219       3.025e-05      0.00057448
v  epsilon                0.068787          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9911e-05       0.0099176      0.00092464       0.0017425
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017862          5.2775         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71349         0.85283


 TIME FOR THE TIME STEP            10316:        0.88391E+02

===============================================================


 INSTANT    0.103170000E-01   TIME STEP NUMBER           10317
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.230109145E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.259227121E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.248301011E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935018E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.126955940E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.466359864E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81123E-03   0.44943E-02 0.19864E+01 
c  Velocity[X]                                      0.13823E-03 
c  Velocity[Y]                                      0.12883E-03 
c  Velocity[Z]                                      0.42273E-02 
c  Pressure     0.36274E-04     131   0.92273E-02   0.25587E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57722E-08   0.16696E-08 0.10004E+00 
c  r22          0.10851E-01      13   0.55842E-08   0.18534E-08 0.10175E+00 
c  r33          0.21858E-01      15   0.60707E-08   0.12747E-07 0.12771E+00 
c  r12          0.93852E-03      18   0.61663E-08   0.29779E-09 0.60344E+00 
c  r13          0.46672E-02      19   0.69860E-08   0.15146E-08 0.19980E+00 
c  r23          0.39973E-02      19   0.64804E-08   0.13099E-08 0.20006E+00 
c  epsilon      0.10970E+02      11   0.33899E-08   0.10012E-01 0.16590E+00 
c  TempC        0.25716E+06      16   0.15142E-04   0.84355E-02 0.43347E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379         0.61351       0.0052552       0.0015073
v  Velocity[Y]            -0.57318         0.54434       0.0030799      0.00087317
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.377          360.04          87.656          169.86
v  r11                   0.0010591         0.08189        0.013071        0.018285
v  r22                   0.0011108        0.082629        0.013351        0.018645
v  r33                   0.0016345         0.17431        0.027245        0.037204
v  r12                   -0.010663        0.013596     -0.00023378     -0.00030929
v  r13                   -0.045556        0.052798      9.2986e-05       0.0010137
v  r23                   -0.046711        0.051207      3.0251e-05      0.00057448
v  epsilon                0.068788           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.991e-05       0.0099176      0.00092465       0.0017425
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017862          5.2778         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778          0.7135         0.85283


 TIME FOR THE TIME STEP            10317:        0.93317E+02

===============================================================


 INSTANT    0.103180000E-01   TIME STEP NUMBER           10318
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.318345537E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188665980E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.381645637E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.302997515E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.112172055E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      46   0.81198E-03   0.45169E-02 0.19918E+01 
c  Velocity[X]                                      0.13817E-03 
c  Velocity[Y]                                      0.12912E-03 
c  Velocity[Z]                                      0.42496E-02 
c  Pressure     0.37005E-04     133   0.94232E-02   0.26103E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58241E-08   0.16794E-08 0.10076E+00 
c  r22          0.10851E-01      13   0.55242E-08   0.18195E-08 0.10156E+00 
c  r33          0.21858E-01      15   0.60642E-08   0.12695E-07 0.12852E+00 
c  r12          0.93852E-03      18   0.64400E-08   0.30131E-09 0.60712E+00 
c  r13          0.46672E-02      19   0.74547E-08   0.14898E-08 0.19933E+00 
c  r23          0.39973E-02      19   0.68979E-08   0.13214E-08 0.20181E+00 
c  epsilon      0.10970E+02      11   0.33723E-08   0.99380E-02 0.16956E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.83589E-02 0.43126E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61349       0.0052551       0.0015072
v  Velocity[Y]            -0.57331          0.5444       0.0030798      0.00087318
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.449             360          87.636          169.83
v  r11                   0.0010591          0.0819        0.013071        0.018285
v  r22                   0.0011108        0.082631        0.013351        0.018645
v  r33                   0.0016345         0.17435        0.027245        0.037204
v  r12                   -0.010663        0.013602     -0.00023378     -0.00030929
v  r13                   -0.045558        0.052799      9.2986e-05       0.0010137
v  r23                   -0.046711        0.051212      3.0251e-05      0.00057448
v  epsilon                0.068789           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.991e-05       0.0099176      0.00092465       0.0017425
v  CourantNb               0.44218             0.6         0.59908         0.59839
v  FourierNb             0.0017862          5.2778         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71349         0.85283


 TIME FOR THE TIME STEP            10318:        0.98854E+02

===============================================================


 INSTANT    0.103190000E-01   TIME STEP NUMBER           10319
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.862583363E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.386627837E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934905E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191115878E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.433879159E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.423108469E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81261E-03   0.45879E-02 0.20042E+01 
c  Velocity[X]                                      0.13856E-03 
c  Velocity[Y]                                      0.12936E-03 
c  Velocity[Z]                                      0.43200E-02 
c  Pressure     0.36371E-04     133   0.92619E-02   0.25656E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.63343E-08   0.16341E-08 0.99634E-01 
c  r22          0.10851E-01      13   0.55820E-08   0.18383E-08 0.10200E+00 
c  r33          0.21858E-01      15   0.63645E-08   0.12596E-07 0.12804E+00 
c  r12          0.93852E-03      18   0.69421E-08   0.29692E-09 0.60435E+00 
c  r13          0.46672E-02      20   0.58501E-08   0.14893E-08 0.20012E+00 
c  r23          0.39973E-02      20   0.56004E-08   0.12854E-08 0.19906E+00 
c  epsilon      0.10970E+02      11   0.34294E-08   0.97928E-02 0.16409E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84434E-02 0.43286E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61346       0.0052552       0.0015072
v  Velocity[Y]            -0.57336         0.54417       0.0030798      0.00087314
v  Velocity[Z]              1.5657          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4374          4.3406          4.3632
v  Pressure                -36.391          360.06          87.684          169.89
v  r11                   0.0010591        0.081902        0.013071        0.018285
v  r22                   0.0011108        0.082632        0.013351        0.018645
v  r33                   0.0016345         0.17433        0.027245        0.037204
v  r12                    -0.01066        0.013612     -0.00023378     -0.00030929
v  r13                   -0.045556        0.052798      9.2987e-05       0.0010137
v  r23                   -0.046709        0.051207      3.0252e-05      0.00057448
v  epsilon                0.068791           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9911e-05       0.0099178      0.00092465       0.0017425
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017862          5.2773         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773          0.7135         0.85283


 TIME FOR THE TIME STEP            10319:        0.10069E+03

===============================================================


 INSTANT    0.103200000E-01   TIME STEP NUMBER           10320
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.235988915E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.384396276E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.895560948E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935017E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.367762267E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.141407011E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81187E-03   0.45309E-02 0.19910E+01 
c  Velocity[X]                                      0.13860E-03 
c  Velocity[Y]                                      0.12844E-03 
c  Velocity[Z]                                      0.42638E-02 
c  Pressure     0.36513E-04     131   0.92927E-02   0.25755E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60710E-08   0.16476E-08 0.10009E+00 
c  r22          0.10851E-01      13   0.53290E-08   0.18394E-08 0.10197E+00 
c  r33          0.21858E-01      15   0.54517E-08   0.12589E-07 0.12811E+00 
c  r12          0.93852E-03      18   0.65247E-08   0.29979E-09 0.60593E+00 
c  r13          0.46672E-02      19   0.72098E-08   0.15012E-08 0.20085E+00 
c  r23          0.39973E-02      19   0.65738E-08   0.12814E-08 0.19976E+00 
c  epsilon      0.10970E+02      11   0.33722E-08   0.98141E-02 0.16459E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.84682E-02 0.43447E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375          0.6135       0.0052552       0.0015072
v  Velocity[Y]            -0.57348          0.5443       0.0030798      0.00087313
v  Velocity[Z]              1.5656          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4374          4.3406          4.3632
v  Pressure                -36.448          360.04          87.668          169.87
v  r11                   0.0010591        0.081908        0.013071        0.018285
v  r22                   0.0011108        0.082633        0.013351        0.018645
v  r33                   0.0016345          0.1743        0.027245        0.037204
v  r12                    -0.01066        0.013611     -0.00023378     -0.00030929
v  r13                   -0.045555        0.052797      9.2989e-05       0.0010137
v  r23                   -0.046709        0.051243      3.0252e-05      0.00057448
v  epsilon                0.068792          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9912e-05       0.0099178      0.00092465       0.0017425
v  CourantNb               0.44217             0.6         0.59908         0.59839
v  FourierNb             0.0017861          5.2767         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767         0.71349         0.85283


 TIME FOR THE TIME STEP            10320:        0.91379E+02

===============================================================


 INSTANT    0.103210000E-01   TIME STEP NUMBER           10321
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.418545881E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.279704763E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.377636471E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.250913716E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.220686422E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81264E-03   0.45267E-02 0.19928E+01 
c  Velocity[X]                                      0.13845E-03 
c  Velocity[Y]                                      0.12941E-03 
c  Velocity[Z]                                      0.42588E-02 
c  Pressure     0.36392E-04     132   0.92699E-02   0.25671E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56728E-08   0.16193E-08 0.99674E-01 
c  r22          0.10851E-01      13   0.51845E-08   0.17875E-08 0.10103E+00 
c  r33          0.21858E-01      15   0.57417E-08   0.12216E-07 0.12696E+00 
c  r12          0.93852E-03      18   0.59821E-08   0.29154E-09 0.60076E+00 
c  r13          0.46672E-02      19   0.69787E-08   0.14454E-08 0.19756E+00 
c  r23          0.39973E-02      19   0.71124E-08   0.12588E-08 0.19900E+00 
c  epsilon      0.10970E+02      11   0.33928E-08   0.92488E-02 0.16061E+00 
c  TempC        0.25716E+06      16   0.15121E-04   0.83679E-02 0.43192E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61348       0.0052552       0.0015072
v  Velocity[Y]             -0.5736         0.54446       0.0030798      0.00087311
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                  -36.4          360.05          87.661          169.87
v  r11                   0.0010591        0.081913        0.013071        0.018285
v  r22                   0.0011108        0.082634        0.013351        0.018645
v  r33                   0.0016345         0.17431        0.027245        0.037204
v  r12                   -0.010662        0.013614     -0.00023378     -0.00030929
v  r13                   -0.045559        0.052797      9.2989e-05       0.0010137
v  r23                   -0.046709        0.051244      3.0253e-05      0.00057448
v  epsilon                0.068793          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099179      0.00092465       0.0017425
v  CourantNb               0.44218             0.6         0.59908         0.59839
v  FourierNb             0.0017861          5.2775         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775          0.7135         0.85283


 TIME FOR THE TIME STEP            10321:        0.10142E+03

===============================================================


 INSTANT    0.103220000E-01   TIME STEP NUMBER           10322
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.146700412E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.355484994E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.120313215E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.113412841E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.890124017E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81154E-03   0.45496E-02 0.20001E+01 
c  Velocity[X]                                      0.13809E-03 
c  Velocity[Y]                                      0.12976E-03 
c  Velocity[Z]                                      0.42818E-02 
c  Pressure     0.36609E-04     134   0.93146E-02   0.25824E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58335E-08   0.16289E-08 0.99899E-01 
c  r22          0.10851E-01      13   0.51801E-08   0.18312E-08 0.10197E+00 
c  r33          0.21858E-01      15   0.59247E-08   0.12491E-07 0.12807E+00 
c  r12          0.93852E-03      18   0.60816E-08   0.30562E-09 0.61089E+00 
c  r13          0.46672E-02      19   0.59743E-08   0.14950E-08 0.20025E+00 
c  r23          0.39973E-02      19   0.61583E-08   0.12939E-08 0.20136E+00 
c  epsilon      0.10970E+02      11   0.33452E-08   0.95436E-02 0.16256E+00 
c  TempC        0.25716E+06      16   0.15164E-04   0.84251E-02 0.43322E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61354       0.0052552       0.0015072
v  Velocity[Y]            -0.57356         0.54415       0.0030798      0.00087314
v  Velocity[Z]              1.5656          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4374          4.3406          4.3632
v  Pressure                -36.438          359.96          87.636          169.81
v  r11                   0.0010591        0.081917        0.013071        0.018285
v  r22                   0.0011108        0.082635        0.013352        0.018645
v  r33                   0.0016345         0.17433        0.027246        0.037204
v  r12                   -0.010663        0.013616     -0.00023378     -0.00030929
v  r13                   -0.045556        0.052799       9.299e-05       0.0010137
v  r23                   -0.046708         0.05123      3.0254e-05      0.00057448
v  epsilon                0.068795          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099177      0.00092465       0.0017425
v  CourantNb               0.44219             0.6         0.59908         0.59839
v  FourierNb             0.0017861          5.2777         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71349         0.85283


 TIME FOR THE TIME STEP            10322:        0.10012E+03

===============================================================


 INSTANT    0.103230000E-01   TIME STEP NUMBER           10323
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.503264337E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.744797475E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.727243397E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.248081771E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.964426510E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81193E-03   0.45236E-02 0.19899E+01 
c  Velocity[X]                                      0.13888E-03 
c  Velocity[Y]                                      0.12853E-03 
c  Velocity[Z]                                      0.42562E-02 
c  Pressure     0.36028E-04     131   0.91678E-02   0.25412E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57472E-08   0.16435E-08 0.99715E-01 
c  r22          0.10851E-01      13   0.53667E-08   0.18380E-08 0.10187E+00 
c  r33          0.21858E-01      15   0.53946E-08   0.12606E-07 0.12797E+00 
c  r12          0.93852E-03      18   0.58896E-08   0.30390E-09 0.60801E+00 
c  r13          0.46672E-02      19   0.65107E-08   0.15093E-08 0.20101E+00 
c  r23          0.39973E-02      19   0.53796E-08   0.12893E-08 0.19959E+00 
c  epsilon      0.10970E+02      11   0.34490E-08   0.98334E-02 0.16440E+00 
c  TempC        0.25716E+06      16   0.15105E-04   0.84796E-02 0.43398E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61354       0.0052551       0.0015071
v  Velocity[Y]            -0.57372         0.54419       0.0030798      0.00087313
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.426          360.07          87.682          169.89
v  r11                   0.0010591        0.081919        0.013071        0.018285
v  r22                   0.0011108         0.08263        0.013352        0.018645
v  r33                   0.0016345         0.17431        0.027246        0.037204
v  r12                   -0.010669        0.013621     -0.00023378     -0.00030929
v  r13                   -0.045555        0.052797      9.2991e-05       0.0010137
v  r23                   -0.046707        0.051247      3.0256e-05      0.00057448
v  epsilon                0.068796          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099177      0.00092465       0.0017425
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017861          5.2777         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71349         0.85283


 TIME FOR THE TIME STEP            10323:        0.91526E+02

===============================================================


 INSTANT    0.103240000E-01   TIME STEP NUMBER           10324
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.278431634E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.307560013E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.696225265E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.629914425E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.371574973E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81244E-03   0.45345E-02 0.19934E+01 
c  Velocity[X]                                      0.13913E-03 
c  Velocity[Y]                                      0.12952E-03 
c  Velocity[Z]                                      0.42658E-02 
c  Pressure     0.36563E-04     132   0.93048E-02   0.25791E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58652E-08   0.16738E-08 0.10073E+00 
c  r22          0.10851E-01      13   0.50112E-08   0.18085E-08 0.10134E+00 
c  r33          0.21858E-01      15   0.70000E-08   0.12657E-07 0.12856E+00 
c  r12          0.93852E-03      18   0.51756E-08   0.29790E-09 0.60462E+00 
c  r13          0.46672E-02      20   0.60782E-08   0.14910E-08 0.19986E+00 
c  r23          0.39973E-02      19   0.61805E-08   0.13185E-08 0.20249E+00 
c  epsilon      0.10970E+02      11   0.34661E-08   0.10076E-01 0.17039E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.84032E-02 0.43276E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61349       0.0052551       0.0015072
v  Velocity[Y]            -0.57378          0.5443       0.0030799      0.00087314
v  Velocity[Z]              1.5656          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4373          4.3406          4.3632
v  Pressure                -36.442          360.06          87.669          169.88
v  r11                   0.0010591        0.081923        0.013071        0.018285
v  r22                   0.0011108         0.08263        0.013352        0.018645
v  r33                   0.0016345         0.17428        0.027246        0.037204
v  r12                   -0.010671        0.013622     -0.00023378     -0.00030929
v  r13                   -0.045558        0.052798      9.2992e-05       0.0010137
v  r23                   -0.046707        0.051244      3.0257e-05      0.00057448
v  epsilon                0.068797          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099176      0.00092465       0.0017426
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017861          5.2781         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781          0.7135         0.85283


 TIME FOR THE TIME STEP            10324:        0.86732E+02

===============================================================


 INSTANT    0.103250000E-01   TIME STEP NUMBER           10325
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.474889862E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.159162959E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.410128101E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.397792889E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.356552210E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81196E-03   0.45391E-02 0.19948E+01 
c  Velocity[X]                                      0.13814E-03 
c  Velocity[Y]                                      0.12869E-03 
c  Velocity[Z]                                      0.42723E-02 
c  Pressure     0.36234E-04     133   0.92230E-02   0.25559E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51288E-08   0.16407E-08 0.99923E-01 
c  r22          0.10851E-01      13   0.48605E-08   0.18751E-08 0.10257E+00 
c  r33          0.21858E-01      15   0.54299E-08   0.12729E-07 0.12866E+00 
c  r12          0.93852E-03      18   0.48966E-08   0.30234E-09 0.60836E+00 
c  r13          0.46672E-02      19   0.52892E-08   0.15144E-08 0.20088E+00 
c  r23          0.39973E-02      19   0.53327E-08   0.12835E-08 0.20045E+00 
c  epsilon      0.10970E+02      11   0.34582E-08   0.98954E-02 0.16495E+00 
c  TempC        0.25716E+06      16   0.15118E-04   0.83576E-02 0.43135E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61353       0.0052552       0.0015072
v  Velocity[Y]            -0.57377         0.54439       0.0030798       0.0008731
v  Velocity[Z]              1.5655          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4373          4.3406          4.3632
v  Pressure                -36.415          360.03          87.643          169.85
v  r11                   0.0010591        0.081927        0.013071        0.018285
v  r22                   0.0011108        0.082631        0.013352        0.018645
v  r33                   0.0016345         0.17429        0.027246        0.037204
v  r12                   -0.010672         0.01362     -0.00023378     -0.00030929
v  r13                   -0.045557        0.052797      9.2992e-05       0.0010137
v  r23                   -0.046706        0.051235      3.0258e-05      0.00057448
v  epsilon                0.068799          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05       0.0099177      0.00092466       0.0017426
v  CourantNb               0.44217             0.6         0.59908         0.59839
v  FourierNb             0.0017861          5.2777         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71349         0.85283


 TIME FOR THE TIME STEP            10325:        0.83375E+02

===============================================================


 INSTANT    0.103260000E-01   TIME STEP NUMBER           10326
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.506446587E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.256030026E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.673967610E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.647068647E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283362837E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81284E-03   0.45434E-02 0.19947E+01 
c  Velocity[X]                                      0.13891E-03 
c  Velocity[Y]                                      0.12950E-03 
c  Velocity[Z]                                      0.42750E-02 
c  Pressure     0.36492E-04     131   0.92893E-02   0.25741E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52728E-08   0.16690E-08 0.10116E+00 
c  r22          0.10851E-01      13   0.46081E-08   0.18301E-08 0.10231E+00 
c  r33          0.21858E-01      15   0.60271E-08   0.12630E-07 0.12922E+00 
c  r12          0.93852E-03      17   0.68080E-08   0.30370E-09 0.61168E+00 
c  r13          0.46672E-02      19   0.54073E-08   0.14937E-08 0.20057E+00 
c  r23          0.39973E-02      19   0.51572E-08   0.13087E-08 0.20325E+00 
c  epsilon      0.10970E+02      11   0.33163E-08   0.94567E-02 0.16340E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84619E-02 0.43401E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382          0.6135       0.0052552       0.0015072
v  Velocity[Y]             -0.5737         0.54421       0.0030798      0.00087312
v  Velocity[Z]              1.5656          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4373          4.3406          4.3632
v  Pressure                -36.467          360.04           87.67          169.87
v  r11                   0.0010591         0.08193        0.013071        0.018285
v  r22                   0.0011108        0.082633        0.013352        0.018645
v  r33                   0.0016345         0.17432        0.027246        0.037204
v  r12                   -0.010671        0.013621     -0.00023378     -0.00030929
v  r13                   -0.045556        0.052797      9.2994e-05       0.0010137
v  r23                   -0.046706        0.051261      3.0259e-05      0.00057448
v  epsilon                  0.0688          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099178      0.00092466       0.0017426
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017861          5.2773         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71349         0.85283


 TIME FOR THE TIME STEP            10326:        0.12919E+03

===============================================================


 INSTANT    0.103270000E-01   TIME STEP NUMBER           10327
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184122143E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.821951106E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276085359E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.970575393E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.263350854E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      40   0.81167E-03   0.45052E-02 0.19888E+01 
c  Velocity[X]                                      0.13741E-03 
c  Velocity[Y]                                      0.12863E-03 
c  Velocity[Z]                                      0.42392E-02 
c  Pressure     0.36447E-04     132   0.92781E-02   0.25709E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57248E-08   0.17006E-08 0.10165E+00 
c  r22          0.10851E-01      13   0.46661E-08   0.18399E-08 0.10238E+00 
c  r33          0.21858E-01      14   0.70422E-08   0.12792E-07 0.12953E+00 
c  r12          0.93852E-03      17   0.68301E-08   0.30674E-09 0.61354E+00 
c  r13          0.46672E-02      18   0.62346E-08   0.14810E-08 0.20003E+00 
c  r23          0.39973E-02      18   0.65905E-08   0.13161E-08 0.20280E+00 
c  epsilon      0.10970E+02      11   0.32476E-08   0.97726E-02 0.16534E+00 
c  TempC        0.25716E+06      16   0.15108E-04   0.84532E-02 0.43340E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63377          0.6135       0.0052553       0.0015072
v  Velocity[Y]            -0.57373          0.5443       0.0030799      0.00087312
v  Velocity[Z]              1.5654          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                -36.424             360          87.637          169.83
v  r11                   0.0010591        0.081935        0.013071        0.018285
v  r22                   0.0011108        0.082634        0.013352        0.018645
v  r33                   0.0016345         0.17435        0.027246        0.037204
v  r12                   -0.010667        0.013627     -0.00023378     -0.00030929
v  r13                   -0.045559        0.052794      9.2994e-05       0.0010137
v  r23                   -0.046706        0.051253       3.026e-05      0.00057448
v  epsilon                0.068801          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099179      0.00092466       0.0017426
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb              0.001786           5.277         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877          0.7135         0.85283


 TIME FOR THE TIME STEP            10327:        0.10186E+03

===============================================================


 INSTANT    0.103280000E-01   TIME STEP NUMBER           10328
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.657733226E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.223083414E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.204285722E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.663982684E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.671095522E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81310E-03   0.45197E-02 0.19915E+01 
c  Velocity[X]                                      0.13878E-03 
c  Velocity[Y]                                      0.12877E-03 
c  Velocity[Z]                                      0.42521E-02 
c  Pressure     0.36458E-04     133   0.92751E-02   0.25718E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.63514E-08   0.16518E-08 0.10011E+00 
c  r22          0.10851E-01      13   0.49821E-08   0.18358E-08 0.10215E+00 
c  r33          0.21858E-01      15   0.53681E-08   0.12548E-07 0.12797E+00 
c  r12          0.93852E-03      18   0.50184E-08   0.30082E-09 0.60600E+00 
c  r13          0.46672E-02      18   0.65052E-08   0.14819E-08 0.19969E+00 
c  r23          0.39973E-02      19   0.54793E-08   0.12818E-08 0.19936E+00 
c  epsilon      0.10970E+02      11   0.33371E-08   0.97808E-02 0.16498E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.84165E-02 0.43324E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61354       0.0052553       0.0015072
v  Velocity[Y]            -0.57357         0.54446       0.0030798      0.00087312
v  Velocity[Z]              1.5654          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                -36.468          360.01          87.633          169.83
v  r11                   0.0010591        0.081941        0.013071        0.018285
v  r22                   0.0011108        0.082633        0.013352        0.018645
v  r33                   0.0016345         0.17432        0.027246        0.037204
v  r12                   -0.010665        0.013624     -0.00023378     -0.00030929
v  r13                   -0.045556        0.052797      9.2995e-05       0.0010137
v  r23                   -0.046707        0.051244      3.0262e-05      0.00057448
v  epsilon                0.068803          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099179      0.00092466       0.0017426
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb              0.001786          5.2773         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773          0.7135         0.85283


 TIME FOR THE TIME STEP            10328:        0.11009E+03

===============================================================


 INSTANT    0.103290000E-01   TIME STEP NUMBER           10329
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.349121085E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.552319417E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.567135586E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.211308766E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.375043993E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81174E-03   0.45521E-02 0.19965E+01 
c  Velocity[X]                                      0.13858E-03 
c  Velocity[Y]                                      0.12882E-03 
c  Velocity[Z]                                      0.42847E-02 
c  Pressure     0.36591E-04     133   0.93117E-02   0.25810E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.61751E-08   0.16723E-08 0.10093E+00 
c  r22          0.10851E-01      13   0.50260E-08   0.18607E-08 0.10283E+00 
c  r33          0.21858E-01      15   0.54626E-08   0.12714E-07 0.12901E+00 
c  r12          0.93852E-03      18   0.56908E-08   0.29927E-09 0.60744E+00 
c  r13          0.46672E-02      18   0.68304E-08   0.15076E-08 0.20170E+00 
c  r23          0.39973E-02      19   0.56960E-08   0.12979E-08 0.20099E+00 
c  epsilon      0.10970E+02      11   0.33416E-08   0.97054E-02 0.16415E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.84533E-02 0.43328E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61353       0.0052552       0.0015072
v  Velocity[Y]            -0.57361         0.54441       0.0030799      0.00087315
v  Velocity[Z]              1.5657          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4373          4.3406          4.3632
v  Pressure                -36.416          360.15          87.719          169.95
v  r11                   0.0010591        0.081942        0.013071        0.018285
v  r22                   0.0011108        0.082634        0.013352        0.018645
v  r33                   0.0016345         0.17429        0.027246        0.037204
v  r12                   -0.010663        0.013628     -0.00023378     -0.00030929
v  r13                   -0.045556        0.052799      9.2996e-05       0.0010137
v  r23                   -0.046707        0.051232      3.0263e-05      0.00057448
v  epsilon                0.068804          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05        0.009918      0.00092466       0.0017426
v  CourantNb                0.4422             0.6         0.59908         0.59839
v  FourierNb              0.001786          5.2769         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71349         0.85283


 TIME FOR THE TIME STEP            10329:        0.10231E+03

===============================================================


 INSTANT    0.103300000E-01   TIME STEP NUMBER           10330
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.756018536E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.359878220E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.719185715E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129351288E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.277405590E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81277E-03   0.45192E-02 0.19912E+01 
c  Velocity[X]                                      0.13827E-03 
c  Velocity[Y]                                      0.12923E-03 
c  Velocity[Z]                                      0.42517E-02 
c  Pressure     0.36342E-04     131   0.92551E-02   0.25634E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58930E-08   0.16367E-08 0.10001E+00 
c  r22          0.10851E-01      13   0.50504E-08   0.18136E-08 0.10162E+00 
c  r33          0.21858E-01      15   0.63427E-08   0.12460E-07 0.12806E+00 
c  r12          0.93852E-03      18   0.52565E-08   0.29626E-09 0.60368E+00 
c  r13          0.46672E-02      19   0.61816E-08   0.14742E-08 0.19931E+00 
c  r23          0.39973E-02      19   0.65883E-08   0.12722E-08 0.20058E+00 
c  epsilon      0.10970E+02      11   0.33850E-08   0.10001E-01 0.17138E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.83717E-02 0.43196E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61348       0.0052552       0.0015072
v  Velocity[Y]            -0.57346         0.54427       0.0030798      0.00087311
v  Velocity[Z]              1.5655          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4373          4.3406          4.3632
v  Pressure                -36.462          359.99          87.644          169.83
v  r11                   0.0010591        0.081944        0.013072        0.018285
v  r22                   0.0011108        0.082634        0.013352        0.018645
v  r33                   0.0016345          0.1743        0.027246        0.037204
v  r12                   -0.010666        0.013628     -0.00023378     -0.00030929
v  r13                   -0.045559        0.052798      9.2997e-05       0.0010137
v  r23                   -0.046706        0.051263      3.0264e-05      0.00057448
v  epsilon                0.068805          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099181      0.00092466       0.0017426
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb              0.001786          5.2764         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8764          0.7135         0.85283


 TIME FOR THE TIME STEP            10330:        0.87864E+02

===============================================================


 INSTANT    0.103310000E-01   TIME STEP NUMBER           10331
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.715698221E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.180287812E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.502096463E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.164788780E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209467711E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81193E-03   0.45448E-02 0.19963E+01 
c  Velocity[X]                                      0.13763E-03 
c  Velocity[Y]                                      0.12918E-03 
c  Velocity[Z]                                      0.42780E-02 
c  Pressure     0.36435E-04     132   0.92871E-02   0.25701E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57600E-08   0.16423E-08 0.10013E+00 
c  r22          0.10851E-01      13   0.49957E-08   0.18651E-08 0.10244E+00 
c  r33          0.21858E-01      15   0.52531E-08   0.12647E-07 0.12836E+00 
c  r12          0.93852E-03      18   0.53614E-08   0.30067E-09 0.60689E+00 
c  r13          0.46672E-02      18   0.70885E-08   0.15033E-08 0.20043E+00 
c  r23          0.39973E-02      19   0.56145E-08   0.12844E-08 0.20053E+00 
c  epsilon      0.10970E+02      11   0.33368E-08   0.97939E-02 0.16414E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.84008E-02 0.43253E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61352       0.0052553       0.0015072
v  Velocity[Y]            -0.57354         0.54432       0.0030799      0.00087317
v  Velocity[Z]              1.5656          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4373          4.3406          4.3632
v  Pressure                -36.413          359.98          87.625          169.82
v  r11                   0.0010591        0.081944        0.013072        0.018285
v  r22                   0.0011108        0.082629        0.013352        0.018645
v  r33                   0.0016345         0.17433        0.027246        0.037204
v  r12                   -0.010665        0.013626     -0.00023378     -0.00030929
v  r13                   -0.045556        0.052798      9.2998e-05       0.0010137
v  r23                   -0.046707        0.051258      3.0265e-05      0.00057448
v  epsilon                0.068806          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05        0.009918      0.00092466       0.0017426
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb              0.001786          5.2764         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8764         0.71349         0.85283


 TIME FOR THE TIME STEP            10331:        0.97611E+02

===============================================================


 INSTANT    0.103320000E-01   TIME STEP NUMBER           10332
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.113071507E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122482638E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237614588E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.131598332E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.689495929E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81296E-03   0.45312E-02 0.19919E+01 
c  Velocity[X]                                      0.13858E-03 
c  Velocity[Y]                                      0.12896E-03 
c  Velocity[Z]                                      0.42637E-02 
c  Pressure     0.36622E-04     133   0.93201E-02   0.25832E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60628E-08   0.16539E-08 0.10009E+00 
c  r22          0.10851E-01      13   0.45906E-08   0.18382E-08 0.10170E+00 
c  r33          0.21858E-01      15   0.51831E-08   0.12574E-07 0.12734E+00 
c  r12          0.93852E-03      18   0.49659E-08   0.29908E-09 0.60633E+00 
c  r13          0.46672E-02      19   0.52573E-08   0.15179E-08 0.20031E+00 
c  r23          0.39973E-02      19   0.54379E-08   0.12888E-08 0.19960E+00 
c  epsilon      0.10970E+02      11   0.33738E-08   0.99291E-02 0.16478E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.84264E-02 0.43290E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61351       0.0052553       0.0015072
v  Velocity[Y]             -0.5733         0.54447       0.0030799      0.00087314
v  Velocity[Z]              1.5655          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4373          4.3406          4.3632
v  Pressure                -36.478          360.01          87.644          169.84
v  r11                   0.0010591        0.081943        0.013072        0.018285
v  r22                   0.0011108        0.082629        0.013352        0.018645
v  r33                   0.0016345          0.1743        0.027246        0.037204
v  r12                   -0.010663        0.013626     -0.00023378     -0.00030929
v  r13                   -0.045555        0.052799      9.2999e-05       0.0010137
v  r23                   -0.046707        0.051251      3.0267e-05      0.00057449
v  epsilon                0.068808          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05        0.009918      0.00092466       0.0017426
v  CourantNb               0.44217             0.6         0.59908         0.59839
v  FourierNb             0.0017859          5.2768         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768          0.7135         0.85283


 TIME FOR THE TIME STEP            10332:        0.90411E+02

===============================================================


 INSTANT    0.103330000E-01   TIME STEP NUMBER           10333
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.342096518E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.373756715E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.201711810E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.191098696E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.472325256E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81302E-03   0.45292E-02 0.19923E+01 
c  Velocity[X]                                      0.13791E-03 
c  Velocity[Y]                                      0.12858E-03 
c  Velocity[Z]                                      0.42628E-02 
c  Pressure     0.36237E-04     133   0.92300E-02   0.25561E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.64963E-08   0.16468E-08 0.10007E+00 
c  r22          0.10851E-01      13   0.50106E-08   0.18139E-08 0.10122E+00 
c  r33          0.21858E-01      15   0.59041E-08   0.12463E-07 0.12724E+00 
c  r12          0.93852E-03      18   0.58333E-08   0.29476E-09 0.60320E+00 
c  r13          0.46672E-02      19   0.62305E-08   0.14715E-08 0.19862E+00 
c  r23          0.39973E-02      19   0.60822E-08   0.12641E-08 0.19883E+00 
c  epsilon      0.10970E+02      11   0.33896E-08   0.98127E-02 0.16419E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.84097E-02 0.43251E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61349       0.0052554       0.0015073
v  Velocity[Y]             -0.5734         0.54424       0.0030799      0.00087317
v  Velocity[Z]              1.5655          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4373          4.3406          4.3632
v  Pressure                -36.452          360.04           87.65          169.87
v  r11                   0.0010591        0.081948        0.013072        0.018285
v  r22                   0.0011108         0.08263        0.013352        0.018645
v  r33                   0.0016345         0.17427        0.027246        0.037204
v  r12                   -0.010667         0.01362     -0.00023378     -0.00030929
v  r13                   -0.045559        0.052798         9.3e-05       0.0010137
v  r23                   -0.046707        0.051278      3.0268e-05      0.00057449
v  epsilon                0.068809          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05       0.0099181      0.00092466       0.0017426
v  CourantNb               0.44217             0.6         0.59908         0.59839
v  FourierNb             0.0017859          5.2772         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772          0.7135         0.85283


 TIME FOR THE TIME STEP            10333:        0.10151E+03

===============================================================


 INSTANT    0.103340000E-01   TIME STEP NUMBER           10334
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.542550014E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.845068725E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.426345361E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935021E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.743779577E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.370459224E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81179E-03   0.45470E-02 0.19974E+01 
c  Velocity[X]                                      0.13825E-03 
c  Velocity[Y]                                      0.12948E-03 
c  Velocity[Z]                                      0.42792E-02 
c  Pressure     0.36776E-04     133   0.93543E-02   0.25940E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.68497E-08   0.16606E-08 0.10047E+00 
c  r22          0.10851E-01      13   0.50672E-08   0.18744E-08 0.10237E+00 
c  r33          0.21858E-01      15   0.54558E-08   0.12760E-07 0.12822E+00 
c  r12          0.93853E-03      18   0.52644E-08   0.30514E-09 0.60971E+00 
c  r13          0.46672E-02      19   0.63950E-08   0.15189E-08 0.20067E+00 
c  r23          0.39973E-02      19   0.54181E-08   0.12906E-08 0.20061E+00 
c  epsilon      0.10970E+02      11   0.33456E-08   0.10181E-01 0.16691E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.84383E-02 0.43324E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386          0.6135       0.0052554       0.0015073
v  Velocity[Y]            -0.57339         0.54433       0.0030799      0.00087315
v  Velocity[Z]              1.5655          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4373          4.3406          4.3632
v  Pressure                -36.481          359.99          87.634          169.83
v  r11                   0.0010591        0.081954        0.013072        0.018285
v  r22                   0.0011108        0.082631        0.013352        0.018645
v  r33                   0.0016345         0.17429        0.027246        0.037204
v  r12                   -0.010667         0.01362     -0.00023378     -0.00030929
v  r13                   -0.045555          0.0528      9.3002e-05       0.0010137
v  r23                   -0.046708        0.051263       3.027e-05      0.00057449
v  epsilon                 0.06881          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05       0.0099181      0.00092467       0.0017426
v  CourantNb               0.44218             0.6         0.59908         0.59839
v  FourierNb             0.0017859          5.2778         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778          0.7135         0.85283


 TIME FOR THE TIME STEP            10334:        0.10709E+03

===============================================================


 INSTANT    0.103350000E-01   TIME STEP NUMBER           10335
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.377563051E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.615470426E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.126154840E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.605428455E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195187290E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81240E-03   0.45370E-02 0.19943E+01 
c  Velocity[X]                                      0.13930E-03 
c  Velocity[Y]                                      0.12894E-03 
c  Velocity[Z]                                      0.42688E-02 
c  Pressure     0.36139E-04     133   0.92069E-02   0.25491E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.69800E-08   0.16363E-08 0.99905E-01 
c  r22          0.10851E-01      13   0.57303E-08   0.18247E-08 0.10131E+00 
c  r33          0.21858E-01      15   0.58426E-08   0.12466E-07 0.12715E+00 
c  r12          0.93853E-03      18   0.57343E-08   0.30040E-09 0.60816E+00 
c  r13          0.46672E-02      19   0.65385E-08   0.14840E-08 0.19897E+00 
c  r23          0.39973E-02      19   0.57191E-08   0.12787E-08 0.19951E+00 
c  epsilon      0.10970E+02      11   0.35092E-08   0.96355E-02 0.16203E+00 
c  TempC        0.25716E+06      16   0.15103E-04   0.84588E-02 0.43374E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61353       0.0052554       0.0015073
v  Velocity[Y]             -0.5735         0.54453       0.0030799      0.00087317
v  Velocity[Z]              1.5654          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                -36.466          360.04          87.658          169.86
v  r11                   0.0010591        0.081954        0.013072        0.018285
v  r22                   0.0011108        0.082631        0.013352        0.018645
v  r33                   0.0016345         0.17431        0.027246        0.037204
v  r12                   -0.010664        0.013624     -0.00023378     -0.00030929
v  r13                   -0.045555        0.052797      9.3002e-05       0.0010137
v  r23                   -0.046708        0.051246      3.0271e-05      0.00057449
v  epsilon                0.068812          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099182      0.00092467       0.0017426
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017859          5.2779         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71349         0.85283


 TIME FOR THE TIME STEP            10335:        0.10497E+03

===============================================================


 INSTANT    0.103360000E-01   TIME STEP NUMBER           10336
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.399732957E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.256145273E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140124069E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199291216E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.477087705E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81287E-03   0.45162E-02 0.19894E+01 
c  Velocity[X]                                      0.13842E-03 
c  Velocity[Y]                                      0.12937E-03 
c  Velocity[Z]                                      0.42484E-02 
c  Pressure     0.36732E-04     132   0.93417E-02   0.25910E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.66533E-08   0.16462E-08 0.10024E+00 
c  r22          0.10851E-01      13   0.55872E-08   0.18418E-08 0.10199E+00 
c  r33          0.21858E-01      15   0.67915E-08   0.12475E-07 0.12751E+00 
c  r12          0.93853E-03      18   0.54736E-08   0.30276E-09 0.60632E+00 
c  r13          0.46672E-02      19   0.67828E-08   0.14865E-08 0.20012E+00 
c  r23          0.39973E-02      20   0.56160E-08   0.12727E-08 0.19863E+00 
c  epsilon      0.10970E+02      11   0.34535E-08   0.98462E-02 0.16445E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.83932E-02 0.43265E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161987


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61349       0.0052554       0.0015073
v  Velocity[Y]            -0.57346         0.54425       0.0030799      0.00087318
v  Velocity[Z]              1.5657          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4373          4.3406          4.3632
v  Pressure                -36.508          360.08           87.67          169.89
v  r11                   0.0010591        0.081951        0.013072        0.018285
v  r22                   0.0011108        0.082631        0.013352        0.018645
v  r33                   0.0016345         0.17434        0.027246        0.037204
v  r12                   -0.010663        0.013626     -0.00023378     -0.00030929
v  r13                   -0.045557        0.052793      9.3002e-05       0.0010137
v  r23                   -0.046708         0.05127      3.0272e-05      0.00057449
v  epsilon                0.068813          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099182      0.00092467       0.0017426
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2778         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71349         0.85283


 TIME FOR THE TIME STEP            10336:        0.96235E+02

===============================================================


 INSTANT    0.103370000E-01   TIME STEP NUMBER           10337
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.891277904E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.900130781E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.481623997E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.756614524E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.583201748E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81196E-03   0.45419E-02 0.19957E+01 
c  Velocity[X]                                      0.13872E-03 
c  Velocity[Y]                                      0.12967E-03 
c  Velocity[Z]                                      0.42735E-02 
c  Pressure     0.36178E-04     132   0.92078E-02   0.25519E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.62282E-08   0.16577E-08 0.10051E+00 
c  r22          0.10851E-01      13   0.58887E-08   0.18654E-08 0.10238E+00 
c  r33          0.21858E-01      15   0.56823E-08   0.12810E-07 0.12884E+00 
c  r12          0.93853E-03      18   0.59629E-08   0.30312E-09 0.61126E+00 
c  r13          0.46673E-02      19   0.69846E-08   0.15487E-08 0.20217E+00 
c  r23          0.39973E-02      20   0.60003E-08   0.13147E-08 0.20203E+00 
c  epsilon      0.10970E+02      11   0.32718E-08   0.10430E-01 0.17174E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.84208E-02 0.43323E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61356       0.0052555       0.0015073
v  Velocity[Y]            -0.57347         0.54427       0.0030799      0.00087319
v  Velocity[Z]              1.5653          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4373          4.3406          4.3632
v  Pressure                -36.431          359.97          87.604           169.8
v  r11                   0.0010591        0.081957        0.013072        0.018285
v  r22                   0.0011108        0.082629        0.013352        0.018645
v  r33                   0.0016345         0.17433        0.027246        0.037204
v  r12                   -0.010666        0.013626     -0.00023378     -0.00030929
v  r13                   -0.045557         0.05279      9.3004e-05       0.0010137
v  r23                   -0.046708        0.051254      3.0274e-05      0.00057449
v  epsilon                0.068814          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099182      0.00092467       0.0017426
v  CourantNb                0.4422             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2767         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767          0.7135         0.85283


 TIME FOR THE TIME STEP            10337:        0.86544E+02

===============================================================


 INSTANT    0.103380000E-01   TIME STEP NUMBER           10338
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.982017002E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.270311543E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.419857821E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.286225524E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.272254987E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81239E-03   0.45103E-02 0.19890E+01 
c  Velocity[X]                                      0.13864E-03 
c  Velocity[Y]                                      0.12932E-03 
c  Velocity[Z]                                      0.42424E-02 
c  Pressure     0.36536E-04     133   0.92993E-02   0.25771E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60583E-08   0.16644E-08 0.10044E+00 
c  r22          0.10851E-01      13   0.52148E-08   0.18317E-08 0.10155E+00 
c  r33          0.21858E-01      15   0.56654E-08   0.12611E-07 0.12782E+00 
c  r12          0.93853E-03      18   0.57492E-08   0.30428E-09 0.61005E+00 
c  r13          0.46673E-02      19   0.71573E-08   0.15066E-08 0.20005E+00 
c  r23          0.39973E-02      19   0.67047E-08   0.12970E-08 0.20053E+00 
c  epsilon      0.10970E+02      11   0.33475E-08   0.10093E-01 0.16657E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.84856E-02 0.43379E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61352       0.0052556       0.0015074
v  Velocity[Y]            -0.57352         0.54441         0.00308      0.00087319
v  Velocity[Z]              1.5654          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                -36.482          360.01          87.644          169.84
v  r11                   0.0010591        0.081961        0.013072        0.018285
v  r22                   0.0011108        0.082627        0.013352        0.018645
v  r33                   0.0016345         0.17429        0.027246        0.037204
v  r12                   -0.010665        0.013629     -0.00023378     -0.00030929
v  r13                   -0.045555        0.052791      9.3004e-05       0.0010137
v  r23                   -0.046708        0.051244      3.0275e-05      0.00057449
v  epsilon                0.068816          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099181      0.00092467       0.0017426
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2765         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765          0.7135         0.85283


 TIME FOR THE TIME STEP            10338:        0.88070E+02

===============================================================


 INSTANT    0.103390000E-01   TIME STEP NUMBER           10339
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.349668947E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.429566069E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.372252019E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.562876957E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.234258026E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81334E-03   0.45411E-02 0.19941E+01 
c  Velocity[X]                                      0.13808E-03 
c  Velocity[Y]                                      0.12829E-03 
c  Velocity[Z]                                      0.42747E-02 
c  Pressure     0.36589E-04     131   0.93203E-02   0.25809E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58499E-08   0.16297E-08 0.99650E-01 
c  r22          0.10851E-01      13   0.56125E-08   0.18382E-08 0.10202E+00 
c  r33          0.21858E-01      15   0.58313E-08   0.12486E-07 0.12751E+00 
c  r12          0.93853E-03      18   0.61433E-08   0.29573E-09 0.60709E+00 
c  r13          0.46673E-02      19   0.62071E-08   0.14991E-08 0.20045E+00 
c  r23          0.39973E-02      19   0.67992E-08   0.12841E-08 0.19939E+00 
c  epsilon      0.10970E+02      11   0.34317E-08   0.97162E-02 0.16439E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.83937E-02 0.43246E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61351       0.0052555       0.0015074
v  Velocity[Y]            -0.57359         0.54452       0.0030799      0.00087322
v  Velocity[Z]              1.5655          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4373          4.3406          4.3632
v  Pressure                -36.414          360.07          87.663          169.88
v  r11                   0.0010591        0.081966        0.013072        0.018285
v  r22                   0.0011108        0.082621        0.013352        0.018645
v  r33                   0.0016345         0.17429        0.027246        0.037204
v  r12                   -0.010662        0.013634     -0.00023378     -0.00030929
v  r13                   -0.045558        0.052792      9.3005e-05       0.0010137
v  r23                   -0.046708        0.051267      3.0276e-05      0.00057449
v  epsilon                0.068817          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099181      0.00092467       0.0017426
v  CourantNb                0.4422             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2765         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765          0.7135         0.85283


 TIME FOR THE TIME STEP            10339:        0.95716E+02

===============================================================


 INSTANT    0.103400000E-01   TIME STEP NUMBER           10340
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.585696011E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.135902822E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934899E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.725372658E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.179519809E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.267331750E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81174E-03   0.45364E-02 0.19950E+01 
c  Velocity[X]                                      0.13896E-03 
c  Velocity[Y]                                      0.12896E-03 
c  Velocity[Z]                                      0.42685E-02 
c  Pressure     0.36499E-04     132   0.92883E-02   0.25747E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56037E-08   0.16283E-08 0.99996E-01 
c  r22          0.10851E-01      13   0.51405E-08   0.17910E-08 0.10150E+00 
c  r33          0.21858E-01      15   0.65626E-08   0.12308E-07 0.12757E+00 
c  r12          0.93853E-03      18   0.57118E-08   0.30279E-09 0.61072E+00 
c  r13          0.46673E-02      19   0.58814E-08   0.14735E-08 0.19993E+00 
c  r23          0.39973E-02      19   0.64427E-08   0.12697E-08 0.19967E+00 
c  epsilon      0.10970E+02      11   0.35211E-08   0.92143E-02 0.16089E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.83761E-02 0.43222E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63395         0.61354       0.0052555       0.0015074
v  Velocity[Y]            -0.57353         0.54434       0.0030799      0.00087321
v  Velocity[Z]              1.5654          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4373          4.3406          4.3632
v  Pressure                -36.471             360          87.641          169.83
v  r11                   0.0010591        0.081985        0.013072        0.018285
v  r22                   0.0011108         0.08262        0.013352        0.018645
v  r33                   0.0016345         0.17432        0.027246        0.037204
v  r12                   -0.010666        0.013632     -0.00023378     -0.00030929
v  r13                   -0.045555        0.052792      9.3006e-05       0.0010137
v  r23                   -0.046707        0.051248      3.0276e-05      0.00057449
v  epsilon                0.068818          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099181      0.00092467       0.0017426
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2773         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773          0.7135         0.85283


 TIME FOR THE TIME STEP            10340:        0.11867E+03

===============================================================


 INSTANT    0.103410000E-01   TIME STEP NUMBER           10341
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.157596382E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.124396757E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.152950002E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.437887832E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.929884055E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81240E-03   0.45502E-02 0.19974E+01 
c  Velocity[X]                                      0.14018E-03 
c  Velocity[Y]                                      0.12888E-03 
c  Velocity[Z]                                      0.42811E-02 
c  Pressure     0.36410E-04     134   0.92686E-02   0.25683E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.61366E-08   0.16406E-08 0.10008E+00 
c  r22          0.10851E-01      13   0.58086E-08   0.18143E-08 0.10135E+00 
c  r33          0.21858E-01      15   0.52476E-08   0.12512E-07 0.12782E+00 
c  r12          0.93853E-03      18   0.62954E-08   0.29159E-09 0.60387E+00 
c  r13          0.46673E-02      19   0.61700E-08   0.14857E-08 0.19967E+00 
c  r23          0.39973E-02      19   0.60924E-08   0.12730E-08 0.19975E+00 
c  epsilon      0.10970E+02      11   0.33556E-08   0.98456E-02 0.16495E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.84512E-02 0.43366E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61352       0.0052556       0.0015074
v  Velocity[Y]            -0.57364         0.54449         0.00308      0.00087324
v  Velocity[Z]              1.5657          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4373          4.3406          4.3632
v  Pressure                -36.462          360.08          87.693          169.91
v  r11                   0.0010591        0.081989        0.013072        0.018285
v  r22                   0.0011108        0.082621        0.013352        0.018645
v  r33                   0.0016345          0.1743        0.027246        0.037204
v  r12                   -0.010664        0.013636     -0.00023378     -0.00030929
v  r13                   -0.045556        0.052791      9.3007e-05       0.0010137
v  r23                   -0.046707         0.05124      3.0278e-05      0.00057449
v  epsilon                0.068819          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099181      0.00092467       0.0017426
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2774         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774          0.7135         0.85283


 TIME FOR THE TIME STEP            10341:        0.10222E+03

===============================================================


 INSTANT    0.103420000E-01   TIME STEP NUMBER           10342
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.105402102E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.865206616E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.190374614E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935015E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136815901E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.353352817E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      40   0.81271E-03   0.45045E-02 0.19871E+01 
c  Velocity[X]                                      0.13761E-03 
c  Velocity[Y]                                      0.12951E-03 
c  Velocity[Z]                                      0.42374E-02 
c  Pressure     0.36540E-04     131   0.92984E-02   0.25773E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55884E-08   0.16305E-08 0.99865E-01 
c  r22          0.10851E-01      13   0.54697E-08   0.18140E-08 0.10156E+00 
c  r33          0.21858E-01      15   0.56801E-08   0.12406E-07 0.12744E+00 
c  r12          0.93853E-03      17   0.69352E-08   0.29492E-09 0.60541E+00 
c  r13          0.46673E-02      19   0.59166E-08   0.14865E-08 0.19978E+00 
c  r23          0.39973E-02      19   0.57832E-08   0.12805E-08 0.19950E+00 
c  epsilon      0.10970E+02      11   0.34276E-08   0.96951E-02 0.16424E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.83796E-02 0.43173E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61351       0.0052556       0.0015074
v  Velocity[Y]            -0.57346          0.5442         0.00308      0.00087319
v  Velocity[Z]              1.5657          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4373          4.3406          4.3632
v  Pressure                -36.471          360.03          87.651          169.85
v  r11                   0.0010591        0.082001        0.013072        0.018285
v  r22                   0.0011108        0.082622        0.013352        0.018645
v  r33                   0.0016345         0.17428        0.027246        0.037204
v  r12                   -0.010665        0.013634     -0.00023378     -0.00030929
v  r13                   -0.045558        0.052791      9.3008e-05       0.0010137
v  r23                   -0.046707        0.051264      3.0279e-05      0.00057449
v  epsilon                0.068821          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05        0.009918      0.00092468       0.0017426
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017857           5.278         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878          0.7135         0.85283


 TIME FOR THE TIME STEP            10342:        0.10192E+03

===============================================================


 INSTANT    0.103430000E-01   TIME STEP NUMBER           10343
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.152840150E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.322572758E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195942924E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.566175475E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.378716080E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81266E-03   0.45311E-02 0.19937E+01 
c  Velocity[X]                                      0.13772E-03 
c  Velocity[Y]                                      0.12922E-03 
c  Velocity[Z]                                      0.42641E-02 
c  Pressure     0.36535E-04     133   0.93009E-02   0.25770E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54690E-08   0.16641E-08 0.10071E+00 
c  r22          0.10851E-01      13   0.51133E-08   0.18258E-08 0.10140E+00 
c  r33          0.21858E-01      15   0.56277E-08   0.12672E-07 0.12815E+00 
c  r12          0.93853E-03      18   0.52594E-08   0.29838E-09 0.60591E+00 
c  r13          0.46673E-02      19   0.60137E-08   0.15057E-08 0.20033E+00 
c  r23          0.39973E-02      19   0.61306E-08   0.13080E-08 0.20099E+00 
c  epsilon      0.10970E+02      11   0.32903E-08   0.10295E-01 0.17051E+00 
c  TempC        0.25716E+06      16   0.15084E-04   0.84380E-02 0.43350E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61354       0.0052556       0.0015074
v  Velocity[Y]            -0.57354         0.54424         0.00308      0.00087322
v  Velocity[Z]              1.5656          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4373          4.3406          4.3632
v  Pressure                -36.415          359.96          87.601          169.79
v  r11                   0.0010591        0.081996        0.013072        0.018285
v  r22                   0.0011108        0.082622        0.013352        0.018645
v  r33                   0.0016346         0.17429        0.027246        0.037204
v  r12                   -0.010664        0.013635     -0.00023378     -0.00030929
v  r13                   -0.045555        0.052789      9.3009e-05       0.0010137
v  r23                   -0.046708        0.051256      3.0281e-05      0.00057449
v  epsilon                0.068822          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05        0.009918      0.00092468       0.0017426
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017857           5.278         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878          0.7135         0.85283


 TIME FOR THE TIME STEP            10343:        0.10257E+03

===============================================================


 INSTANT    0.103440000E-01   TIME STEP NUMBER           10344
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.164463226E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.293431711E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.401836938E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105884759E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.711271583E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81260E-03   0.45487E-02 0.19973E+01 
c  Velocity[X]                                      0.13968E-03 
c  Velocity[Y]                                      0.12929E-03 
c  Velocity[Z]                                      0.42798E-02 
c  Pressure     0.36713E-04     132   0.93490E-02   0.25897E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59467E-08   0.16615E-08 0.10034E+00 
c  r22          0.10851E-01      13   0.52246E-08   0.18892E-08 0.10250E+00 
c  r33          0.21858E-01      15   0.51110E-08   0.12852E-07 0.12847E+00 
c  r12          0.93853E-03      18   0.56498E-08   0.30154E-09 0.60825E+00 
c  r13          0.46673E-02      19   0.56662E-08   0.15319E-08 0.20129E+00 
c  r23          0.39973E-02      19   0.58334E-08   0.12881E-08 0.19942E+00 
c  epsilon      0.10970E+02      11   0.32453E-08   0.10439E-01 0.17007E+00 
c  TempC        0.25716E+06      16   0.15189E-04   0.84960E-02 0.43506E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61352       0.0052556       0.0015073
v  Velocity[Y]             -0.5736          0.5444         0.00308      0.00087321
v  Velocity[Z]              1.5656          5.4373          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4373          4.3406          4.3632
v  Pressure                -36.471          360.06           87.69          169.89
v  r11                   0.0010591        0.081985        0.013072        0.018285
v  r22                   0.0011108        0.082622        0.013352        0.018645
v  r33                   0.0016346         0.17431        0.027246        0.037204
v  r12                   -0.010665        0.013635     -0.00023378     -0.00030929
v  r13                   -0.045554        0.052791       9.301e-05       0.0010137
v  r23                   -0.046707        0.051239      3.0282e-05       0.0005745
v  epsilon                0.068823          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099179      0.00092468       0.0017426
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017857          5.2783         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783          0.7135         0.85283


 TIME FOR THE TIME STEP            10344:        0.88142E+02

===============================================================


 INSTANT    0.103450000E-01   TIME STEP NUMBER           10345
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181532315E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.168690699E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.388832323E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155390626E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.423821381E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81241E-03   0.45111E-02 0.19896E+01 
c  Velocity[X]                                      0.13792E-03 
c  Velocity[Y]                                      0.12829E-03 
c  Velocity[Z]                                      0.42449E-02 
c  Pressure     0.36211E-04     133   0.92128E-02   0.25542E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57840E-08   0.16487E-08 0.10001E+00 
c  r22          0.10851E-01      13   0.48914E-08   0.18232E-08 0.10143E+00 
c  r33          0.21858E-01      15   0.51918E-08   0.12546E-07 0.12738E+00 
c  r12          0.93853E-03      17   0.69446E-08   0.29434E-09 0.60458E+00 
c  r13          0.46673E-02      19   0.56378E-08   0.14924E-08 0.19937E+00 
c  r23          0.39973E-02      19   0.58205E-08   0.12861E-08 0.19939E+00 
c  epsilon      0.10970E+02      11   0.33232E-08   0.10095E-01 0.16688E+00 
c  TempC        0.25716E+06      16   0.15106E-04   0.84145E-02 0.43260E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61352       0.0052556       0.0015074
v  Velocity[Y]            -0.57363         0.54453         0.00308      0.00087322
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.464          360.06           87.65          169.87
v  r11                   0.0010591        0.081965        0.013072        0.018285
v  r22                   0.0011108        0.082619        0.013352        0.018645
v  r33                   0.0016346         0.17434        0.027246        0.037204
v  r12                   -0.010664        0.013624     -0.00023378     -0.00030929
v  r13                   -0.045558        0.052792      9.3011e-05       0.0010137
v  r23                   -0.046707        0.051219      3.0283e-05       0.0005745
v  epsilon                0.068825          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099179      0.00092468       0.0017426
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017857          5.2781         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71349         0.85283


 TIME FOR THE TIME STEP            10345:        0.96330E+02

===============================================================


 INSTANT    0.103460000E-01   TIME STEP NUMBER           10346
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120001008E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199127596E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.465390150E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.971310848E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.345581863E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81152E-03   0.45248E-02 0.19954E+01 
c  Velocity[X]                                      0.13866E-03 
c  Velocity[Y]                                      0.12892E-03 
c  Velocity[Z]                                      0.42572E-02 
c  Pressure     0.36471E-04     133   0.92788E-02   0.25725E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.62998E-08   0.16156E-08 0.99371E-01 
c  r22          0.10851E-01      13   0.48253E-08   0.17941E-08 0.10100E+00 
c  r33          0.21858E-01      15   0.55680E-08   0.12344E-07 0.12691E+00 
c  r12          0.93853E-03      17   0.69355E-08   0.28839E-09 0.59953E+00 
c  r13          0.46673E-02      19   0.54958E-08   0.14655E-08 0.19872E+00 
c  r23          0.39973E-02      19   0.56450E-08   0.12765E-08 0.19840E+00 
c  epsilon      0.10970E+02      11   0.34209E-08   0.95474E-02 0.16411E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.84072E-02 0.43224E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394          0.6135       0.0052556       0.0015074
v  Velocity[Y]            -0.57355         0.54433         0.00308      0.00087321
v  Velocity[Z]              1.5652          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.461          359.96          87.628          169.81
v  r11                   0.0010591        0.081948        0.013072        0.018285
v  r22                   0.0011109        0.082621        0.013352        0.018645
v  r33                   0.0016346         0.17432        0.027246        0.037204
v  r12                   -0.010668        0.013623     -0.00023378     -0.00030929
v  r13                   -0.045554        0.052794      9.3012e-05       0.0010137
v  r23                   -0.046707        0.051244      3.0285e-05       0.0005745
v  epsilon                0.068826          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099178      0.00092468       0.0017426
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2778         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71349         0.85282


 TIME FOR THE TIME STEP            10346:        0.12025E+03

===============================================================


 INSTANT    0.103470000E-01   TIME STEP NUMBER           10347
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.658525214E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.484976607E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.175116754E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.950314099E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.212174138E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81212E-03   0.45556E-02 0.19995E+01 
c  Velocity[X]                                      0.13952E-03 
c  Velocity[Y]                                      0.12936E-03 
c  Velocity[Z]                                      0.42867E-02 
c  Pressure     0.36690E-04     132   0.93338E-02   0.25880E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.61170E-08   0.16453E-08 0.10003E+00 
c  r22          0.10851E-01      13   0.50437E-08   0.18313E-08 0.10159E+00 
c  r33          0.21858E-01      15   0.56500E-08   0.12562E-07 0.12755E+00 
c  r12          0.93853E-03      17   0.68783E-08   0.29436E-09 0.60342E+00 
c  r13          0.46673E-02      19   0.62208E-08   0.14955E-08 0.19967E+00 
c  r23          0.39973E-02      19   0.55537E-08   0.12703E-08 0.19831E+00 
c  epsilon      0.10970E+02      11   0.32551E-08   0.10109E-01 0.16875E+00 
c  TempC        0.25716E+06      16   0.15121E-04   0.84472E-02 0.43351E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162016


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61355       0.0052556       0.0015074
v  Velocity[Y]            -0.57346         0.54444       0.0030802      0.00087331
v  Velocity[Z]              1.5651          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4374          4.3406          4.3632
v  Pressure                -36.421          360.04          87.662          169.87
v  r11                   0.0010591        0.081937        0.013072        0.018285
v  r22                   0.0011109        0.082622        0.013352        0.018645
v  r33                   0.0016346         0.17428        0.027246        0.037204
v  r12                   -0.010666        0.013621     -0.00023378     -0.00030929
v  r13                   -0.045554         0.05279      9.3013e-05       0.0010137
v  r23                   -0.046707        0.051232      3.0285e-05       0.0005745
v  epsilon                0.068827          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099178      0.00092468       0.0017426
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2776         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776          0.7135         0.85283


 TIME FOR THE TIME STEP            10347:        0.12242E+03

===============================================================


 INSTANT    0.103480000E-01   TIME STEP NUMBER           10348
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181463091E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.196507629E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.582840256E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.140179366E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.221612715E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      40   0.81306E-03   0.45008E-02 0.19866E+01 
c  Velocity[X]                                      0.13832E-03 
c  Velocity[Y]                                      0.12893E-03 
c  Velocity[Z]                                      0.42336E-02 
c  Pressure     0.36312E-04     132   0.92464E-02   0.25613E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.61718E-08   0.16506E-08 0.10002E+00 
c  r22          0.10851E-01      13   0.50472E-08   0.18940E-08 0.10272E+00 
c  r33          0.21858E-01      15   0.54356E-08   0.12782E-07 0.12854E+00 
c  r12          0.93853E-03      17   0.66868E-08   0.30766E-09 0.61132E+00 
c  r13          0.46673E-02      19   0.53740E-08   0.15443E-08 0.20172E+00 
c  r23          0.39973E-02      18   0.63231E-08   0.12848E-08 0.20032E+00 
c  epsilon      0.10970E+02      11   0.32083E-08   0.10174E-01 0.16805E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.83739E-02 0.43197E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63396         0.61352       0.0052557       0.0015074
v  Velocity[Y]             -0.5733         0.54416       0.0030801      0.00087325
v  Velocity[Z]              1.5652          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.506          360.02          87.643          169.84
v  r11                   0.0010591        0.081927        0.013072        0.018285
v  r22                   0.0011109        0.082623        0.013352        0.018645
v  r33                   0.0016346         0.17429        0.027246        0.037204
v  r12                   -0.010666        0.013613     -0.00023378     -0.00030929
v  r13                   -0.045557        0.052789      9.3014e-05       0.0010137
v  r23                   -0.046706        0.051228      3.0286e-05       0.0005745
v  epsilon                0.068828          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05       0.0099179      0.00092468       0.0017426
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2778         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778          0.7135         0.85283


 TIME FOR THE TIME STEP            10348:        0.11494E+03

===============================================================


 INSTANT    0.103490000E-01   TIME STEP NUMBER           10349
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.298487578E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.356538064E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.102289604E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.523827024E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.375814092E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81141E-03   0.45060E-02 0.19880E+01 
c  Velocity[X]                                      0.13879E-03 
c  Velocity[Y]                                      0.12783E-03 
c  Velocity[Z]                                      0.42394E-02 
c  Pressure     0.36306E-04     132   0.92392E-02   0.25610E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60554E-08   0.16625E-08 0.10042E+00 
c  r22          0.10851E-01      13   0.52638E-08   0.18597E-08 0.10228E+00 
c  r33          0.21858E-01      15   0.53828E-08   0.12810E-07 0.12894E+00 
c  r12          0.93853E-03      17   0.69496E-08   0.30072E-09 0.60865E+00 
c  r13          0.46673E-02      19   0.60015E-08   0.15237E-08 0.20120E+00 
c  r23          0.39973E-02      18   0.63315E-08   0.13119E-08 0.20239E+00 
c  epsilon      0.10970E+02      11   0.34763E-08   0.10442E-01 0.17309E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.84303E-02 0.43304E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61354       0.0052556       0.0015074
v  Velocity[Y]            -0.57335         0.54418       0.0030801      0.00087326
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.433          360.08          87.666          169.89
v  r11                   0.0010591        0.081921        0.013072        0.018285
v  r22                   0.0011109        0.082623        0.013352        0.018645
v  r33                   0.0016346         0.17432        0.027246        0.037204
v  r12                   -0.010663         0.01361     -0.00023378     -0.00030929
v  r13                   -0.045557        0.052791      9.3014e-05       0.0010137
v  r23                   -0.046706        0.051257      3.0288e-05       0.0005745
v  epsilon                 0.06883          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099177      0.00092468       0.0017426
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2784         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784          0.7135         0.85283


 TIME FOR THE TIME STEP            10349:        0.12063E+03

===============================================================


 INSTANT    0.103500000E-01   TIME STEP NUMBER           10350
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136421884E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.633791257E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208523033E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.755472655E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.469653709E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81253E-03   0.45505E-02 0.19965E+01 
c  Velocity[X]                                      0.13921E-03 
c  Velocity[Y]                                      0.12919E-03 
c  Velocity[Z]                                      0.42821E-02 
c  Pressure     0.36599E-04     133   0.93191E-02   0.25815E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60971E-08   0.16207E-08 0.99498E-01 
c  r22          0.10851E-01      13   0.50031E-08   0.18196E-08 0.10148E+00 
c  r33          0.21858E-01      14   0.70232E-08   0.12372E-07 0.12716E+00 
c  r12          0.93853E-03      18   0.50665E-08   0.29632E-09 0.60592E+00 
c  r13          0.46673E-02      19   0.59728E-08   0.14978E-08 0.20020E+00 
c  r23          0.39973E-02      18   0.60119E-08   0.12542E-08 0.19785E+00 
c  epsilon      0.10970E+02      11   0.33765E-08   0.97400E-02 0.16461E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.84447E-02 0.43355E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63396         0.61352       0.0052556       0.0015074
v  Velocity[Y]            -0.57327         0.54437       0.0030801      0.00087326
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.466          360.05           87.68          169.88
v  r11                   0.0010591        0.081917        0.013072        0.018285
v  r22                   0.0011109        0.082624        0.013352        0.018645
v  r33                   0.0016346         0.17429        0.027246        0.037204
v  r12                    -0.01066        0.013601     -0.00023378     -0.00030929
v  r13                   -0.045555        0.052793      9.3015e-05       0.0010137
v  r23                   -0.046706        0.051239      3.0288e-05       0.0005745
v  epsilon                0.068831          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099175      0.00092469       0.0017426
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2788         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71349         0.85283


 TIME FOR THE TIME STEP            10350:        0.84579E+02

===============================================================


 INSTANT    0.103510000E-01   TIME STEP NUMBER           10351
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129560635E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.573021876E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.493633675E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.147654657E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.449357829E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      40   0.81241E-03   0.45101E-02 0.19914E+01 
c  Velocity[X]                                      0.13772E-03 
c  Velocity[Y]                                      0.12909E-03 
c  Velocity[Z]                                      0.42433E-02 
c  Pressure     0.36556E-04     132   0.93074E-02   0.25786E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55680E-08   0.16485E-08 0.99599E-01 
c  r22          0.10851E-01      13   0.50612E-08   0.18230E-08 0.10123E+00 
c  r33          0.21858E-01      15   0.57619E-08   0.12432E-07 0.12699E+00 
c  r12          0.93853E-03      18   0.58931E-08   0.29896E-09 0.60696E+00 
c  r13          0.46673E-02      19   0.61691E-08   0.14743E-08 0.19872E+00 
c  r23          0.39973E-02      18   0.67564E-08   0.12958E-08 0.19952E+00 
c  epsilon      0.10970E+02      11   0.35191E-08   0.98783E-02 0.16493E+00 
c  TempC        0.25716E+06      16   0.15104E-04   0.84193E-02 0.43290E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61352       0.0052556       0.0015074
v  Velocity[Y]             -0.5733         0.54449       0.0030801       0.0008733
v  Velocity[Z]              1.5652          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.433          359.97          87.613          169.81
v  r11                   0.0010591        0.081913        0.013072        0.018285
v  r22                   0.0011109        0.082621        0.013352        0.018645
v  r33                   0.0016346         0.17427        0.027246        0.037204
v  r12                   -0.010658         0.01359     -0.00023378     -0.00030929
v  r13                   -0.045557        0.052792      9.3016e-05       0.0010137
v  r23                   -0.046706        0.051224      3.0289e-05       0.0005745
v  epsilon                0.068832          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099174      0.00092469       0.0017426
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2788         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788          0.7135         0.85283


 TIME FOR THE TIME STEP            10351:        0.82661E+02

===============================================================


 INSTANT    0.103520000E-01   TIME STEP NUMBER           10352
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145543080E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.576610509E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.927493052E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.330005819E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.105394970E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      40   0.81230E-03   0.45307E-02 0.19932E+01 
c  Velocity[X]                                      0.13803E-03 
c  Velocity[Y]                                      0.12868E-03 
c  Velocity[Z]                                      0.42640E-02 
c  Pressure     0.36631E-04     133   0.93163E-02   0.25839E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52453E-08   0.16418E-08 0.99707E-01 
c  r22          0.10851E-01      13   0.52162E-08   0.18595E-08 0.10203E+00 
c  r33          0.21858E-01      15   0.52301E-08   0.12716E-07 0.12813E+00 
c  r12          0.93853E-03      18   0.56633E-08   0.29560E-09 0.60566E+00 
c  r13          0.46673E-02      19   0.71374E-08   0.15119E-08 0.20076E+00 
c  r23          0.39973E-02      19   0.52682E-08   0.12904E-08 0.20007E+00 
c  epsilon      0.10970E+02      11   0.34543E-08   0.10244E-01 0.16831E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.84307E-02 0.43342E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61352       0.0052556       0.0015074
v  Velocity[Y]            -0.57331         0.54429       0.0030801      0.00087328
v  Velocity[Z]              1.5652          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.457             360          87.644          169.84
v  r11                   0.0010591        0.081906        0.013072        0.018285
v  r22                   0.0011109        0.082621        0.013352        0.018645
v  r33                   0.0016346         0.17428        0.027246        0.037204
v  r12                   -0.010658        0.013585     -0.00023378     -0.00030929
v  r13                   -0.045554        0.052791      9.3017e-05       0.0010137
v  r23                   -0.046706        0.051216       3.029e-05       0.0005745
v  epsilon                0.068833          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05       0.0099174      0.00092469       0.0017426
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2783         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783          0.7135         0.85283


 TIME FOR THE TIME STEP            10352:        0.88608E+02

===============================================================


 INSTANT    0.103530000E-01   TIME STEP NUMBER           10353
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.644766529E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.352048228E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239052230E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.343589855E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.270262933E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81127E-03   0.45431E-02 0.19971E+01 
c  Velocity[X]                                      0.13964E-03 
c  Velocity[Y]                                      0.12894E-03 
c  Velocity[Z]                                      0.42745E-02 
c  Pressure     0.36441E-04     133   0.92785E-02   0.25704E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.50597E-08   0.16650E-08 0.10070E+00 
c  r22          0.10851E-01      13   0.50748E-08   0.18267E-08 0.10189E+00 
c  r33          0.21858E-01      15   0.55858E-08   0.12595E-07 0.12865E+00 
c  r12          0.93853E-03      18   0.62701E-08   0.30195E-09 0.61048E+00 
c  r13          0.46673E-02      19   0.64457E-08   0.14964E-08 0.20102E+00 
c  r23          0.39973E-02      18   0.69481E-08   0.12890E-08 0.20095E+00 
c  epsilon      0.10970E+02      11   0.33073E-08   0.98885E-02 0.16659E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.84662E-02 0.43416E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61353       0.0052556       0.0015073
v  Velocity[Y]            -0.57347         0.54444       0.0030802       0.0008733
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.399          360.07          87.655          169.88
v  r11                   0.0010591        0.081905        0.013072        0.018285
v  r22                   0.0011109        0.082622        0.013352        0.018645
v  r33                   0.0016346          0.1743        0.027246        0.037204
v  r12                   -0.010657        0.013579     -0.00023378     -0.00030929
v  r13                   -0.045556         0.05279      9.3018e-05       0.0010137
v  r23                   -0.046706        0.051256      3.0291e-05       0.0005745
v  epsilon                0.068835          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9933e-05       0.0099173      0.00092469       0.0017426
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017855           5.278         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878          0.7135         0.85283


 TIME FOR THE TIME STEP            10353:        0.86508E+02

===============================================================


 INSTANT    0.103540000E-01   TIME STEP NUMBER           10354
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140388210E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.325280353E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934913E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.165676215E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.327007030E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.102152102E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81276E-03   0.45159E-02 0.19901E+01 
c  Velocity[X]                                      0.13859E-03 
c  Velocity[Y]                                      0.12844E-03 
c  Velocity[Z]                                      0.42488E-02 
c  Pressure     0.36259E-04     131   0.92250E-02   0.25576E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.50062E-08   0.16430E-08 0.99757E-01 
c  r22          0.10851E-01      13   0.50682E-08   0.18238E-08 0.10133E+00 
c  r33          0.21858E-01      15   0.65788E-08   0.12472E-07 0.12731E+00 
c  r12          0.93853E-03      18   0.69838E-08   0.29991E-09 0.60794E+00 
c  r13          0.46673E-02      19   0.63184E-08   0.14843E-08 0.19932E+00 
c  r23          0.39973E-02      18   0.66149E-08   0.12817E-08 0.19970E+00 
c  epsilon      0.10970E+02      11   0.32790E-08   0.97943E-02 0.16528E+00 
c  TempC        0.25716E+06      16   0.15155E-04   0.83545E-02 0.43098E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61351       0.0052556       0.0015073
v  Velocity[Y]            -0.57339         0.54414       0.0030801       0.0008733
v  Velocity[Z]              1.5651          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4374          4.3406          4.3632
v  Pressure                -36.473          360.02          87.655          169.85
v  r11                   0.0010591        0.081907        0.013072        0.018285
v  r22                   0.0011109        0.082623        0.013352        0.018645
v  r33                   0.0016346         0.17433        0.027246        0.037204
v  r12                   -0.010657        0.013576     -0.00023378     -0.00030929
v  r13                   -0.045558        0.052791      9.3018e-05       0.0010137
v  r23                   -0.046706         0.05125      3.0291e-05       0.0005745
v  epsilon                0.068836          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099173      0.00092469       0.0017426
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017855           5.278         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71349         0.85283


 TIME FOR THE TIME STEP            10354:        0.89240E+02

===============================================================


 INSTANT    0.103550000E-01   TIME STEP NUMBER           10355
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.357088018E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.224331835E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.398296075E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.242802671E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.152940101E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81194E-03   0.45472E-02 0.19977E+01 
c  Velocity[X]                                      0.13880E-03 
c  Velocity[Y]                                      0.12936E-03 
c  Velocity[Z]                                      0.42791E-02 
c  Pressure     0.36535E-04     131   0.92990E-02   0.25771E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55040E-08   0.16771E-08 0.10066E+00 
c  r22          0.10851E-01      13   0.49885E-08   0.18561E-08 0.10217E+00 
c  r33          0.21858E-01      15   0.58519E-08   0.12815E-07 0.12891E+00 
c  r12          0.93853E-03      18   0.62457E-08   0.30109E-09 0.60661E+00 
c  r13          0.46673E-02      19   0.63990E-08   0.15068E-08 0.20095E+00 
c  r23          0.39973E-02      18   0.67933E-08   0.13017E-08 0.20061E+00 
c  epsilon      0.10970E+02      11   0.32753E-08   0.10104E-01 0.16690E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.84003E-02 0.43231E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61352       0.0052556       0.0015073
v  Velocity[Y]            -0.57361         0.54418       0.0030802      0.00087329
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.392          360.09          87.697          169.91
v  r11                   0.0010591        0.081912        0.013072        0.018285
v  r22                   0.0011109        0.082622        0.013352        0.018645
v  r33                   0.0016346         0.17432        0.027246        0.037204
v  r12                   -0.010655        0.013572     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052788      9.3019e-05       0.0010137
v  r23                   -0.046706        0.051247      3.0292e-05       0.0005745
v  epsilon                0.068837          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099174      0.00092469       0.0017426
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2777         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777          0.7135         0.85283


 TIME FOR THE TIME STEP            10355:        0.89147E+02

===============================================================


 INSTANT    0.103560000E-01   TIME STEP NUMBER           10356
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.128265173E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108285782E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249178181E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.635334818E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.112535334E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81273E-03   0.44847E-02 0.19869E+01 
c  Velocity[X]                                      0.13854E-03 
c  Velocity[Y]                                      0.12940E-03 
c  Velocity[Z]                                      0.42167E-02 
c  Pressure     0.36674E-04     131   0.93419E-02   0.25869E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53801E-08   0.16954E-08 0.10143E+00 
c  r22          0.10851E-01      13   0.47780E-08   0.18500E-08 0.10204E+00 
c  r33          0.21858E-01      14   0.70747E-08   0.12884E-07 0.12922E+00 
c  r12          0.93854E-03      18   0.54814E-08   0.30295E-09 0.61162E+00 
c  r13          0.46673E-02      19   0.54726E-08   0.15281E-08 0.20101E+00 
c  r23          0.39973E-02      18   0.64708E-08   0.13239E-08 0.20290E+00 
c  epsilon      0.10970E+02      11   0.34381E-08   0.10638E-01 0.17609E+00 
c  TempC        0.25716E+06      16   0.15171E-04   0.84521E-02 0.43397E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61352       0.0052556       0.0015073
v  Velocity[Y]            -0.57359         0.54438       0.0030803      0.00087335
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.453             360          87.656          169.85
v  r11                   0.0010591        0.081935        0.013072        0.018285
v  r22                   0.0011109        0.082622        0.013352        0.018645
v  r33                   0.0016346         0.17428        0.027246        0.037204
v  r12                   -0.010655        0.013572     -0.00023379     -0.00030929
v  r13                   -0.045554        0.052789       9.302e-05       0.0010137
v  r23                   -0.046707        0.051272      3.0292e-05       0.0005745
v  epsilon                0.068838          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099174      0.00092469       0.0017426
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2776         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776          0.7135         0.85283


 TIME FOR THE TIME STEP            10356:        0.80508E+02

===============================================================


 INSTANT    0.103570000E-01   TIME STEP NUMBER           10357
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.196728800E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.495089417E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.412117567E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.426492034E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.405650274E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81271E-03   0.45239E-02 0.19886E+01 
c  Velocity[X]                                      0.13821E-03 
c  Velocity[Y]                                      0.12758E-03 
c  Velocity[Z]                                      0.42581E-02 
c  Pressure     0.35978E-04     131   0.91598E-02   0.25378E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55858E-08   0.16823E-08 0.10074E+00 
c  r22          0.10851E-01      13   0.49154E-08   0.18488E-08 0.10187E+00 
c  r33          0.21858E-01      15   0.55090E-08   0.12806E-07 0.12843E+00 
c  r12          0.93854E-03      18   0.57565E-08   0.30614E-09 0.61142E+00 
c  r13          0.46673E-02      19   0.60877E-08   0.14892E-08 0.19906E+00 
c  r23          0.39973E-02      19   0.51846E-08   0.13056E-08 0.20053E+00 
c  epsilon      0.10970E+02      11   0.35819E-08   0.10113E-01 0.16761E+00 
c  TempC        0.25716E+06      16   0.15099E-04   0.84260E-02 0.43317E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61353       0.0052556       0.0015073
v  Velocity[Y]            -0.57352         0.54449       0.0030803      0.00087335
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.397          360.01          87.635          169.84
v  r11                   0.0010591        0.081958        0.013072        0.018285
v  r22                   0.0011109        0.082618        0.013352        0.018645
v  r33                   0.0016346          0.1743        0.027246        0.037204
v  r12                   -0.010658        0.013572     -0.00023379     -0.00030929
v  r13                   -0.045558         0.05279       9.302e-05       0.0010137
v  r23                   -0.046708        0.051263      3.0292e-05       0.0005745
v  epsilon                 0.06884          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099174      0.00092469       0.0017426
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2769         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769          0.7135         0.85283


 TIME FOR THE TIME STEP            10357:        0.76003E+02

===============================================================


 INSTANT    0.103580000E-01   TIME STEP NUMBER           10358
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.539550179E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.220746877E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.210009544E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.342925356E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.824603442E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81194E-03   0.45377E-02 0.19954E+01 
c  Velocity[X]                                      0.13781E-03 
c  Velocity[Y]                                      0.13002E-03 
c  Velocity[Z]                                      0.42698E-02 
c  Pressure     0.36985E-04     133   0.94119E-02   0.26089E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59151E-08   0.16422E-08 0.10042E+00 
c  r22          0.10851E-01      13   0.49527E-08   0.18206E-08 0.10177E+00 
c  r33          0.21858E-01      15   0.52218E-08   0.12446E-07 0.12787E+00 
c  r12          0.93854E-03      18   0.57664E-08   0.29561E-09 0.60623E+00 
c  r13          0.46673E-02      19   0.54063E-08   0.14819E-08 0.19982E+00 
c  r23          0.39973E-02      19   0.52960E-08   0.12738E-08 0.19973E+00 
c  epsilon      0.10970E+02      11   0.34710E-08   0.93903E-02 0.16204E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.84154E-02 0.43276E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61352       0.0052556       0.0015073
v  Velocity[Y]             -0.5734         0.54427       0.0030803      0.00087333
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.456          359.99          87.649          169.84
v  r11                   0.0010591        0.081975        0.013072        0.018285
v  r22                   0.0011109        0.082619        0.013352        0.018645
v  r33                   0.0016347         0.17432        0.027246        0.037204
v  r12                   -0.010659        0.013579     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052792      9.3021e-05       0.0010137
v  r23                   -0.046708        0.051239      3.0292e-05       0.0005745
v  epsilon                0.068841          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099175      0.00092469       0.0017426
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2771         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71349         0.85283


 TIME FOR THE TIME STEP            10358:        0.82960E+02

===============================================================


 INSTANT    0.103590000E-01   TIME STEP NUMBER           10359
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.698319178E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.132854983E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.162814778E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181098232E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161426928E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81195E-03   0.45541E-02 0.19979E+01 
c  Velocity[X]                                      0.13915E-03 
c  Velocity[Y]                                      0.12892E-03 
c  Velocity[Z]                                      0.42860E-02 
c  Pressure     0.36336E-04     131   0.92542E-02   0.25631E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54457E-08   0.16119E-08 0.99053E-01 
c  r22          0.10851E-01      13   0.47991E-08   0.18063E-08 0.10060E+00 
c  r33          0.21858E-01      15   0.59131E-08   0.12337E-07 0.12616E+00 
c  r12          0.93854E-03      17   0.69496E-08   0.29612E-09 0.60339E+00 
c  r13          0.46673E-02      19   0.73926E-08   0.14862E-08 0.19841E+00 
c  r23          0.39973E-02      18   0.70729E-08   0.12565E-08 0.19692E+00 
c  epsilon      0.10970E+02      11   0.34656E-08   0.97685E-02 0.16354E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.84643E-02 0.43386E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61355       0.0052557       0.0015074
v  Velocity[Y]            -0.57361         0.54434       0.0030803      0.00087338
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.391          360.11            87.7          169.92
v  r11                   0.0010591        0.081978        0.013072        0.018285
v  r22                   0.0011109        0.082621        0.013352        0.018645
v  r33                   0.0016347          0.1743        0.027246        0.037204
v  r12                   -0.010657        0.013576     -0.00023379     -0.00030929
v  r13                   -0.045555         0.05279      9.3023e-05       0.0010137
v  r23                   -0.046709        0.051229      3.0293e-05       0.0005745
v  epsilon                0.068842          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099175       0.0009247       0.0017426
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2767         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767          0.7135         0.85284


 TIME FOR THE TIME STEP            10359:        0.83606E+02

===============================================================


 INSTANT    0.103600000E-01   TIME STEP NUMBER           10360
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.771132982E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.371430797E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.628859550E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.665687258E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.392217473E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81336E-03   0.44900E-02 0.19844E+01 
c  Velocity[X]                                      0.13870E-03 
c  Velocity[Y]                                      0.12803E-03 
c  Velocity[Z]                                      0.42233E-02 
c  Pressure     0.36198E-04     132   0.92157E-02   0.25533E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53586E-08   0.16409E-08 0.99913E-01 
c  r22          0.10851E-01      13   0.49862E-08   0.18392E-08 0.10172E+00 
c  r33          0.21858E-01      14   0.68930E-08   0.12601E-07 0.12770E+00 
c  r12          0.93854E-03      18   0.53870E-08   0.29953E-09 0.60465E+00 
c  r13          0.46673E-02      19   0.59499E-08   0.14910E-08 0.19956E+00 
c  r23          0.39973E-02      19   0.55030E-08   0.12675E-08 0.19914E+00 
c  epsilon      0.10970E+02      11   0.33075E-08   0.10066E-01 0.16727E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.83746E-02 0.43197E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61351       0.0052556       0.0015073
v  Velocity[Y]            -0.57359         0.54404       0.0030802      0.00087333
v  Velocity[Z]              1.5652          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4374          4.3406          4.3632
v  Pressure                -36.446             360          87.634          169.83
v  r11                   0.0010591        0.081993        0.013072        0.018285
v  r22                   0.0011109        0.082621        0.013352        0.018645
v  r33                   0.0016347         0.17427        0.027246        0.037204
v  r12                   -0.010664        0.013579     -0.00023379     -0.00030929
v  r13                   -0.045557        0.052789      9.3024e-05       0.0010137
v  r23                    -0.04671        0.051247      3.0294e-05       0.0005745
v  epsilon                0.068843          271.19          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099177       0.0009247       0.0017426
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2766         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766          0.7135         0.85284


 TIME FOR THE TIME STEP            10360:        0.81328E+02

===============================================================


 INSTANT    0.103610000E-01   TIME STEP NUMBER           10361
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.458869357E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.287246263E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.308666850E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.256958860E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.224285816E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81131E-03   0.45412E-02 0.19946E+01 
c  Velocity[X]                                      0.13874E-03 
c  Velocity[Y]                                      0.12988E-03 
c  Velocity[Z]                                      0.42726E-02 
c  Pressure     0.36607E-04     133   0.93202E-02   0.25822E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55874E-08   0.16485E-08 0.99993E-01 
c  r22          0.10851E-01      13   0.52270E-08   0.18291E-08 0.10170E+00 
c  r33          0.21858E-01      15   0.51628E-08   0.12577E-07 0.12794E+00 
c  r12          0.93854E-03      18   0.55965E-08   0.29760E-09 0.60559E+00 
c  r13          0.46673E-02      19   0.56083E-08   0.15063E-08 0.20039E+00 
c  r23          0.39973E-02      19   0.52863E-08   0.12943E-08 0.19987E+00 
c  epsilon      0.10970E+02      11   0.33285E-08   0.99678E-02 0.16618E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.83956E-02 0.43248E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61354       0.0052556       0.0015073
v  Velocity[Y]            -0.57375         0.54411       0.0030803       0.0008734
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.403           360.1          87.687          169.91
v  r11                   0.0010591        0.081998        0.013072        0.018285
v  r22                   0.0011109        0.082623        0.013352        0.018645
v  r33                   0.0016347         0.17428        0.027246        0.037204
v  r12                   -0.010665        0.013576     -0.00023379     -0.00030929
v  r13                   -0.045556        0.052788      9.3024e-05       0.0010137
v  r23                    -0.04671        0.051245      3.0295e-05       0.0005745
v  epsilon                0.068845          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099178       0.0009247       0.0017426
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2764         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8764          0.7135         0.85283


 TIME FOR THE TIME STEP            10361:        0.76468E+02

===============================================================


 INSTANT    0.103620000E-01   TIME STEP NUMBER           10362
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.160818087E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.429891789E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.108892952E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169270661E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.320465263E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81225E-03   0.45725E-02 0.20008E+01 
c  Velocity[X]                                      0.13850E-03 
c  Velocity[Y]                                      0.12946E-03 
c  Velocity[Z]                                      0.43046E-02 
c  Pressure     0.36556E-04     131   0.93004E-02   0.25785E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51842E-08   0.16631E-08 0.10047E+00 
c  r22          0.10851E-01      13   0.49693E-08   0.18088E-08 0.10134E+00 
c  r33          0.21858E-01      15   0.55202E-08   0.12621E-07 0.12830E+00 
c  r12          0.93854E-03      18   0.53479E-08   0.29931E-09 0.60764E+00 
c  r13          0.46673E-02      19   0.65078E-08   0.14850E-08 0.19938E+00 
c  r23          0.39973E-02      19   0.56828E-08   0.13125E-08 0.20163E+00 
c  epsilon      0.10970E+02      11   0.34253E-08   0.10244E-01 0.17095E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84412E-02 0.43330E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61354       0.0052556       0.0015073
v  Velocity[Y]            -0.57367         0.54429       0.0030803      0.00087338
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.452          359.99          87.646          169.83
v  r11                   0.0010591        0.082005        0.013072        0.018285
v  r22                   0.0011109        0.082624        0.013352        0.018645
v  r33                   0.0016347         0.17431        0.027246        0.037204
v  r12                   -0.010669        0.013584     -0.00023379     -0.00030929
v  r13                   -0.045555         0.05279      9.3025e-05       0.0010137
v  r23                   -0.046711        0.051244      3.0295e-05       0.0005745
v  epsilon                0.068846          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9929e-05       0.0099178       0.0009247       0.0017426
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2759         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8759          0.7135         0.85283


 TIME FOR THE TIME STEP            10362:        0.77643E+02

===============================================================


 INSTANT    0.103630000E-01   TIME STEP NUMBER           10363
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.345507456E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.223880702E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.822200187E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.230574513E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.210875322E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81301E-03   0.44989E-02 0.19876E+01 
c  Velocity[X]                                      0.13806E-03 
c  Velocity[Y]                                      0.12807E-03 
c  Velocity[Z]                                      0.42328E-02 
c  Pressure     0.36397E-04     133   0.92620E-02   0.25674E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51000E-08   0.16268E-08 0.10021E+00 
c  r22          0.10851E-01      13   0.49808E-08   0.18203E-08 0.10167E+00 
c  r33          0.21858E-01      15   0.53713E-08   0.12409E-07 0.12793E+00 
c  r12          0.93854E-03      18   0.57138E-08   0.29223E-09 0.60212E+00 
c  r13          0.46673E-02      19   0.60864E-08   0.14867E-08 0.20036E+00 
c  r23          0.39973E-02      19   0.53244E-08   0.12566E-08 0.19966E+00 
c  epsilon      0.10970E+02      11   0.34181E-08   0.96851E-02 0.16371E+00 
c  TempC        0.25716E+06      16   0.15110E-04   0.84104E-02 0.43277E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61353       0.0052556       0.0015073
v  Velocity[Y]            -0.57363         0.54398       0.0030804      0.00087342
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.411          360.06          87.656          169.88
v  r11                   0.0010591        0.082005        0.013072        0.018285
v  r22                   0.0011109        0.082621        0.013352        0.018645
v  r33                   0.0016347         0.17434        0.027246        0.037204
v  r12                   -0.010666        0.013585     -0.00023379     -0.00030929
v  r13                   -0.045557        0.052789      9.3026e-05       0.0010137
v  r23                   -0.046711        0.051265      3.0296e-05      0.00057451
v  epsilon                0.068847          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9929e-05       0.0099178       0.0009247       0.0017426
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2758         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8758          0.7135         0.85283


 TIME FOR THE TIME STEP            10363:        0.78484E+02

===============================================================


 INSTANT    0.103640000E-01   TIME STEP NUMBER           10364
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.617191107E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.343584794E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.730178453E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.165127431E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.499631585E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81239E-03   0.45032E-02 0.19878E+01 
c  Velocity[X]                                      0.13859E-03 
c  Velocity[Y]                                      0.12898E-03 
c  Velocity[Z]                                      0.42356E-02 
c  Pressure     0.35932E-04     132   0.91422E-02   0.25345E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51354E-08   0.16346E-08 0.99748E-01 
c  r22          0.10851E-01      13   0.48081E-08   0.18566E-08 0.10220E+00 
c  r33          0.21858E-01      15   0.56357E-08   0.12680E-07 0.12813E+00 
c  r12          0.93854E-03      18   0.52846E-08   0.30062E-09 0.60966E+00 
c  r13          0.46673E-02      20   0.59151E-08   0.15075E-08 0.20044E+00 
c  r23          0.39973E-02      19   0.59104E-08   0.12972E-08 0.20071E+00 
c  epsilon      0.10970E+02      11   0.35478E-08   0.10181E-01 0.16683E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.84280E-02 0.43283E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61351       0.0052556       0.0015073
v  Velocity[Y]            -0.57345         0.54389       0.0030804      0.00087339
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.453          360.02          87.663          169.86
v  r11                   0.0010591        0.082017        0.013072        0.018285
v  r22                   0.0011109        0.082622        0.013352        0.018645
v  r33                   0.0016347         0.17433        0.027246        0.037204
v  r12                   -0.010662        0.013584     -0.00023379     -0.00030929
v  r13                   -0.045554        0.052792      9.3027e-05       0.0010137
v  r23                   -0.046711        0.051255      3.0297e-05      0.00057451
v  epsilon                0.068848          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05        0.009918       0.0009247       0.0017426
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2759         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8759          0.7135         0.85283


 TIME FOR THE TIME STEP            10364:        0.81065E+02

===============================================================


 INSTANT    0.103650000E-01   TIME STEP NUMBER           10365
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.196542549E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171928027E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.142982589E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.226345010E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.101060864E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81163E-03   0.45293E-02 0.19936E+01 
c  Velocity[X]                                      0.13993E-03 
c  Velocity[Y]                                      0.12884E-03 
c  Velocity[Z]                                      0.42605E-02 
c  Pressure     0.36350E-04     132   0.92511E-02   0.25640E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55222E-08   0.16218E-08 0.99644E-01 
c  r22          0.10851E-01      13   0.49813E-08   0.18205E-08 0.10154E+00 
c  r33          0.21858E-01      14   0.70040E-08   0.12395E-07 0.12756E+00 
c  r12          0.93854E-03      18   0.61601E-08   0.29841E-09 0.60559E+00 
c  r13          0.46673E-02      20   0.60320E-08   0.14878E-08 0.19910E+00 
c  r23          0.39973E-02      19   0.60793E-08   0.12645E-08 0.19926E+00 
c  epsilon      0.10970E+02      11   0.34537E-08   0.96958E-02 0.16347E+00 
c  TempC        0.25716E+06      16   0.15127E-04   0.84553E-02 0.43410E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387          0.6135       0.0052555       0.0015073
v  Velocity[Y]            -0.57348         0.54403       0.0030804       0.0008734
v  Velocity[Z]              1.5652          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.403          360.06          87.671          169.88
v  r11                   0.0010591        0.082022        0.013072        0.018285
v  r22                   0.0011109        0.082624        0.013352        0.018645
v  r33                   0.0016347         0.17429        0.027246        0.037204
v  r12                   -0.010658        0.013578     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052792      9.3028e-05       0.0010137
v  r23                   -0.046711        0.051247      3.0298e-05      0.00057451
v  epsilon                0.068849          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9929e-05        0.009918       0.0009247       0.0017426
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2762         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8762          0.7135         0.85283


 TIME FOR THE TIME STEP            10365:        0.82360E+02

===============================================================


 INSTANT    0.103660000E-01   TIME STEP NUMBER           10366
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.393262304E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.324311322E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.220230116E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181624528E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283701754E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81268E-03   0.45033E-02 0.19861E+01 
c  Velocity[X]                                      0.13762E-03 
c  Velocity[Y]                                      0.12829E-03 
c  Velocity[Z]                                      0.42374E-02 
c  Pressure     0.36255E-04     132   0.92291E-02   0.25573E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55753E-08   0.16788E-08 0.10068E+00 
c  r22          0.10851E-01      13   0.52874E-08   0.18785E-08 0.10270E+00 
c  r33          0.21858E-01      15   0.60050E-08   0.12844E-07 0.12890E+00 
c  r12          0.93854E-03      18   0.69490E-08   0.30866E-09 0.61125E+00 
c  r13          0.46673E-02      19   0.71796E-08   0.15223E-08 0.20132E+00 
c  r23          0.39973E-02      19   0.59355E-08   0.13071E-08 0.20164E+00 
c  epsilon      0.10970E+02      11   0.35267E-08   0.10314E-01 0.16924E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.83519E-02 0.43090E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61349       0.0052555       0.0015073
v  Velocity[Y]             -0.5734         0.54415       0.0030804      0.00087338
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                 -36.46          360.06          87.675          169.88
v  r11                   0.0010591        0.082015        0.013072        0.018285
v  r22                    0.001111        0.082627        0.013352        0.018645
v  r33                   0.0016347          0.1743        0.027246        0.037204
v  r12                   -0.010658        0.013584     -0.00023379     -0.00030929
v  r13                   -0.045558        0.052794      9.3028e-05       0.0010137
v  r23                   -0.046711        0.051237      3.0298e-05      0.00057451
v  epsilon                0.068851          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099179       0.0009247       0.0017426
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2765         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765          0.7135         0.85283


 TIME FOR THE TIME STEP            10366:        0.80808E+02

===============================================================


 INSTANT    0.103670000E-01   TIME STEP NUMBER           10367
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.128659847E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.549905528E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199737655E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.432779749E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.378759019E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      40   0.81235E-03   0.45481E-02 0.19979E+01 
c  Velocity[X]                                      0.13927E-03 
c  Velocity[Y]                                      0.12967E-03 
c  Velocity[Z]                                      0.42791E-02 
c  Pressure     0.36401E-04     132   0.92667E-02   0.25676E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55099E-08   0.16443E-08 0.99950E-01 
c  r22          0.10851E-01      13   0.50987E-08   0.19173E-08 0.10371E+00 
c  r33          0.21858E-01      15   0.56937E-08   0.12881E-07 0.12933E+00 
c  r12          0.93854E-03      18   0.58762E-08   0.31078E-09 0.61255E+00 
c  r13          0.46673E-02      19   0.62558E-08   0.15480E-08 0.20297E+00 
c  r23          0.39973E-02      19   0.60425E-08   0.12906E-08 0.20084E+00 
c  epsilon      0.10970E+02      11   0.33975E-08   0.10154E-01 0.16642E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.84039E-02 0.43266E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63371         0.61352       0.0052557       0.0015073
v  Velocity[Y]            -0.57351         0.54431       0.0030805      0.00087341
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.385          359.97          87.608          169.81
v  r11                   0.0010591        0.082007        0.013072        0.018285
v  r22                    0.001111        0.082627        0.013352        0.018645
v  r33                   0.0016347         0.17433        0.027246        0.037204
v  r12                   -0.010658        0.013581     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052791      9.3029e-05       0.0010137
v  r23                   -0.046711        0.051273      3.0299e-05      0.00057451
v  epsilon                0.068852          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9929e-05       0.0099174      0.00092471       0.0017426
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2777         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777          0.7135         0.85283


 TIME FOR THE TIME STEP            10367:        0.85529E+02

===============================================================


 INSTANT    0.103680000E-01   TIME STEP NUMBER           10368
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.298325695E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.318117777E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934908E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.535175413E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.243857275E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208092648E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      44   0.81284E-03   0.45243E-02 0.19931E+01 
c  Velocity[X]                                      0.13877E-03 
c  Velocity[Y]                                      0.12936E-03 
c  Velocity[Z]                                      0.42562E-02 
c  Pressure     0.36515E-04     133   0.92928E-02   0.25757E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58362E-08   0.16688E-08 0.10064E+00 
c  r22          0.10851E-01      13   0.49028E-08   0.18403E-08 0.10216E+00 
c  r33          0.21858E-01      15   0.66523E-08   0.12759E-07 0.12890E+00 
c  r12          0.93854E-03      18   0.62913E-08   0.30396E-09 0.61063E+00 
c  r13          0.46673E-02      19   0.71222E-08   0.15316E-08 0.20226E+00 
c  r23          0.39973E-02      19   0.62725E-08   0.13210E-08 0.20243E+00 
c  epsilon      0.10970E+02      11   0.34704E-08   0.10384E-01 0.17249E+00 
c  TempC        0.25716E+06      16   0.15155E-04   0.84618E-02 0.43392E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61352       0.0052557       0.0015073
v  Velocity[Y]            -0.57348         0.54427       0.0030805      0.00087342
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.448          359.99          87.654          169.84
v  r11                   0.0010591        0.081992        0.013072        0.018285
v  r22                    0.001111        0.082626        0.013352        0.018645
v  r33                   0.0016347          0.1743        0.027246        0.037204
v  r12                   -0.010659         0.01359     -0.00023379     -0.00030929
v  r13                   -0.045554        0.052791       9.303e-05       0.0010137
v  r23                   -0.046711        0.051274        3.03e-05      0.00057451
v  epsilon                0.068853          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099173      0.00092471       0.0017426
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017852           5.279         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879          0.7135         0.85283


 TIME FOR THE TIME STEP            10368:        0.82240E+02

===============================================================


 INSTANT    0.103690000E-01   TIME STEP NUMBER           10369
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141287055E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.210762008E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.144091426E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.817801309E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.146099791E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81281E-03   0.45182E-02 0.19892E+01 
c  Velocity[X]                                      0.13749E-03 
c  Velocity[Y]                                      0.12803E-03 
c  Velocity[Z]                                      0.42527E-02 
c  Pressure     0.36275E-04     133   0.92312E-02   0.25588E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58157E-08   0.16477E-08 0.99941E-01 
c  r22          0.10851E-01      13   0.49416E-08   0.18150E-08 0.10161E+00 
c  r33          0.21858E-01      15   0.61218E-08   0.12456E-07 0.12736E+00 
c  r12          0.93854E-03      18   0.65236E-08   0.30608E-09 0.60972E+00 
c  r13          0.46673E-02      20   0.58405E-08   0.14914E-08 0.19960E+00 
c  r23          0.39974E-02      19   0.65876E-08   0.12916E-08 0.19994E+00 
c  epsilon      0.10970E+02      11   0.34843E-08   0.96158E-02 0.16320E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.83519E-02 0.43112E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61351       0.0052557       0.0015074
v  Velocity[Y]            -0.57356         0.54417       0.0030804      0.00087338
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.424          360.03          87.641          169.85
v  r11                   0.0010591        0.081984        0.013072        0.018285
v  r22                    0.001111        0.082622        0.013352        0.018645
v  r33                   0.0016348         0.17427        0.027246        0.037204
v  r12                   -0.010659        0.013589     -0.00023379     -0.00030929
v  r13                   -0.045558        0.052792       9.303e-05       0.0010137
v  r23                   -0.046711        0.051269        3.03e-05      0.00057451
v  epsilon                0.068854          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099173      0.00092471       0.0017426
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2793         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8793          0.7135         0.85283


 TIME FOR THE TIME STEP            10369:        0.79871E+02

===============================================================


 INSTANT    0.103700000E-01   TIME STEP NUMBER           10370
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.244093052E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.376171167E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934906E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227093791E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.661868529E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.198766659E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81287E-03   0.45307E-02 0.19927E+01 
c  Velocity[X]                                      0.13865E-03 
c  Velocity[Y]                                      0.12921E-03 
c  Velocity[Z]                                      0.42628E-02 
c  Pressure     0.36637E-04     132   0.93212E-02   0.25843E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.62376E-08   0.16925E-08 0.10180E+00 
c  r22          0.10851E-01      13   0.51033E-08   0.18747E-08 0.10289E+00 
c  r33          0.21858E-01      15   0.57441E-08   0.12864E-07 0.12992E+00 
c  r12          0.93854E-03      18   0.61568E-08   0.31195E-09 0.62096E+00 
c  r13          0.46673E-02      20   0.64457E-08   0.15156E-08 0.20168E+00 
c  r23          0.39974E-02      19   0.55760E-08   0.13231E-08 0.20427E+00 
c  epsilon      0.10970E+02      11   0.36102E-08   0.97664E-02 0.16385E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.84236E-02 0.43308E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61354       0.0052556       0.0015073
v  Velocity[Y]            -0.57352         0.54423       0.0030805       0.0008734
v  Velocity[Z]              1.5652          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.441             360          87.645          169.83
v  r11                   0.0010592        0.081979        0.013072        0.018285
v  r22                    0.001111        0.082624        0.013352        0.018645
v  r33                   0.0016348         0.17429        0.027246        0.037204
v  r12                   -0.010664        0.013586     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052794      9.3031e-05       0.0010137
v  r23                   -0.046711        0.051269      3.0301e-05      0.00057451
v  epsilon                0.068855          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05       0.0099175      0.00092471       0.0017426
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2794         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8794         0.71349         0.85283


 TIME FOR THE TIME STEP            10370:        0.81450E+02

===============================================================


 INSTANT    0.103710000E-01   TIME STEP NUMBER           10371
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239028160E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.202573019E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.146815178E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.147110370E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.369278235E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81171E-03   0.45734E-02 0.20021E+01 
c  Velocity[X]                                      0.14008E-03 
c  Velocity[Y]                                      0.12896E-03 
c  Velocity[Z]                                      0.43043E-02 
c  Pressure     0.36710E-04     132   0.93511E-02   0.25895E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.64522E-08   0.17071E-08 0.10195E+00 
c  r22          0.10851E-01      13   0.47495E-08   0.18587E-08 0.10267E+00 
c  r33          0.21858E-01      15   0.52617E-08   0.12855E-07 0.12979E+00 
c  r12          0.93854E-03      18   0.56786E-08   0.30947E-09 0.61655E+00 
c  r13          0.46673E-02      19   0.66901E-08   0.15089E-08 0.20124E+00 
c  r23          0.39974E-02      19   0.54942E-08   0.13073E-08 0.20283E+00 
c  epsilon      0.10970E+02      11   0.34499E-08   0.97212E-02 0.16423E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.84655E-02 0.43411E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61355       0.0052557       0.0015073
v  Velocity[Y]            -0.57343         0.54439       0.0030805      0.00087346
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.403          360.07          87.665          169.89
v  r11                   0.0010592        0.081977        0.013072        0.018285
v  r22                    0.001111        0.082625        0.013352        0.018645
v  r33                   0.0016348         0.17431        0.027246        0.037204
v  r12                   -0.010661        0.013585     -0.00023379     -0.00030929
v  r13                   -0.045554        0.052791      9.3033e-05       0.0010137
v  r23                   -0.046711        0.051296      3.0302e-05      0.00057451
v  epsilon                0.068857          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099176      0.00092471       0.0017426
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2793         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8793          0.7135         0.85283


 TIME FOR THE TIME STEP            10371:        0.80456E+02

===============================================================


 INSTANT    0.103720000E-01   TIME STEP NUMBER           10372
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115508290E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.759959928E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.154106411E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.673716426E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.177955638E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81394E-03   0.45097E-02 0.19882E+01 
c  Velocity[X]                                      0.13734E-03 
c  Velocity[Y]                                      0.12854E-03 
c  Velocity[Z]                                      0.42439E-02 
c  Pressure     0.36034E-04     133   0.91751E-02   0.25418E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.64267E-08   0.16499E-08 0.99812E-01 
c  r22          0.10851E-01      13   0.50857E-08   0.18570E-08 0.10230E+00 
c  r33          0.21859E-01      15   0.55274E-08   0.12669E-07 0.12823E+00 
c  r12          0.93854E-03      18   0.59313E-08   0.29618E-09 0.60705E+00 
c  r13          0.46673E-02      19   0.63712E-08   0.15048E-08 0.20116E+00 
c  r23          0.39974E-02      19   0.60544E-08   0.12678E-08 0.19867E+00 
c  epsilon      0.10970E+02      11   0.34538E-08   0.10030E-01 0.16688E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.84060E-02 0.43277E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61352       0.0052557       0.0015073
v  Velocity[Y]            -0.57341         0.54421       0.0030805      0.00087343
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.485          360.02          87.638          169.85
v  r11                   0.0010592        0.081979        0.013072        0.018285
v  r22                    0.001111        0.082624        0.013352        0.018645
v  r33                   0.0016348         0.17434        0.027247        0.037204
v  r12                   -0.010662         0.01358     -0.00023379     -0.00030929
v  r13                   -0.045557         0.05279      9.3033e-05       0.0010137
v  r23                   -0.046711        0.051293      3.0302e-05      0.00057451
v  epsilon                0.068858          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05       0.0099177      0.00092471       0.0017426
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2788         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788          0.7135         0.85283


 TIME FOR THE TIME STEP            10372:        0.83895E+02

===============================================================


 INSTANT    0.103730000E-01   TIME STEP NUMBER           10373
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.156990063E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.261688014E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283679073E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.957781587E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.331209030E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81167E-03   0.45461E-02 0.19927E+01 
c  Velocity[X]                                      0.13909E-03 
c  Velocity[Y]                                      0.12873E-03 
c  Velocity[Z]                                      0.42783E-02 
c  Pressure     0.36253E-04     133   0.92340E-02   0.25572E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60218E-08   0.16981E-08 0.10124E+00 
c  r22          0.10851E-01      13   0.51114E-08   0.18522E-08 0.10219E+00 
c  r33          0.21859E-01      15   0.65223E-08   0.12811E-07 0.12883E+00 
c  r12          0.93854E-03      18   0.53798E-08   0.29832E-09 0.60696E+00 
c  r13          0.46673E-02      20   0.60099E-08   0.15080E-08 0.20027E+00 
c  r23          0.39974E-02      19   0.68013E-08   0.13180E-08 0.20186E+00 
c  epsilon      0.10970E+02      11   0.35524E-08   0.98470E-02 0.16514E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.84291E-02 0.43328E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61358       0.0052557       0.0015074
v  Velocity[Y]            -0.57352         0.54433       0.0030805      0.00087343
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.428          359.98          87.619          169.81
v  r11                   0.0010592        0.081986        0.013072        0.018285
v  r22                    0.001111        0.082623        0.013352        0.018645
v  r33                   0.0016348         0.17431        0.027247        0.037204
v  r12                   -0.010661        0.013581     -0.00023379     -0.00030929
v  r13                   -0.045556        0.052789      9.3034e-05       0.0010137
v  r23                    -0.04671        0.051279      3.0303e-05      0.00057451
v  epsilon                0.068859          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099177      0.00092471       0.0017426
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2784         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784          0.7135         0.85283


 TIME FOR THE TIME STEP            10373:        0.87558E+02

===============================================================


 INSTANT    0.103740000E-01   TIME STEP NUMBER           10374
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122527763E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.234737524E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.700621014E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.250656559E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.332985945E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81187E-03   0.45588E-02 0.20001E+01 
c  Velocity[X]                                      0.13844E-03 
c  Velocity[Y]                                      0.12982E-03 
c  Velocity[Z]                                      0.42905E-02 
c  Pressure     0.36822E-04     133   0.93655E-02   0.25973E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52094E-08   0.16295E-08 0.99877E-01 
c  r22          0.10851E-01      13   0.50084E-08   0.18032E-08 0.10166E+00 
c  r33          0.21859E-01      16   0.59307E-08   0.12321E-07 0.12738E+00 
c  r12          0.93854E-03      18   0.51719E-08   0.29434E-09 0.60457E+00 
c  r13          0.46673E-02      20   0.62709E-08   0.14663E-08 0.19973E+00 
c  r23          0.39974E-02      19   0.59381E-08   0.12575E-08 0.19796E+00 
c  epsilon      0.10970E+02      11   0.35877E-08   0.94424E-02 0.16221E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.83981E-02 0.43194E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61356       0.0052557       0.0015074
v  Velocity[Y]            -0.57349         0.54451       0.0030804       0.0008734
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4374          4.3406          4.3632
v  Pressure                -36.476          360.03          87.664          169.86
v  r11                   0.0010592        0.081995        0.013072        0.018285
v  r22                    0.001111        0.082623        0.013352        0.018645
v  r33                   0.0016348         0.17428        0.027247        0.037204
v  r12                   -0.010658        0.013579     -0.00023379     -0.00030929
v  r13                   -0.045554        0.052792      9.3035e-05       0.0010137
v  r23                    -0.04671         0.05129      3.0304e-05      0.00057451
v  epsilon                 0.06886          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099176      0.00092471       0.0017426
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2778         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778          0.7135         0.85283


 TIME FOR THE TIME STEP            10374:        0.81944E+02

===============================================================


 INSTANT    0.103750000E-01   TIME STEP NUMBER           10375
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.251264402E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.979099573E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166649697E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.347093381E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.385346310E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81260E-03   0.45072E-02 0.19902E+01 
c  Velocity[X]                                      0.13807E-03 
c  Velocity[Y]                                      0.12899E-03 
c  Velocity[Z]                                      0.42401E-02 
c  Pressure     0.35938E-04     133   0.91471E-02   0.25349E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52841E-08   0.16743E-08 0.10062E+00 
c  r22          0.10851E-01      13   0.58681E-08   0.18692E-08 0.10236E+00 
c  r33          0.21859E-01      16   0.61802E-08   0.12804E-07 0.12850E+00 
c  r12          0.93854E-03      18   0.54074E-08   0.30565E-09 0.61001E+00 
c  r13          0.46673E-02      20   0.60811E-08   0.15091E-08 0.20011E+00 
c  r23          0.39974E-02      20   0.57872E-08   0.12966E-08 0.20007E+00 
c  epsilon      0.10970E+02      11   0.34879E-08   0.10598E-01 0.17451E+00 
c  TempC        0.25716E+06      16   0.15099E-04   0.84200E-02 0.43279E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379         0.61355       0.0052558       0.0015074
v  Velocity[Y]             -0.5736         0.54421       0.0030806      0.00087346
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.445          360.09          87.673           169.9
v  r11                   0.0010592        0.082003        0.013072        0.018285
v  r22                    0.001111        0.082618        0.013352        0.018645
v  r33                   0.0016348         0.17429        0.027247        0.037204
v  r12                   -0.010661        0.013578     -0.00023379     -0.00030929
v  r13                   -0.045556        0.052791      9.3036e-05       0.0010137
v  r23                   -0.046709         0.05127      3.0304e-05      0.00057451
v  epsilon                0.068861          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099174      0.00092471       0.0017426
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2773         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773          0.7135         0.85283


 TIME FOR THE TIME STEP            10375:        0.80905E+02

===============================================================


 INSTANT    0.103760000E-01   TIME STEP NUMBER           10376
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.741566056E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.293301054E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.359607240E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.109758352E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.236695092E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81268E-03   0.45081E-02 0.19892E+01 
c  Velocity[X]                                      0.13841E-03 
c  Velocity[Y]                                      0.12884E-03 
c  Velocity[Z]                                      0.42408E-02 
c  Pressure     0.36250E-04     133   0.92250E-02   0.25570E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52023E-08   0.16306E-08 0.99590E-01 
c  r22          0.10851E-01      13   0.58954E-08   0.18261E-08 0.10200E+00 
c  r33          0.21859E-01      15   0.73081E-08   0.12483E-07 0.12761E+00 
c  r12          0.93854E-03      18   0.57093E-08   0.29504E-09 0.60332E+00 
c  r13          0.46673E-02      19   0.67029E-08   0.14980E-08 0.19989E+00 
c  r23          0.39974E-02      19   0.71192E-08   0.12716E-08 0.19838E+00 
c  epsilon      0.10970E+02      11   0.34579E-08   0.99535E-02 0.16695E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.84193E-02 0.43300E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61356       0.0052558       0.0015074
v  Velocity[Y]            -0.57355         0.54426       0.0030805      0.00087346
v  Velocity[Z]              1.5652          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.505             360          87.646          169.84
v  r11                   0.0010592        0.081999        0.013072        0.018285
v  r22                    0.001111        0.082618        0.013352        0.018645
v  r33                   0.0016348         0.17431        0.027247        0.037204
v  r12                   -0.010657        0.013577     -0.00023379     -0.00030929
v  r13                   -0.045554         0.05279      9.3036e-05       0.0010137
v  r23                   -0.046709        0.051253      3.0305e-05      0.00057451
v  epsilon                0.068863          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05       0.0099174      0.00092472       0.0017426
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2773         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773          0.7135         0.85283


 TIME FOR THE TIME STEP            10376:        0.83193E+02

===============================================================


 INSTANT    0.103770000E-01   TIME STEP NUMBER           10377
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.219941776E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.986288290E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.866812436E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.293342349E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.135436601E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81156E-03   0.45236E-02 0.19914E+01 
c  Velocity[X]                                      0.13902E-03 
c  Velocity[Y]                                      0.12874E-03 
c  Velocity[Z]                                      0.42558E-02 
c  Pressure     0.36344E-04     131   0.92584E-02   0.25636E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51791E-08   0.16173E-08 0.99544E-01 
c  r22          0.10851E-01      13   0.53714E-08   0.17921E-08 0.10088E+00 
c  r33          0.21859E-01      16   0.59253E-08   0.12252E-07 0.12658E+00 
c  r12          0.93854E-03      18   0.50840E-08   0.29094E-09 0.60117E+00 
c  r13          0.46673E-02      19   0.74231E-08   0.14563E-08 0.19768E+00 
c  r23          0.39974E-02      19   0.68646E-08   0.12524E-08 0.19753E+00 
c  epsilon      0.10970E+02      11   0.34287E-08   0.95401E-02 0.16292E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.84591E-02 0.43414E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61355       0.0052558       0.0015074
v  Velocity[Y]            -0.57349          0.5444       0.0030806      0.00087344
v  Velocity[Z]              1.5655          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.447          359.99          87.621          169.82
v  r11                   0.0010592        0.081991        0.013072        0.018285
v  r22                    0.001111        0.082619        0.013352        0.018645
v  r33                   0.0016348         0.17429        0.027247        0.037204
v  r12                   -0.010652        0.013575     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052788      9.3037e-05       0.0010137
v  r23                   -0.046709        0.051268      3.0306e-05      0.00057451
v  epsilon                0.068864          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099174      0.00092472       0.0017426
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2778         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778          0.7135         0.85284


 TIME FOR THE TIME STEP            10377:        0.83484E+02

===============================================================


 INSTANT    0.103780000E-01   TIME STEP NUMBER           10378
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188696328E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282274618E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.125465518E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.220560953E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186252688E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81296E-03   0.45137E-02 0.19899E+01 
c  Velocity[X]                                      0.13831E-03 
c  Velocity[Y]                                      0.12896E-03 
c  Velocity[Z]                                      0.42464E-02 
c  Pressure     0.36859E-04     131   0.93776E-02   0.25999E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55016E-08   0.16372E-08 0.99887E-01 
c  r22          0.10851E-01      13   0.55404E-08   0.18273E-08 0.10198E+00 
c  r33          0.21859E-01      15   0.68566E-08   0.12577E-07 0.12822E+00 
c  r12          0.93854E-03      18   0.52835E-08   0.29979E-09 0.60816E+00 
c  r13          0.46673E-02      20   0.59510E-08   0.15028E-08 0.20044E+00 
c  r23          0.39974E-02      20   0.59690E-08   0.12904E-08 0.20054E+00 
c  epsilon      0.10970E+02      11   0.34859E-08   0.99779E-02 0.16743E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.83813E-02 0.43194E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61356       0.0052558       0.0015074
v  Velocity[Y]            -0.57339         0.54425       0.0030805       0.0008734
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.463          360.03          87.651          169.86
v  r11                   0.0010592        0.081994        0.013072        0.018285
v  r22                    0.001111         0.08262        0.013352        0.018645
v  r33                   0.0016348         0.17426        0.027247        0.037204
v  r12                   -0.010648        0.013564     -0.00023379     -0.00030929
v  r13                   -0.045558         0.05279      9.3039e-05       0.0010137
v  r23                   -0.046709        0.051256      3.0306e-05      0.00057451
v  epsilon                0.068865          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05       0.0099174      0.00092472       0.0017426
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017851           5.278         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878          0.7135         0.85283


 TIME FOR THE TIME STEP            10378:        0.81559E+02

===============================================================


 INSTANT    0.103790000E-01   TIME STEP NUMBER           10379
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.199189870E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.348252366E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.150181618E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.125498967E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.588274493E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81200E-03   0.45408E-02 0.19970E+01 
c  Velocity[X]                                      0.13858E-03 
c  Velocity[Y]                                      0.12927E-03 
c  Velocity[Z]                                      0.42729E-02 
c  Pressure     0.37052E-04     132   0.94375E-02   0.26135E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56337E-08   0.16321E-08 0.10002E+00 
c  r22          0.10851E-01      13   0.54026E-08   0.18461E-08 0.10239E+00 
c  r33          0.21859E-01      15   0.65681E-08   0.12521E-07 0.12809E+00 
c  r12          0.93854E-03      18   0.53159E-08   0.29855E-09 0.60707E+00 
c  r13          0.46673E-02      19   0.71323E-08   0.15068E-08 0.20078E+00 
c  r23          0.39974E-02      19   0.67469E-08   0.12731E-08 0.19890E+00 
c  epsilon      0.10970E+02      11   0.34808E-08   0.97852E-02 0.16533E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84378E-02 0.43312E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61358       0.0052558       0.0015074
v  Velocity[Y]             -0.5735         0.54436       0.0030805      0.00087341
v  Velocity[Z]              1.5652          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.409          360.01          87.635          169.84
v  r11                   0.0010592        0.081992        0.013072        0.018285
v  r22                    0.001111        0.082619        0.013352        0.018645
v  r33                   0.0016349         0.17428        0.027247        0.037204
v  r12                   -0.010645        0.013565     -0.00023379     -0.00030929
v  r13                   -0.045556        0.052789      9.3041e-05       0.0010137
v  r23                   -0.046709        0.051233      3.0308e-05      0.00057451
v  epsilon                0.068866          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099174      0.00092472       0.0017426
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2774         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774          0.7135         0.85283


 TIME FOR THE TIME STEP            10379:        0.81421E+02

===============================================================


 INSTANT    0.103800000E-01   TIME STEP NUMBER           10380
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.547351973E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.215005598E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141173609E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.406525458E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154863510E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81222E-03   0.45147E-02 0.19914E+01 
c  Velocity[X]                                      0.13912E-03 
c  Velocity[Y]                                      0.12883E-03 
c  Velocity[Z]                                      0.42468E-02 
c  Pressure     0.36137E-04     133   0.91983E-02   0.25490E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58306E-08   0.16408E-08 0.10001E+00 
c  r22          0.10851E-01      13   0.52032E-08   0.18195E-08 0.10131E+00 
c  r33          0.21859E-01      15   0.57558E-08   0.12522E-07 0.12762E+00 
c  r12          0.93854E-03      18   0.53325E-08   0.30562E-09 0.61086E+00 
c  r13          0.46673E-02      19   0.68523E-08   0.15032E-08 0.20019E+00 
c  r23          0.39974E-02      19   0.66045E-08   0.12836E-08 0.19992E+00 
c  epsilon      0.10970E+02      11   0.34240E-08   0.99296E-02 0.16558E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.84373E-02 0.43371E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61358       0.0052558       0.0015074
v  Velocity[Y]            -0.57352         0.54455       0.0030805       0.0008734
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.482          360.06          87.678          169.88
v  r11                   0.0010592        0.081991        0.013072        0.018285
v  r22                    0.001111        0.082619        0.013352        0.018645
v  r33                   0.0016349          0.1743        0.027247        0.037204
v  r12                   -0.010644        0.013573     -0.00023379     -0.00030929
v  r13                   -0.045554         0.05279      9.3042e-05       0.0010137
v  r23                   -0.046708        0.051249      3.0309e-05      0.00057451
v  epsilon                0.068867          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099174      0.00092472       0.0017426
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2774         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774          0.7135         0.85284


 TIME FOR THE TIME STEP            10380:        0.89135E+02

===============================================================


 INSTANT    0.103810000E-01   TIME STEP NUMBER           10381
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267543458E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.185964060E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.214973904E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.124330859E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.297967558E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      40   0.81298E-03   0.44994E-02 0.19870E+01 
c  Velocity[X]                                      0.13802E-03 
c  Velocity[Y]                                      0.12800E-03 
c  Velocity[Z]                                      0.42334E-02 
c  Pressure     0.36336E-04     132   0.92465E-02   0.25630E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57573E-08   0.16567E-08 0.10016E+00 
c  r22          0.10851E-01      13   0.50200E-08   0.17978E-08 0.10092E+00 
c  r33          0.21859E-01      15   0.61745E-08   0.12503E-07 0.12767E+00 
c  r12          0.93854E-03      18   0.53674E-08   0.29649E-09 0.60322E+00 
c  r13          0.46673E-02      19   0.60783E-08   0.14729E-08 0.19857E+00 
c  r23          0.39974E-02      19   0.57711E-08   0.12951E-08 0.20082E+00 
c  epsilon      0.10970E+02      11   0.33362E-08   0.10118E-01 0.17067E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.83649E-02 0.43128E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61356       0.0052558       0.0015074
v  Velocity[Y]            -0.57366          0.5442       0.0030805      0.00087342
v  Velocity[Z]              1.5653          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4375          4.3406          4.3632
v  Pressure                -36.447          360.02          87.631          169.84
v  r11                   0.0010592           0.082        0.013072        0.018285
v  r22                    0.001111        0.082615        0.013352        0.018645
v  r33                   0.0016349         0.17433        0.027247        0.037204
v  r12                   -0.010641        0.013581     -0.00023379     -0.00030929
v  r13                   -0.045558        0.052791      9.3042e-05       0.0010137
v  r23                   -0.046708        0.051232       3.031e-05      0.00057451
v  epsilon                0.068869          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099174      0.00092472       0.0017426
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2776         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776          0.7135         0.85283


 TIME FOR THE TIME STEP            10381:        0.81420E+02

===============================================================


 INSTANT    0.103820000E-01   TIME STEP NUMBER           10382
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.635794356E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.187092911E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.274065406E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.921789746E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.149027148E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81256E-03   0.45450E-02 0.19956E+01 
c  Velocity[X]                                      0.13786E-03 
c  Velocity[Y]                                      0.12908E-03 
c  Velocity[Z]                                      0.42781E-02 
c  Pressure     0.36415E-04     132   0.92776E-02   0.25686E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59209E-08   0.16561E-08 0.10024E+00 
c  r22          0.10851E-01      13   0.47178E-08   0.18417E-08 0.10158E+00 
c  r33          0.21859E-01      15   0.54095E-08   0.12689E-07 0.12799E+00 
c  r12          0.93855E-03      17   0.67315E-08   0.29890E-09 0.60547E+00 
c  r13          0.46673E-02      19   0.58604E-08   0.15110E-08 0.20051E+00 
c  r23          0.39974E-02      19   0.59205E-08   0.12904E-08 0.19968E+00 
c  epsilon      0.10970E+02      11   0.32456E-08   0.10157E-01 0.16835E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.84168E-02 0.43306E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61357       0.0052559       0.0015075
v  Velocity[Y]            -0.57355         0.54425       0.0030805       0.0008734
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.469             360          87.636          169.83
v  r11                   0.0010592         0.08199        0.013072        0.018285
v  r22                   0.0011111        0.082616        0.013352        0.018645
v  r33                   0.0016349         0.17431        0.027247        0.037204
v  r12                   -0.010642        0.013582     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052792      9.3043e-05       0.0010137
v  r23                   -0.046707        0.051211      3.0311e-05      0.00057451
v  epsilon                 0.06887          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05       0.0099175      0.00092472       0.0017426
v  CourantNb                0.4422             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2773         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8773          0.7135         0.85282


 TIME FOR THE TIME STEP            10382:        0.83201E+02

===============================================================


 INSTANT    0.103830000E-01   TIME STEP NUMBER           10383
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.443122758E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.223644957E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.299591707E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195443409E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.372898712E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81170E-03   0.45544E-02 0.19988E+01 
c  Velocity[X]                                      0.13939E-03 
c  Velocity[Y]                                      0.12939E-03 
c  Velocity[Z]                                      0.42857E-02 
c  Pressure     0.36612E-04     131   0.93150E-02   0.25825E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51954E-08   0.16210E-08 0.99387E-01 
c  r22          0.10851E-01      13   0.46001E-08   0.18190E-08 0.10100E+00 
c  r33          0.21859E-01      15   0.55957E-08   0.12387E-07 0.12679E+00 
c  r12          0.93855E-03      17   0.69373E-08   0.29489E-09 0.60239E+00 
c  r13          0.46673E-02      19   0.55206E-08   0.14894E-08 0.19909E+00 
c  r23          0.39974E-02      19   0.56941E-08   0.12700E-08 0.19814E+00 
c  epsilon      0.10970E+02      11   0.33234E-08   0.96764E-02 0.16353E+00 
c  TempC        0.25716E+06      16   0.15094E-04   0.84617E-02 0.43392E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61361       0.0052559       0.0015075
v  Velocity[Y]            -0.57358         0.54439       0.0030805      0.00087341
v  Velocity[Z]              1.5652          5.4374          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4374          4.3406          4.3632
v  Pressure                -36.426          360.04          87.653          169.86
v  r11                   0.0010592        0.081981        0.013072        0.018285
v  r22                   0.0011111        0.082617        0.013352        0.018645
v  r33                   0.0016349         0.17428        0.027247        0.037204
v  r12                   -0.010639        0.013589     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052789      9.3043e-05       0.0010137
v  r23                   -0.046707        0.051237      3.0312e-05      0.00057451
v  epsilon                0.068871          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099176      0.00092472       0.0017426
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2771         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8771          0.7135         0.85283


 TIME FOR THE TIME STEP            10383:        0.84794E+02

===============================================================


 INSTANT    0.103840000E-01   TIME STEP NUMBER           10384
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100481145E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.213205615E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154808341E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.233882139E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.281788875E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81343E-03   0.44948E-02 0.19865E+01 
c  Velocity[X]                                      0.13848E-03 
c  Velocity[Y]                                      0.12894E-03 
c  Velocity[Z]                                      0.42274E-02 
c  Pressure     0.35840E-04     133   0.91223E-02   0.25280E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.50399E-08   0.16428E-08 0.99203E-01 
c  r22          0.10851E-01      13   0.50305E-08   0.18414E-08 0.10111E+00 
c  r33          0.21859E-01      15   0.64429E-08   0.12616E-07 0.12694E+00 
c  r12          0.93855E-03      17   0.67135E-08   0.29810E-09 0.60304E+00 
c  r13          0.46673E-02      19   0.70139E-08   0.14954E-08 0.19871E+00 
c  r23          0.39974E-02      19   0.59866E-08   0.12626E-08 0.19715E+00 
c  epsilon      0.10970E+02      11   0.33535E-08   0.10306E-01 0.16829E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.83919E-02 0.43204E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61357       0.0052558       0.0015074
v  Velocity[Y]             -0.5736         0.54452       0.0030805       0.0008734
v  Velocity[Z]              1.5654          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4374          4.3406          4.3632
v  Pressure                -36.467          360.01          87.635          169.84
v  r11                   0.0010592        0.081972        0.013072        0.018285
v  r22                   0.0011111        0.082618        0.013352        0.018645
v  r33                   0.0016349         0.17429        0.027247        0.037204
v  r12                   -0.010639        0.013596     -0.00023379     -0.00030929
v  r13                   -0.045557        0.052789      9.3045e-05       0.0010137
v  r23                   -0.046707         0.05123      3.0313e-05      0.00057451
v  epsilon                0.068872          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099176      0.00092473       0.0017426
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2777         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8777          0.7135         0.85283


 TIME FOR THE TIME STEP            10384:        0.86093E+02

===============================================================


 INSTANT    0.103850000E-01   TIME STEP NUMBER           10385
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119921102E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.114038617E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226483564E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.302345790E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.252687729E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81080E-03   0.45140E-02 0.19900E+01 
c  Velocity[X]                                      0.13811E-03 
c  Velocity[Y]                                      0.12815E-03 
c  Velocity[Z]                                      0.42477E-02 
c  Pressure     0.36724E-04     134   0.93451E-02   0.25904E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57200E-08   0.16410E-08 0.99522E-01 
c  r22          0.10851E-01      13   0.51008E-08   0.18473E-08 0.10144E+00 
c  r33          0.21859E-01      15   0.68448E-08   0.12693E-07 0.12776E+00 
c  r12          0.93855E-03      18   0.50153E-08   0.30364E-09 0.60678E+00 
c  r13          0.46673E-02      20   0.63167E-08   0.15205E-08 0.20030E+00 
c  r23          0.39974E-02      19   0.63337E-08   0.12947E-08 0.19966E+00 
c  epsilon      0.10970E+02      11   0.34812E-08   0.10246E-01 0.16717E+00 
c  TempC        0.25716E+06      16   0.15127E-04   0.84225E-02 0.43297E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161986


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61359       0.0052558       0.0015074
v  Velocity[Y]            -0.57362         0.54432       0.0030804      0.00087336
v  Velocity[Z]              1.5653          5.4374          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4374          4.3406          4.3632
v  Pressure                -36.416          360.06          87.668          169.88
v  r11                   0.0010592        0.081962        0.013072        0.018285
v  r22                   0.0011111        0.082618        0.013352        0.018645
v  r33                   0.0016349         0.17432        0.027247        0.037204
v  r12                   -0.010642        0.013594     -0.00023379     -0.00030929
v  r13                   -0.045557        0.052788      9.3046e-05       0.0010137
v  r23                   -0.046706        0.051226      3.0316e-05      0.00057452
v  epsilon                0.068873          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9939e-05       0.0099176      0.00092473       0.0017426
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2781         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781          0.7135         0.85283


 TIME FOR THE TIME STEP            10385:        0.83045E+02

===============================================================


 INSTANT    0.103860000E-01   TIME STEP NUMBER           10386
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.457675103E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.254217561E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.124367833E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.356580255E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.284784062E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81250E-03   0.45178E-02 0.19924E+01 
c  Velocity[X]                                      0.13780E-03 
c  Velocity[Y]                                      0.12913E-03 
c  Velocity[Z]                                      0.42509E-02 
c  Pressure     0.36215E-04     133   0.92138E-02   0.25544E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56480E-08   0.16282E-08 0.99795E-01 
c  r22          0.10851E-01      13   0.47673E-08   0.18108E-08 0.10144E+00 
c  r33          0.21859E-01      15   0.62693E-08   0.12470E-07 0.12782E+00 
c  r12          0.93855E-03      18   0.53578E-08   0.30046E-09 0.60774E+00 
c  r13          0.46673E-02      19   0.67209E-08   0.14962E-08 0.19999E+00 
c  r23          0.39974E-02      19   0.60229E-08   0.12886E-08 0.20074E+00 
c  epsilon      0.10970E+02      11   0.34748E-08   0.97705E-02 0.16424E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.84267E-02 0.43271E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61356       0.0052558       0.0015074
v  Velocity[Y]            -0.57363         0.54442       0.0030805      0.00087341
v  Velocity[Z]              1.5654          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4375          4.3406          4.3632
v  Pressure                -36.474          359.99          87.646          169.83
v  r11                   0.0010592        0.081952        0.013072        0.018285
v  r22                   0.0011111        0.082619        0.013352        0.018645
v  r33                   0.0016349         0.17435        0.027247        0.037204
v  r12                   -0.010644          0.0136     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052789      9.3047e-05       0.0010137
v  r23                   -0.046706        0.051216      3.0316e-05      0.00057452
v  epsilon                0.068875          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.994e-05       0.0099176      0.00092473       0.0017426
v  CourantNb                0.4422             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2779         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8779          0.7135         0.85283


 TIME FOR THE TIME STEP            10386:        0.88777E+02

===============================================================


 INSTANT    0.103870000E-01   TIME STEP NUMBER           10387
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.989966964E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.213493099E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.439120395E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.390725657E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.263648639E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81252E-03   0.45171E-02 0.19900E+01 
c  Velocity[X]                                      0.13859E-03 
c  Velocity[Y]                                      0.12832E-03 
c  Velocity[Z]                                      0.42502E-02 
c  Pressure     0.35937E-04     132   0.91455E-02   0.25349E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53953E-08   0.16690E-08 0.10025E+00 
c  r22          0.10851E-01      13   0.49818E-08   0.18642E-08 0.10214E+00 
c  r33          0.21859E-01      15   0.60423E-08   0.12841E-07 0.12891E+00 
c  r12          0.93855E-03      18   0.57925E-08   0.29961E-09 0.60714E+00 
c  r13          0.46673E-02      19   0.67891E-08   0.15037E-08 0.19988E+00 
c  r23          0.39974E-02      19   0.54323E-08   0.13144E-08 0.20207E+00 
c  epsilon      0.10970E+02      11   0.33936E-08   0.10639E-01 0.17288E+00 
c  TempC        0.25716E+06      16   0.15114E-04   0.84271E-02 0.43313E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61357       0.0052558       0.0015074
v  Velocity[Y]            -0.57367         0.54411       0.0030805       0.0008734
v  Velocity[Z]              1.5657          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4375          4.3406          4.3632
v  Pressure                -36.461          359.99          87.628          169.83
v  r11                   0.0010592        0.081946        0.013072        0.018285
v  r22                   0.0011111        0.082619        0.013352        0.018645
v  r33                   0.0016349         0.17432        0.027247        0.037204
v  r12                    -0.01065        0.013605     -0.00023379     -0.00030929
v  r13                   -0.045557        0.052787      9.3047e-05       0.0010137
v  r23                   -0.046706        0.051237      3.0317e-05      0.00057452
v  epsilon                0.068876          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9945e-05       0.0099175      0.00092473       0.0017426
v  CourantNb               0.44215             0.6         0.59908         0.59839
v  FourierNb              0.001785           5.278         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.878          0.7135         0.85283


 TIME FOR THE TIME STEP            10387:        0.78572E+02

===============================================================


 INSTANT    0.103880000E-01   TIME STEP NUMBER           10388
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.517592176E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.273738984E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200597416E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935017E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.452263009E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111585655E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81260E-03   0.45077E-02 0.19905E+01 
c  Velocity[X]                                      0.13844E-03 
c  Velocity[Y]                                      0.12864E-03 
c  Velocity[Z]                                      0.42406E-02 
c  Pressure     0.36887E-04     132   0.93910E-02   0.26019E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59787E-08   0.16197E-08 0.99510E-01 
c  r22          0.10851E-01      13   0.48192E-08   0.18367E-08 0.10177E+00 
c  r33          0.21859E-01      15   0.54389E-08   0.12427E-07 0.12772E+00 
c  r12          0.93855E-03      18   0.59752E-08   0.29498E-09 0.60513E+00 
c  r13          0.46673E-02      19   0.68401E-08   0.14944E-08 0.20013E+00 
c  r23          0.39974E-02      19   0.61589E-08   0.12621E-08 0.19855E+00 
c  epsilon      0.10970E+02      11   0.32641E-08   0.96805E-02 0.16399E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.83976E-02 0.43242E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61357       0.0052558       0.0015074
v  Velocity[Y]            -0.57363         0.54416       0.0030804      0.00087334
v  Velocity[Z]              1.5655          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4375          4.3406          4.3632
v  Pressure                -36.475          359.99          87.635          169.83
v  r11                   0.0010592        0.081938        0.013072        0.018285
v  r22                   0.0011111        0.082618        0.013352        0.018645
v  r33                   0.0016349          0.1743        0.027247        0.037204
v  r12                   -0.010653        0.013609     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052788      9.3048e-05       0.0010137
v  r23                   -0.046707        0.051232      3.0318e-05      0.00057452
v  epsilon                0.068877          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9945e-05       0.0099175      0.00092473       0.0017426
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2781         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781          0.7135         0.85283


 TIME FOR THE TIME STEP            10388:        0.80720E+02

===============================================================


 INSTANT    0.103890000E-01   TIME STEP NUMBER           10389
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.151748786E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.286141620E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184974124E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166894744E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.230663877E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      43   0.81238E-03   0.45336E-02 0.19955E+01 
c  Velocity[X]                                      0.13874E-03 
c  Velocity[Y]                                      0.12866E-03 
c  Velocity[Z]                                      0.42662E-02 
c  Pressure     0.36194E-04     133   0.92095E-02   0.25530E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.62962E-08   0.16461E-08 0.10010E+00 
c  r22          0.10851E-01      13   0.47520E-08   0.18226E-08 0.10163E+00 
c  r33          0.21859E-01      15   0.52360E-08   0.12479E-07 0.12791E+00 
c  r12          0.93855E-03      18   0.66419E-08   0.30719E-09 0.61387E+00 
c  r13          0.46673E-02      20   0.60794E-08   0.14737E-08 0.19921E+00 
c  r23          0.39974E-02      19   0.68786E-08   0.12892E-08 0.20107E+00 
c  epsilon      0.10970E+02      11   0.32810E-08   0.94489E-02 0.16188E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.84521E-02 0.43411E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61356       0.0052557       0.0015074
v  Velocity[Y]            -0.57362         0.54432       0.0030805      0.00087335
v  Velocity[Z]              1.5656          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4375          4.3406          4.3632
v  Pressure                -36.414           360.1          87.694          169.92
v  r11                   0.0010592        0.081945        0.013072        0.018285
v  r22                   0.0011111        0.082615        0.013352        0.018645
v  r33                    0.001635          0.1743        0.027247        0.037204
v  r12                   -0.010656        0.013606     -0.00023379     -0.00030929
v  r13                   -0.045556        0.052791      9.3048e-05       0.0010137
v  r23                   -0.046708        0.051227      3.0319e-05      0.00057452
v  epsilon                0.068878          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099176      0.00092473       0.0017426
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2779         0.11441         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8779          0.7135         0.85283


 TIME FOR THE TIME STEP            10389:        0.84070E+02

===============================================================


 INSTANT    0.103900000E-01   TIME STEP NUMBER           10390
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.151094303E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.333391071E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.353628992E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186979225E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136982587E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      42   0.81244E-03   0.44917E-02 0.19867E+01 
c  Velocity[X]                                      0.13808E-03 
c  Velocity[Y]                                      0.12864E-03 
c  Velocity[Z]                                      0.42250E-02 
c  Pressure     0.36127E-04     132   0.91907E-02   0.25483E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.65874E-08   0.16412E-08 0.99475E-01 
c  r22          0.10851E-01      13   0.48030E-08   0.18739E-08 0.10237E+00 
c  r33          0.21859E-01      15   0.56039E-08   0.12747E-07 0.12817E+00 
c  r12          0.93855E-03      18   0.68513E-08   0.30163E-09 0.61025E+00 
c  r13          0.46673E-02      19   0.70931E-08   0.15030E-08 0.20041E+00 
c  r23          0.39974E-02      19   0.64504E-08   0.12785E-08 0.19925E+00 
c  epsilon      0.10970E+02      11   0.31818E-08   0.99393E-02 0.16529E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.83830E-02 0.43190E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61356       0.0052557       0.0015074
v  Velocity[Y]            -0.57356         0.54404       0.0030804      0.00087332
v  Velocity[Z]              1.5655          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4375          4.3406          4.3632
v  Pressure                -36.464          360.02           87.65          169.85
v  r11                   0.0010592        0.081948        0.013072        0.018285
v  r22                   0.0011111        0.082616        0.013352        0.018645
v  r33                    0.001635         0.17432        0.027247        0.037204
v  r12                   -0.010656        0.013607     -0.00023379     -0.00030929
v  r13                   -0.045558         0.05279      9.3049e-05       0.0010137
v  r23                    -0.04671        0.051253       3.032e-05      0.00057452
v  epsilon                0.068879          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099177      0.00092473       0.0017426
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2779         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8779          0.7135         0.85283


 TIME FOR THE TIME STEP            10390:        0.90984E+02

===============================================================


 INSTANT    0.103910000E-01   TIME STEP NUMBER           10391
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200167460E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.332301821E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934905E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.848056508E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.285073734E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151539742E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81248E-03   0.45548E-02 0.19988E+01 
c  Velocity[X]                                      0.13886E-03 
c  Velocity[Y]                                      0.12933E-03 
c  Velocity[Z]                                      0.42867E-02 
c  Pressure     0.36792E-04     132   0.93649E-02   0.25952E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60837E-08   0.16355E-08 0.99551E-01 
c  r22          0.10851E-01      13   0.46906E-08   0.18808E-08 0.10245E+00 
c  r33          0.21859E-01      15   0.57769E-08   0.12737E-07 0.12823E+00 
c  r12          0.93855E-03      18   0.60128E-08   0.29297E-09 0.60463E+00 
c  r13          0.46673E-02      19   0.61315E-08   0.15308E-08 0.20101E+00 
c  r23          0.39974E-02      19   0.57789E-08   0.12705E-08 0.19813E+00 
c  epsilon      0.10970E+02      11   0.33705E-08   0.10208E-01 0.16730E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.84086E-02 0.43236E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61358       0.0052558       0.0015074
v  Velocity[Y]            -0.57355         0.54362       0.0030805      0.00087335
v  Velocity[Z]              1.5653          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4375          4.3406          4.3632
v  Pressure                -36.378          360.01          87.638          169.83
v  r11                   0.0010592        0.081942        0.013072        0.018285
v  r22                   0.0011111        0.082616        0.013352        0.018645
v  r33                    0.001635         0.17431        0.027247        0.037204
v  r12                   -0.010654        0.013596     -0.00023379     -0.00030929
v  r13                   -0.045556        0.052786      9.3051e-05       0.0010137
v  r23                   -0.046711        0.051246      3.0322e-05      0.00057452
v  epsilon                0.068881          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099178      0.00092473       0.0017426
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2781         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781          0.7135         0.85283


 TIME FOR THE TIME STEP            10391:        0.10400E+03

===============================================================


 INSTANT    0.103920000E-01   TIME STEP NUMBER           10392
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.229832374E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.189282747E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.246841568E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935019E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.216531328E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158651469E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81236E-03   0.45227E-02 0.19912E+01 
c  Velocity[X]                                      0.13857E-03 
c  Velocity[Y]                                      0.12888E-03 
c  Velocity[Z]                                      0.42553E-02 
c  Pressure     0.36752E-04     132   0.93627E-02   0.25923E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.62584E-08   0.16632E-08 0.10040E+00 
c  r22          0.10851E-01      13   0.46389E-08   0.18644E-08 0.10253E+00 
c  r33          0.21859E-01      15   0.64931E-08   0.12733E-07 0.12867E+00 
c  r12          0.93855E-03      18   0.57774E-08   0.30218E-09 0.60985E+00 
c  r13          0.46673E-02      19   0.68262E-08   0.15348E-08 0.20180E+00 
c  r23          0.39974E-02      19   0.63007E-08   0.13121E-08 0.20091E+00 
c  epsilon      0.10970E+02      11   0.36135E-08   0.99226E-02 0.16522E+00 
c  TempC        0.25716E+06      16   0.15181E-04   0.84507E-02 0.43379E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61359       0.0052558       0.0015074
v  Velocity[Y]            -0.57334         0.54378       0.0030804      0.00087333
v  Velocity[Z]              1.5655          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4375          4.3406          4.3632
v  Pressure                 -36.45          360.02          87.639          169.84
v  r11                   0.0010592        0.081947        0.013072        0.018285
v  r22                   0.0011111        0.082617        0.013352        0.018645
v  r33                    0.001635         0.17428        0.027247        0.037204
v  r12                   -0.010654        0.013593     -0.00023379     -0.00030929
v  r13                   -0.045554        0.052787      9.3051e-05       0.0010137
v  r23                   -0.046712        0.051232      3.0323e-05      0.00057452
v  epsilon                0.068882          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9949e-05        0.009918      0.00092473       0.0017426
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2786         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8786          0.7135         0.85283


 TIME FOR THE TIME STEP            10392:        0.82876E+02

===============================================================


 INSTANT    0.103930000E-01   TIME STEP NUMBER           10393
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.249303651E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.705247768E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173983893E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162489814E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.958792865E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36449E+01      41   0.81236E-03   0.45259E-02 0.19908E+01 
c  Velocity[X]                                      0.13736E-03 
c  Velocity[Y]                                      0.12856E-03 
c  Velocity[Z]                                      0.42599E-02 
c  Pressure     0.36133E-04     131   0.91971E-02   0.25487E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.61310E-08   0.16938E-08 0.10120E+00 
c  r22          0.10851E-01      13   0.45908E-08   0.18243E-08 0.10143E+00 
c  r33          0.21859E-01      15   0.52632E-08   0.12648E-07 0.12817E+00 
c  r12          0.93855E-03      18   0.60708E-08   0.29929E-09 0.60958E+00 
c  r13          0.46673E-02      19   0.56700E-08   0.14877E-08 0.19945E+00 
c  r23          0.39974E-02      19   0.56124E-08   0.12983E-08 0.20123E+00 
c  epsilon      0.10970E+02      11   0.34503E-08   0.10231E-01 0.17205E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.84043E-02 0.43269E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61359       0.0052558       0.0015074
v  Velocity[Y]            -0.57347         0.54392       0.0030805      0.00087333
v  Velocity[Z]              1.5656          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4375          4.3406          4.3632
v  Pressure                -36.418          360.05          87.649          169.86
v  r11                   0.0010592        0.081953        0.013072        0.018285
v  r22                   0.0011111        0.082619        0.013352        0.018645
v  r33                    0.001635          0.1743        0.027247        0.037204
v  r12                   -0.010653        0.013588     -0.00023379     -0.00030929
v  r13                   -0.045558        0.052787      9.3052e-05       0.0010137
v  r23                   -0.046712        0.051261      3.0323e-05      0.00057452
v  epsilon                0.068883          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05        0.009918      0.00092474       0.0017426
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2792         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8792          0.7135         0.85283


 TIME FOR THE TIME STEP            10393:        0.85229E+02

===============================================================


 INSTANT    0.103940000E-01   TIME STEP NUMBER           10394
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.314972404E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.745079459E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.953081996E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.270360597E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934918E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.223710485E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81241E-03   0.45425E-02 0.19965E+01 
c  Velocity[X]                                      0.13842E-03 
c  Velocity[Y]                                      0.12930E-03 
c  Velocity[Z]                                      0.42748E-02 
c  Pressure     0.36712E-04     132   0.93417E-02   0.25895E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58589E-08   0.16552E-08 0.10056E+00 
c  r22          0.10851E-01      13   0.47669E-08   0.18525E-08 0.10240E+00 
c  r33          0.21859E-01      15   0.54448E-08   0.12684E-07 0.12890E+00 
c  r12          0.93855E-03      18   0.58724E-08   0.29754E-09 0.60707E+00 
c  r13          0.46673E-02      19   0.57724E-08   0.15208E-08 0.20191E+00 
c  r23          0.39974E-02      19   0.59728E-08   0.12826E-08 0.20042E+00 
c  epsilon      0.10970E+02      11   0.33287E-08   0.10117E-01 0.16918E+00 
c  TempC        0.25716E+06      16   0.15169E-04   0.84363E-02 0.43303E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386          0.6136       0.0052557       0.0015073
v  Velocity[Y]            -0.57351         0.54413       0.0030804      0.00087332
v  Velocity[Z]              1.5656          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4375          4.3406          4.3632
v  Pressure                -36.428          360.04          87.674          169.87
v  r11                   0.0010592        0.081962        0.013072        0.018285
v  r22                   0.0011111        0.082619        0.013352        0.018645
v  r33                    0.001635         0.17433        0.027247        0.037205
v  r12                    -0.01065        0.013581     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052788      9.3053e-05       0.0010137
v  r23                   -0.046712        0.051254      3.0324e-05      0.00057452
v  epsilon                0.068884          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9953e-05        0.009918      0.00092474       0.0017426
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2792         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8792          0.7135         0.85283


 TIME FOR THE TIME STEP            10394:        0.89404E+02

===============================================================


 INSTANT    0.103950000E-01   TIME STEP NUMBER           10395
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.138828576E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.277212664E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105686971E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.149981830E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.611528303E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81209E-03   0.45096E-02 0.19897E+01 
c  Velocity[X]                                      0.13961E-03 
c  Velocity[Y]                                      0.12846E-03 
c  Velocity[Z]                                      0.42415E-02 
c  Pressure     0.36282E-04     132   0.92417E-02   0.25591E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56765E-08   0.16617E-08 0.10056E+00 
c  r22          0.10851E-01      13   0.48647E-08   0.18270E-08 0.10159E+00 
c  r33          0.21859E-01      15   0.54349E-08   0.12535E-07 0.12773E+00 
c  r12          0.93855E-03      18   0.53977E-08   0.29589E-09 0.60698E+00 
c  r13          0.46673E-02      18   0.70765E-08   0.14958E-08 0.20033E+00 
c  r23          0.39974E-02      19   0.53969E-08   0.12834E-08 0.19975E+00 
c  epsilon      0.10970E+02      11   0.33438E-08   0.99108E-02 0.16426E+00 
c  TempC        0.25716E+06      16   0.15103E-04   0.84565E-02 0.43366E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61361       0.0052558       0.0015073
v  Velocity[Y]            -0.57359         0.54436       0.0030805      0.00087334
v  Velocity[Z]              1.5655          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4375          4.3406          4.3632
v  Pressure                -36.404          360.07          87.677          169.89
v  r11                   0.0010592        0.081964        0.013072        0.018285
v  r22                   0.0011111        0.082621        0.013352        0.018645
v  r33                    0.001635          0.1743        0.027247        0.037205
v  r12                    -0.01065        0.013586     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052789      9.3054e-05       0.0010137
v  r23                   -0.046713        0.051244      3.0326e-05      0.00057452
v  epsilon                0.068885          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9956e-05       0.0099181      0.00092474       0.0017426
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2782         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8782          0.7135         0.85283


 TIME FOR THE TIME STEP            10395:        0.86316E+02

===============================================================


 INSTANT    0.103960000E-01   TIME STEP NUMBER           10396
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.236189738E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149434922E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.129052431E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.295410560E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.723956916E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81375E-03   0.45152E-02 0.19911E+01 
c  Velocity[X]                                      0.13908E-03 
c  Velocity[Y]                                      0.12889E-03 
c  Velocity[Z]                                      0.42472E-02 
c  Pressure     0.36651E-04     131   0.93258E-02   0.25853E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51306E-08   0.16778E-08 0.10053E+00 
c  r22          0.10851E-01      13   0.48242E-08   0.18509E-08 0.10223E+00 
c  r33          0.21859E-01      15   0.55229E-08   0.12812E-07 0.12868E+00 
c  r12          0.93855E-03      18   0.57231E-08   0.30349E-09 0.60741E+00 
c  r13          0.46673E-02      18   0.72450E-08   0.15172E-08 0.20071E+00 
c  r23          0.39974E-02      19   0.52757E-08   0.13242E-08 0.20120E+00 
c  epsilon      0.10970E+02      11   0.34186E-08   0.10306E-01 0.16852E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.83665E-02 0.43196E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61356       0.0052558       0.0015073
v  Velocity[Y]             -0.5735         0.54414       0.0030805      0.00087335
v  Velocity[Z]              1.5654          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4375          4.3406          4.3632
v  Pressure                -36.448          360.05           87.66          169.87
v  r11                   0.0010592        0.081967        0.013072        0.018285
v  r22                   0.0011111        0.082622        0.013352        0.018645
v  r33                    0.001635         0.17427        0.027247        0.037205
v  r12                   -0.010651        0.013582     -0.00023379     -0.00030929
v  r13                   -0.045557        0.052791      9.3055e-05       0.0010137
v  r23                   -0.046713        0.051239      3.0327e-05      0.00057452
v  epsilon                0.068887          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9954e-05       0.0099182      0.00092474       0.0017426
v  CourantNb               0.44217             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2781         0.11442         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781          0.7135         0.85284


 TIME FOR THE TIME STEP            10396:        0.89438E+02

===============================================================


 INSTANT    0.103970000E-01   TIME STEP NUMBER           10397
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232903706E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.427467288E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.278379885E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.238534970E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.543817312E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81202E-03   0.45469E-02 0.19963E+01 
c  Velocity[X]                                      0.13807E-03 
c  Velocity[Y]                                      0.13010E-03 
c  Velocity[Z]                                      0.42787E-02 
c  Pressure     0.36054E-04     132   0.91712E-02   0.25432E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54623E-08   0.16651E-08 0.10065E+00 
c  r22          0.10851E-01      13   0.49841E-08   0.18536E-08 0.10181E+00 
c  r33          0.21859E-01      15   0.51965E-08   0.12680E-07 0.12820E+00 
c  r12          0.93855E-03      18   0.60876E-08   0.30427E-09 0.60994E+00 
c  r13          0.46673E-02      19   0.63178E-08   0.15091E-08 0.20043E+00 
c  r23          0.39974E-02      19   0.53182E-08   0.12713E-08 0.19972E+00 
c  epsilon      0.10970E+02      11   0.33143E-08   0.10092E-01 0.16632E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.83825E-02 0.43218E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63401         0.61359       0.0052558       0.0015073
v  Velocity[Y]             -0.5734         0.54425       0.0030806      0.00087339
v  Velocity[Z]              1.5653          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4375          4.3406          4.3632
v  Pressure                 -36.39             360          87.637          169.84
v  r11                   0.0010592        0.081976        0.013072        0.018285
v  r22                   0.0011111        0.082619        0.013352        0.018645
v  r33                    0.001635         0.17429        0.027247        0.037205
v  r12                   -0.010651        0.013589     -0.00023379     -0.00030929
v  r13                   -0.045556        0.052792      9.3056e-05       0.0010137
v  r23                   -0.046713        0.051263      3.0329e-05      0.00057452
v  epsilon                0.068888          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9953e-05       0.0099182      0.00092474       0.0017426
v  CourantNb                0.4422             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2779         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8779          0.7135         0.85284


 TIME FOR THE TIME STEP            10397:        0.85727E+02

===============================================================


 INSTANT    0.103980000E-01   TIME STEP NUMBER           10398
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.268878618E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.133408322E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.554686410E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.209960031E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.731520306E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81289E-03   0.45161E-02 0.19898E+01 
c  Velocity[X]                                      0.13869E-03 
c  Velocity[Y]                                      0.12940E-03 
c  Velocity[Z]                                      0.42480E-02 
c  Pressure     0.36463E-04     133   0.92857E-02   0.25719E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53985E-08   0.16519E-08 0.10021E+00 
c  r22          0.10851E-01      13   0.53032E-08   0.18212E-08 0.10146E+00 
c  r33          0.21859E-01      15   0.60045E-08   0.12499E-07 0.12743E+00 
c  r12          0.93855E-03      18   0.67587E-08   0.30140E-09 0.60911E+00 
c  r13          0.46673E-02      19   0.69099E-08   0.14884E-08 0.19965E+00 
c  r23          0.39974E-02      19   0.61072E-08   0.12757E-08 0.19908E+00 
c  epsilon      0.10970E+02      11   0.35095E-08   0.97788E-02 0.16339E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.84249E-02 0.43266E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63401         0.61358       0.0052558       0.0015073
v  Velocity[Y]            -0.57342         0.54443       0.0030805      0.00087334
v  Velocity[Z]              1.5654          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4375          4.3406          4.3632
v  Pressure                -36.429             360          87.658          169.84
v  r11                   0.0010592        0.081973        0.013072        0.018285
v  r22                   0.0011112        0.082623        0.013352        0.018645
v  r33                   0.0016351         0.17432        0.027247        0.037205
v  r12                   -0.010655        0.013595     -0.00023379     -0.00030929
v  r13                   -0.045554        0.052795      9.3057e-05       0.0010137
v  r23                   -0.046713        0.051255      3.0331e-05      0.00057452
v  epsilon                0.068889          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9949e-05       0.0099182      0.00092474       0.0017426
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2783         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8783          0.7135         0.85283


 TIME FOR THE TIME STEP            10398:        0.83203E+02

===============================================================


 INSTANT    0.103990000E-01   TIME STEP NUMBER           10399
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.819031142E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.286023282E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.307098121E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140811968E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.210989628E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81307E-03   0.45182E-02 0.19910E+01 
c  Velocity[X]                                      0.13799E-03 
c  Velocity[Y]                                      0.12869E-03 
c  Velocity[Z]                                      0.42515E-02 
c  Pressure     0.36618E-04     131   0.93265E-02   0.25829E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56270E-08   0.16982E-08 0.10105E+00 
c  r22          0.10851E-01      13   0.52745E-08   0.18623E-08 0.10196E+00 
c  r33          0.21859E-01      15   0.70009E-08   0.13004E-07 0.12933E+00 
c  r12          0.93855E-03      18   0.68183E-08   0.30072E-09 0.60551E+00 
c  r13          0.46673E-02      19   0.65917E-08   0.15056E-08 0.20032E+00 
c  r23          0.39974E-02      20   0.56444E-08   0.13335E-08 0.20290E+00 
c  epsilon      0.10970E+02      11   0.36498E-08   0.10912E-01 0.17576E+00 
c  TempC        0.25716E+06      16   0.15108E-04   0.84492E-02 0.43357E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -0.634         0.61357       0.0052557       0.0015073
v  Velocity[Y]            -0.57342         0.54408       0.0030805      0.00087338
v  Velocity[Z]              1.5657          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4375          4.3406          4.3632
v  Pressure                -36.373          360.08          87.683           169.9
v  r11                   0.0010592         0.08197        0.013072        0.018285
v  r22                   0.0011112        0.082625        0.013352        0.018645
v  r33                   0.0016351         0.17435        0.027247        0.037205
v  r12                   -0.010657        0.013592     -0.00023379     -0.00030929
v  r13                   -0.045557        0.052793      9.3057e-05       0.0010137
v  r23                   -0.046713        0.051252      3.0331e-05      0.00057452
v  epsilon                 0.06889          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099182      0.00092474       0.0017426
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2785         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8785          0.7135         0.85283


 TIME FOR THE TIME STEP            10399:        0.84762E+02

===============================================================


 INSTANT    0.104000000E-01   TIME STEP NUMBER           10400
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.936623721E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.349111681E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.783414974E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.576171905E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188526103E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81187E-03   0.45410E-02 0.19967E+01 
c  Velocity[X]                                      0.13817E-03 
c  Velocity[Y]                                      0.12809E-03 
c  Velocity[Z]                                      0.42747E-02 
c  Pressure     0.36688E-04     133   0.93362E-02   0.25880E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.49901E-08   0.16218E-08 0.99645E-01 
c  r22          0.10851E-01      13   0.50730E-08   0.18142E-08 0.10139E+00 
c  r33          0.21859E-01      15   0.58405E-08   0.12319E-07 0.12716E+00 
c  r12          0.93855E-03      18   0.59734E-08   0.29113E-09 0.60214E+00 
c  r13          0.46673E-02      19   0.64385E-08   0.14805E-08 0.19882E+00 
c  r23          0.39974E-02      19   0.65870E-08   0.12551E-08 0.19772E+00 
c  epsilon      0.10970E+02      11   0.34176E-08   0.95200E-02 0.16341E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.84484E-02 0.43384E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63407         0.61359       0.0052558       0.0015073
v  Velocity[Y]            -0.57332         0.54412       0.0030805      0.00087336
v  Velocity[Z]              1.5655          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4375          4.3406          4.3632
v  Pressure                -36.424          360.07          87.695          169.91
v  r11                   0.0010592        0.081978        0.013072        0.018285
v  r22                   0.0011112        0.082626        0.013352        0.018645
v  r33                   0.0016351         0.17432        0.027247        0.037205
v  r12                   -0.010665        0.013596     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052795      9.3057e-05       0.0010137
v  r23                   -0.046713        0.051278      3.0332e-05      0.00057452
v  epsilon                0.068891          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099181      0.00092474       0.0017426
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2789         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8789          0.7135         0.85283


 TIME FOR THE TIME STEP            10400:        0.83265E+02

===============================================================


 INSTANT    0.104010000E-01   TIME STEP NUMBER           10401
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150743591E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.433628668E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.266353153E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.219989686E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.470553305E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81206E-03   0.45442E-02 0.19976E+01 
c  Velocity[X]                                      0.13920E-03 
c  Velocity[Y]                                      0.12939E-03 
c  Velocity[Z]                                      0.42756E-02 
c  Pressure     0.36451E-04     133   0.92831E-02   0.25712E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51374E-08   0.16663E-08 0.10000E+00 
c  r22          0.10851E-01      13   0.55578E-08   0.18285E-08 0.10139E+00 
c  r33          0.21859E-01      15   0.54310E-08   0.12564E-07 0.12733E+00 
c  r12          0.93855E-03      18   0.65148E-08   0.29933E-09 0.60909E+00 
c  r13          0.46673E-02      19   0.54061E-08   0.14930E-08 0.19936E+00 
c  r23          0.39974E-02      19   0.64650E-08   0.12913E-08 0.19922E+00 
c  epsilon      0.10970E+02      11   0.34578E-08   0.99440E-02 0.16459E+00 
c  TempC        0.25716E+06      16   0.15172E-04   0.84672E-02 0.43406E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63406         0.61359       0.0052558       0.0015073
v  Velocity[Y]            -0.57348         0.54427       0.0030805      0.00087337
v  Velocity[Z]              1.5657          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4375          4.3406          4.3632
v  Pressure                -36.369          360.04           87.67          169.87
v  r11                   0.0010592        0.081973        0.013072        0.018285
v  r22                   0.0011112        0.082627        0.013352        0.018645
v  r33                   0.0016351         0.17429        0.027247        0.037205
v  r12                   -0.010664        0.013604     -0.00023379     -0.00030929
v  r13                   -0.045556        0.052795      9.3058e-05       0.0010137
v  r23                   -0.046713        0.051264      3.0334e-05      0.00057452
v  epsilon                0.068892          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.994e-05       0.0099181      0.00092474       0.0017426
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2788         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8788          0.7135         0.85284


 TIME FOR THE TIME STEP            10401:        0.83498E+02

===============================================================


 INSTANT    0.104020000E-01   TIME STEP NUMBER           10402
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.259362097E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.717527860E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122544583E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.148083600E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.447383785E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81297E-03   0.45081E-02 0.19880E+01 
c  Velocity[X]                                      0.13834E-03 
c  Velocity[Y]                                      0.12936E-03 
c  Velocity[Z]                                      0.42404E-02 
c  Pressure     0.36167E-04     133   0.92077E-02   0.25510E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51044E-08   0.16550E-08 0.10044E+00 
c  r22          0.10851E-01      13   0.52907E-08   0.18388E-08 0.10176E+00 
c  r33          0.21859E-01      14   0.69335E-08   0.12592E-07 0.12801E+00 
c  r12          0.93855E-03      18   0.57543E-08   0.29625E-09 0.60717E+00 
c  r13          0.46674E-02      18   0.61054E-08   0.14835E-08 0.19941E+00 
c  r23          0.39974E-02      19   0.61406E-08   0.12846E-08 0.20069E+00 
c  epsilon      0.10970E+02      11   0.33785E-08   0.99600E-02 0.16627E+00 
c  TempC        0.25716E+06      16   0.15122E-04   0.83304E-02 0.43043E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61355       0.0052558       0.0015073
v  Velocity[Y]            -0.57345          0.5441       0.0030806      0.00087338
v  Velocity[Z]              1.5655          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4375          4.3406          4.3632
v  Pressure                 -36.43          360.02           87.65          169.85
v  r11                   0.0010592        0.081974        0.013072        0.018285
v  r22                   0.0011112        0.082628        0.013352        0.018645
v  r33                   0.0016351          0.1743        0.027247        0.037205
v  r12                    -0.01066        0.013609     -0.00023379     -0.00030929
v  r13                   -0.045558        0.052795      9.3058e-05       0.0010137
v  r23                   -0.046713         0.05125      3.0334e-05      0.00057452
v  epsilon                0.068894          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099179      0.00092475       0.0017426
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2787         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8787          0.7135         0.85283


 TIME FOR THE TIME STEP            10402:        0.84419E+02

===============================================================


 INSTANT    0.104030000E-01   TIME STEP NUMBER           10403
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.499504656E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.271655742E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.318015568E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.206350275E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.521419743E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81228E-03   0.45238E-02 0.19936E+01 
c  Velocity[X]                                      0.13855E-03 
c  Velocity[Y]                                      0.12872E-03 
c  Velocity[Z]                                      0.42565E-02 
c  Pressure     0.36590E-04     131   0.93049E-02   0.25810E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58644E-08   0.16541E-08 0.99942E-01 
c  r22          0.10851E-01      13   0.48574E-08   0.18346E-08 0.10171E+00 
c  r33          0.21859E-01      15   0.62297E-08   0.12592E-07 0.12768E+00 
c  r12          0.93855E-03      18   0.55265E-08   0.29858E-09 0.60839E+00 
c  r13          0.46673E-02      18   0.64888E-08   0.14923E-08 0.19928E+00 
c  r23          0.39974E-02      19   0.60102E-08   0.12877E-08 0.19970E+00 
c  epsilon      0.10970E+02      11   0.35065E-08   0.98214E-02 0.16434E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.84230E-02 0.43342E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63395         0.61359       0.0052558       0.0015072
v  Velocity[Y]            -0.57354         0.54421       0.0030805      0.00087336
v  Velocity[Z]              1.5653          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4375          4.3406          4.3632
v  Pressure                -36.396          360.02           87.65          169.85
v  r11                   0.0010592        0.081966        0.013072        0.018285
v  r22                   0.0011112        0.082628        0.013352        0.018645
v  r33                   0.0016351         0.17433        0.027247        0.037205
v  r12                   -0.010657        0.013605     -0.00023379     -0.00030929
v  r13                   -0.045556        0.052795      9.3059e-05       0.0010137
v  r23                   -0.046713        0.051248      3.0334e-05      0.00057452
v  epsilon                0.068895          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099178      0.00092475       0.0017426
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2783         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8783          0.7135         0.85283


 TIME FOR THE TIME STEP            10403:        0.84869E+02

===============================================================


 INSTANT    0.104040000E-01   TIME STEP NUMBER           10404
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.741703962E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.794583259E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.157566996E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.180605746E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119092764E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81291E-03   0.45271E-02 0.19926E+01 
c  Velocity[X]                                      0.13863E-03 
c  Velocity[Y]                                      0.12848E-03 
c  Velocity[Z]                                      0.42600E-02 
c  Pressure     0.36475E-04     133   0.92915E-02   0.25729E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54784E-08   0.16588E-08 0.10048E+00 
c  r22          0.10851E-01      13   0.52878E-08   0.18254E-08 0.10175E+00 
c  r33          0.21859E-01      15   0.58962E-08   0.12541E-07 0.12790E+00 
c  r12          0.93855E-03      18   0.63078E-08   0.30368E-09 0.61095E+00 
c  r13          0.46674E-02      19   0.55549E-08   0.14941E-08 0.19942E+00 
c  r23          0.39974E-02      19   0.71917E-08   0.12901E-08 0.20057E+00 
c  epsilon      0.10970E+02      11   0.33808E-08   0.96307E-02 0.16366E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.84402E-02 0.43321E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63401         0.61359       0.0052557       0.0015073
v  Velocity[Y]            -0.57361         0.54439       0.0030805      0.00087337
v  Velocity[Z]              1.5655          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4375          4.3406          4.3632
v  Pressure                -36.437          360.07          87.703          169.91
v  r11                   0.0010592        0.081964        0.013072        0.018285
v  r22                   0.0011112        0.082628        0.013352        0.018645
v  r33                   0.0016351          0.1743        0.027247        0.037205
v  r12                   -0.010657        0.013605     -0.00023379     -0.00030929
v  r13                   -0.045554        0.052795      9.3059e-05       0.0010137
v  r23                   -0.046713         0.05128      3.0336e-05      0.00057452
v  epsilon                0.068896          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099177      0.00092475       0.0017426
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2788         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8788          0.7135         0.85283


 TIME FOR THE TIME STEP            10404:        0.84242E+02

===============================================================


 INSTANT    0.104050000E-01   TIME STEP NUMBER           10405
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.450825898E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.238372412E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.346250014E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178865498E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.508489002E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81243E-03   0.45348E-02 0.19924E+01 
c  Velocity[X]                                      0.13815E-03 
c  Velocity[Y]                                      0.12925E-03 
c  Velocity[Z]                                      0.42674E-02 
c  Pressure     0.36304E-04     132   0.92417E-02   0.25607E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55332E-08   0.16939E-08 0.10112E+00 
c  r22          0.10851E-01      13   0.49257E-08   0.18437E-08 0.10190E+00 
c  r33          0.21859E-01      15   0.56058E-08   0.12774E-07 0.12862E+00 
c  r12          0.93855E-03      18   0.63978E-08   0.30045E-09 0.60929E+00 
c  r13          0.46674E-02      18   0.69253E-08   0.14809E-08 0.19913E+00 
c  r23          0.39974E-02      19   0.64552E-08   0.13091E-08 0.20206E+00 
c  epsilon      0.10970E+02      11   0.34795E-08   0.10383E-01 0.17219E+00 
c  TempC        0.25716E+06      16   0.15100E-04   0.83812E-02 0.43194E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63399         0.61357       0.0052557       0.0015072
v  Velocity[Y]            -0.57373         0.54406       0.0030805      0.00087334
v  Velocity[Z]              1.5655          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4375          4.3406          4.3632
v  Pressure                -36.375          360.06          87.666          169.88
v  r11                   0.0010592        0.081965        0.013072        0.018285
v  r22                   0.0011112        0.082625        0.013352        0.018645
v  r33                   0.0016351         0.17427        0.027247        0.037205
v  r12                   -0.010656        0.013605     -0.00023379     -0.00030929
v  r13                   -0.045558        0.052796      9.3059e-05       0.0010137
v  r23                   -0.046712        0.051275      3.0337e-05      0.00057452
v  epsilon                0.068897          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099177      0.00092475       0.0017426
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2786         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8786          0.7135         0.85283


 TIME FOR THE TIME STEP            10405:        0.88092E+02

===============================================================


 INSTANT    0.104060000E-01   TIME STEP NUMBER           10406
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.128073564E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.242478672E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.159638464E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.457541617E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.303172243E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81240E-03   0.45310E-02 0.19940E+01 
c  Velocity[X]                                      0.13808E-03 
c  Velocity[Y]                                      0.12890E-03 
c  Velocity[Z]                                      0.42640E-02 
c  Pressure     0.36205E-04     133   0.92164E-02   0.25538E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55405E-08   0.16384E-08 0.10022E+00 
c  r22          0.10851E-01      13   0.48741E-08   0.18466E-08 0.10225E+00 
c  r33          0.21859E-01      15   0.55264E-08   0.12447E-07 0.12775E+00 
c  r12          0.93855E-03      18   0.60629E-08   0.30283E-09 0.61305E+00 
c  r13          0.46674E-02      18   0.70899E-08   0.15007E-08 0.20025E+00 
c  r23          0.39974E-02      19   0.56793E-08   0.12682E-08 0.19936E+00 
c  epsilon      0.10970E+02      11   0.33440E-08   0.95448E-02 0.16221E+00 
c  TempC        0.25716E+06      16   0.15177E-04   0.84316E-02 0.43328E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63405         0.61357       0.0052558       0.0015072
v  Velocity[Y]            -0.57362         0.54411       0.0030806      0.00087339
v  Velocity[Z]              1.5656          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4375          4.3406          4.3632
v  Pressure                -36.411          359.96          87.628          169.81
v  r11                   0.0010592        0.081968        0.013072        0.018285
v  r22                   0.0011112        0.082626        0.013352        0.018645
v  r33                   0.0016351         0.17428        0.027247        0.037205
v  r12                   -0.010656        0.013595     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052796      9.3061e-05       0.0010137
v  r23                   -0.046711        0.051261      3.0338e-05      0.00057453
v  epsilon                0.068898          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9939e-05       0.0099176      0.00092475       0.0017426
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2789         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8789          0.7135         0.85283


 TIME FOR THE TIME STEP            10406:        0.85944E+02

===============================================================


 INSTANT    0.104070000E-01   TIME STEP NUMBER           10407
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183541230E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.461253176E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.388205729E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.315955098E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.214331514E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81246E-03   0.45293E-02 0.19934E+01 
c  Velocity[X]                                      0.13866E-03 
c  Velocity[Y]                                      0.12944E-03 
c  Velocity[Z]                                      0.42612E-02 
c  Pressure     0.36552E-04     132   0.93042E-02   0.25783E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53530E-08   0.16181E-08 0.99142E-01 
c  r22          0.10851E-01      13   0.50613E-08   0.18269E-08 0.10126E+00 
c  r33          0.21859E-01      15   0.61947E-08   0.12413E-07 0.12688E+00 
c  r12          0.93855E-03      18   0.68057E-08   0.28847E-09 0.60166E+00 
c  r13          0.46674E-02      19   0.54553E-08   0.14971E-08 0.19881E+00 
c  r23          0.39974E-02      19   0.60038E-08   0.12694E-08 0.19787E+00 
c  epsilon      0.10970E+02      11   0.33287E-08   0.98990E-02 0.16402E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.84701E-02 0.43422E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63406         0.61358       0.0052558       0.0015073
v  Velocity[Y]            -0.57361         0.54427       0.0030806      0.00087344
v  Velocity[Z]              1.5657          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4375          4.3406          4.3632
v  Pressure                -36.386          360.08          87.685           169.9
v  r11                   0.0010593        0.081973        0.013072        0.018285
v  r22                   0.0011112        0.082627        0.013352        0.018645
v  r33                   0.0016351         0.17431        0.027247        0.037205
v  r12                   -0.010652        0.013592     -0.00023379     -0.00030929
v  r13                   -0.045554        0.052793      9.3062e-05       0.0010137
v  r23                   -0.046709        0.051281      3.0339e-05      0.00057453
v  epsilon                0.068899          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099176      0.00092475       0.0017426
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2791         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8791          0.7135         0.85283


 TIME FOR THE TIME STEP            10407:        0.83868E+02

===============================================================


 INSTANT    0.104080000E-01   TIME STEP NUMBER           10408
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.231547087E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160708644E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.314826067E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.175823532E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.417688732E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81344E-03   0.44848E-02 0.19841E+01 
c  Velocity[X]                                      0.13859E-03 
c  Velocity[Y]                                      0.12870E-03 
c  Velocity[Z]                                      0.42176E-02 
c  Pressure     0.36470E-04     131   0.92806E-02   0.25725E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59840E-08   0.16459E-08 0.99972E-01 
c  r22          0.10851E-01      13   0.50359E-08   0.18265E-08 0.10166E+00 
c  r33          0.21859E-01      15   0.59232E-08   0.12565E-07 0.12813E+00 
c  r12          0.93855E-03      18   0.67309E-08   0.29600E-09 0.60560E+00 
c  r13          0.46674E-02      19   0.58205E-08   0.14879E-08 0.19945E+00 
c  r23          0.39974E-02      19   0.63471E-08   0.12862E-08 0.19996E+00 
c  epsilon      0.10970E+02      11   0.32364E-08   0.99598E-02 0.16498E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.83944E-02 0.43235E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61355       0.0052557       0.0015072
v  Velocity[Y]            -0.57361          0.5444       0.0030806      0.00087337
v  Velocity[Z]              1.5655          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4375          4.3406          4.3632
v  Pressure                 -36.43          359.98          87.618          169.82
v  r11                   0.0010593        0.081977        0.013072        0.018285
v  r22                   0.0011112        0.082628        0.013352        0.018645
v  r33                   0.0016351         0.17435        0.027247        0.037205
v  r12                   -0.010653        0.013591     -0.00023379     -0.00030929
v  r13                   -0.045557        0.052795      9.3062e-05       0.0010137
v  r23                   -0.046708        0.051256      3.0339e-05      0.00057453
v  epsilon                0.068901          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099176      0.00092475       0.0017426
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2786         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8786          0.7135         0.85283


 TIME FOR THE TIME STEP            10408:        0.83990E+02

===============================================================


 INSTANT    0.104090000E-01   TIME STEP NUMBER           10409
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.156338499E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138024646E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.356679039E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.617125552E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125856075E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81209E-03   0.45454E-02 0.19952E+01 
c  Velocity[X]                                      0.13885E-03 
c  Velocity[Y]                                      0.12872E-03 
c  Velocity[Z]                                      0.42779E-02 
c  Pressure     0.36506E-04     133   0.92942E-02   0.25750E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59932E-08   0.16158E-08 0.99490E-01 
c  r22          0.10851E-01      13   0.46956E-08   0.18197E-08 0.10139E+00 
c  r33          0.21859E-01      15   0.66570E-08   0.12346E-07 0.12697E+00 
c  r12          0.93855E-03      18   0.63789E-08   0.29547E-09 0.60342E+00 
c  r13          0.46674E-02      19   0.67793E-08   0.14915E-08 0.19918E+00 
c  r23          0.39974E-02      19   0.63725E-08   0.12610E-08 0.19834E+00 
c  epsilon      0.10970E+02      11   0.32522E-08   0.96176E-02 0.16259E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.84421E-02 0.43297E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393         0.61363       0.0052558       0.0015072
v  Velocity[Y]            -0.57372         0.54419       0.0030806      0.00087339
v  Velocity[Z]              1.5655          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4375          4.3406          4.3632
v  Pressure                -36.379          360.03           87.65          169.85
v  r11                   0.0010593        0.081983        0.013072        0.018285
v  r22                   0.0011112        0.082629        0.013352        0.018645
v  r33                   0.0016352         0.17432        0.027247        0.037205
v  r12                   -0.010653        0.013585     -0.00023379     -0.00030929
v  r13                   -0.045556        0.052793      9.3063e-05       0.0010137
v  r23                   -0.046707         0.05125       3.034e-05      0.00057453
v  epsilon                0.068902           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9951e-05       0.0099174      0.00092475       0.0017426
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2777         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8777          0.7135         0.85283


 TIME FOR THE TIME STEP            10409:        0.81529E+02

===============================================================


 INSTANT    0.104100000E-01   TIME STEP NUMBER           10410
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201099965E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.143031279E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934907E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.104239447E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.744387317E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.275403950E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81251E-03   0.45713E-02 0.20012E+01 
c  Velocity[X]                                      0.13974E-03 
c  Velocity[Y]                                      0.12922E-03 
c  Velocity[Z]                                      0.43023E-02 
c  Pressure     0.36847E-04     131   0.93760E-02   0.25991E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.63305E-08   0.16203E-08 0.99523E-01 
c  r22          0.10851E-01      13   0.49888E-08   0.18176E-08 0.10174E+00 
c  r33          0.21859E-01      15   0.68098E-08   0.12435E-07 0.12758E+00 
c  r12          0.93855E-03      18   0.66405E-08   0.30137E-09 0.60775E+00 
c  r13          0.46674E-02      20   0.61768E-08   0.15089E-08 0.20109E+00 
c  r23          0.39974E-02      20   0.57494E-08   0.12641E-08 0.19908E+00 
c  epsilon      0.10970E+02      11   0.33646E-08   0.98579E-02 0.16541E+00 
c  TempC        0.25716E+06      16   0.15122E-04   0.84215E-02 0.43301E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63399         0.61358       0.0052558       0.0015073
v  Velocity[Y]            -0.57368         0.54433       0.0030806      0.00087342
v  Velocity[Z]              1.5654          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4375          4.3406          4.3632
v  Pressure                -36.425             360          87.652          169.84
v  r11                   0.0010593        0.081983        0.013072        0.018285
v  r22                   0.0011113         0.08263        0.013352        0.018645
v  r33                   0.0016352         0.17429        0.027247        0.037205
v  r12                   -0.010651        0.013583     -0.00023379     -0.00030929
v  r13                   -0.045554        0.052793      9.3064e-05       0.0010137
v  r23                   -0.046707        0.051248      3.0341e-05      0.00057453
v  epsilon                0.068903          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9955e-05       0.0099175      0.00092475       0.0017426
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2771         0.11441         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8771          0.7135         0.85283


 TIME FOR THE TIME STEP            10410:        0.83299E+02

===============================================================


 INSTANT    0.104110000E-01   TIME STEP NUMBER           10411
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.409505805E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.246069088E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.766162478E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.281016304E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.759744200E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81217E-03   0.45209E-02 0.19927E+01 
c  Velocity[X]                                      0.13812E-03 
c  Velocity[Y]                                      0.12935E-03 
c  Velocity[Z]                                      0.42535E-02 
c  Pressure     0.36343E-04     131   0.92522E-02   0.25635E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.66680E-08   0.17252E-08 0.10213E+00 
c  r22          0.10851E-01      13   0.54804E-08   0.18960E-08 0.10365E+00 
c  r33          0.21859E-01      15   0.62117E-08   0.13115E-07 0.13098E+00 
c  r12          0.93856E-03      18   0.69653E-08   0.31557E-09 0.62223E+00 
c  r13          0.46674E-02      19   0.72885E-08   0.15318E-08 0.20262E+00 
c  r23          0.39974E-02      20   0.55860E-08   0.13611E-08 0.20682E+00 
c  epsilon      0.10970E+02      11   0.34316E-08   0.10508E-01 0.17379E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.83951E-02 0.43265E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63405         0.61357       0.0052559       0.0015073
v  Velocity[Y]            -0.57369         0.54402       0.0030806      0.00087343
v  Velocity[Z]              1.5653          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4375          4.3406          4.3632
v  Pressure                -36.425          360.04          87.663          169.87
v  r11                   0.0010593        0.081987        0.013072        0.018285
v  r22                   0.0011113         0.08263        0.013352        0.018645
v  r33                   0.0016352          0.1743        0.027247        0.037205
v  r12                   -0.010652        0.013577     -0.00023379     -0.00030929
v  r13                   -0.045557        0.052791      9.3064e-05       0.0010137
v  r23                   -0.046706        0.051245      3.0341e-05      0.00057453
v  epsilon                0.068904          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.996e-05       0.0099175      0.00092476       0.0017426
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2769         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8769          0.7135         0.85283


 TIME FOR THE TIME STEP            10411:        0.84246E+02

===============================================================


 INSTANT    0.104120000E-01   TIME STEP NUMBER           10412
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.107264453E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.386812432E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.534782075E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.292282134E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.439400354E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81299E-03   0.45080E-02 0.19896E+01 
c  Velocity[X]                                      0.13828E-03 
c  Velocity[Y]                                      0.12898E-03 
c  Velocity[Z]                                      0.42408E-02 
c  Pressure     0.36268E-04     132   0.92385E-02   0.25581E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.67823E-08   0.16348E-08 0.10028E+00 
c  r22          0.10851E-01      13   0.51939E-08   0.18347E-08 0.10233E+00 
c  r33          0.21859E-01      15   0.60116E-08   0.12451E-07 0.12841E+00 
c  r12          0.93856E-03      19   0.57990E-08   0.29612E-09 0.60876E+00 
c  r13          0.46674E-02      19   0.73496E-08   0.14844E-08 0.20062E+00 
c  r23          0.39974E-02      19   0.74253E-08   0.12757E-08 0.20078E+00 
c  epsilon      0.10970E+02      11   0.35043E-08   0.96791E-02 0.16451E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.83991E-02 0.43266E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63404         0.61359       0.0052559       0.0015072
v  Velocity[Y]            -0.57356         0.54408       0.0030807      0.00087342
v  Velocity[Z]              1.5655          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4375          4.3406          4.3632
v  Pressure                -36.436          359.99          87.647          169.84
v  r11                   0.0010593        0.081992        0.013072        0.018285
v  r22                   0.0011113        0.082631        0.013352        0.018645
v  r33                   0.0016352         0.17433        0.027247        0.037205
v  r12                   -0.010654         0.01357     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052792      9.3064e-05       0.0010137
v  r23                   -0.046705         0.05125      3.0341e-05      0.00057453
v  epsilon                0.068905          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9961e-05       0.0099172      0.00092476       0.0017426
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017847           5.277         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.877          0.7135         0.85283


 TIME FOR THE TIME STEP            10412:        0.82586E+02

===============================================================


 INSTANT    0.104130000E-01   TIME STEP NUMBER           10413
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.389819585E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.112867327E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.230691530E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.861542467E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.339116033E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81202E-03   0.45136E-02 0.19886E+01 
c  Velocity[X]                                      0.13898E-03 
c  Velocity[Y]                                      0.12992E-03 
c  Velocity[Z]                                      0.42447E-02 
c  Pressure     0.36433E-04     133   0.92730E-02   0.25698E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60699E-08   0.16337E-08 0.10013E+00 
c  r22          0.10851E-01      13   0.50589E-08   0.18082E-08 0.10135E+00 
c  r33          0.21859E-01      15   0.64929E-08   0.12391E-07 0.12748E+00 
c  r12          0.93856E-03      18   0.68019E-08   0.29403E-09 0.60478E+00 
c  r13          0.46674E-02      20   0.63951E-08   0.14681E-08 0.19842E+00 
c  r23          0.39974E-02      20   0.61115E-08   0.12663E-08 0.19987E+00 
c  epsilon      0.10970E+02      11   0.34979E-08   0.97665E-02 0.16357E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.84613E-02 0.43432E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63407         0.61358       0.0052559       0.0015072
v  Velocity[Y]            -0.57355          0.5442       0.0030807      0.00087345
v  Velocity[Z]              1.5655          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4375          4.3406          4.3632
v  Pressure                -36.382          360.06          87.664          169.88
v  r11                   0.0010593        0.082004        0.013072        0.018285
v  r22                   0.0011113        0.082628        0.013352        0.018645
v  r33                   0.0016352         0.17431        0.027247        0.037205
v  r12                   -0.010654        0.013572     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052794      9.3065e-05       0.0010137
v  r23                   -0.046704        0.051273      3.0343e-05      0.00057453
v  epsilon                0.068906          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9961e-05       0.0099172      0.00092476       0.0017426
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2762         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8762          0.7135         0.85283


 TIME FOR THE TIME STEP            10413:        0.81468E+02

===============================================================


 INSTANT    0.104140000E-01   TIME STEP NUMBER           10414
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.144226669E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.293984512E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.502411466E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125516678E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319926045E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81270E-03   0.45284E-02 0.19938E+01 
c  Velocity[X]                                      0.13886E-03 
c  Velocity[Y]                                      0.12943E-03 
c  Velocity[Z]                                      0.42601E-02 
c  Pressure     0.36669E-04     133   0.93263E-02   0.25865E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.61472E-08   0.16288E-08 0.99869E-01 
c  r22          0.10851E-01      13   0.55649E-08   0.18326E-08 0.10172E+00 
c  r33          0.21859E-01      15   0.61608E-08   0.12541E-07 0.12791E+00 
c  r12          0.93856E-03      19   0.58085E-08   0.29987E-09 0.60775E+00 
c  r13          0.46674E-02      20   0.58788E-08   0.15097E-08 0.19972E+00 
c  r23          0.39974E-02      20   0.56941E-08   0.12757E-08 0.20034E+00 
c  epsilon      0.10970E+02      11   0.33806E-08   0.99803E-02 0.16588E+00 
c  TempC        0.25716E+06      16   0.15167E-04   0.84123E-02 0.43236E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63414         0.61352       0.0052558       0.0015073
v  Velocity[Y]             -0.5734         0.54437       0.0030806      0.00087341
v  Velocity[Z]              1.5653          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4375          4.3406          4.3632
v  Pressure                -36.444          360.06          87.696           169.9
v  r11                   0.0010593        0.082007        0.013072        0.018285
v  r22                   0.0011113         0.08263        0.013352        0.018645
v  r33                   0.0016352         0.17428        0.027247        0.037205
v  r12                   -0.010657        0.013577     -0.00023379     -0.00030929
v  r13                   -0.045556        0.052796      9.3065e-05       0.0010137
v  r23                   -0.046704        0.051272      3.0344e-05      0.00057453
v  epsilon                0.068908          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9961e-05       0.0099173      0.00092476       0.0017426
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2766         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8766          0.7135         0.85284


 TIME FOR THE TIME STEP            10414:        0.88821E+02

===============================================================


 INSTANT    0.104150000E-01   TIME STEP NUMBER           10415
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.156135924E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.914440361E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.166085587E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.460821103E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.149850804E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81210E-03   0.45301E-02 0.19945E+01 
c  Velocity[X]                                      0.13859E-03 
c  Velocity[Y]                                      0.12864E-03 
c  Velocity[Z]                                      0.42629E-02 
c  Pressure     0.36680E-04     132   0.93478E-02   0.25873E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.64289E-08   0.16116E-08 0.99417E-01 
c  r22          0.10851E-01      13   0.50589E-08   0.17999E-08 0.10145E+00 
c  r33          0.21859E-01      15   0.58865E-08   0.12257E-07 0.12719E+00 
c  r12          0.93856E-03      18   0.69300E-08   0.29355E-09 0.60412E+00 
c  r13          0.46674E-02      20   0.65403E-08   0.14723E-08 0.19912E+00 
c  r23          0.39974E-02      19   0.66156E-08   0.12571E-08 0.19823E+00 
c  epsilon      0.10970E+02      11   0.32776E-08   0.95995E-02 0.16280E+00 
c  TempC        0.25716E+06      16   0.15125E-04   0.84166E-02 0.43220E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63405         0.61361       0.0052559       0.0015073
v  Velocity[Y]            -0.57347         0.54419       0.0030806      0.00087343
v  Velocity[Z]              1.5652          5.4375          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4375          4.3406          4.3632
v  Pressure                -36.404          360.05          87.675          169.88
v  r11                   0.0010593        0.082004        0.013072        0.018285
v  r22                   0.0011113         0.08263        0.013352        0.018645
v  r33                   0.0016352         0.17429        0.027247        0.037205
v  r12                   -0.010655        0.013586     -0.00023379      -0.0003093
v  r13                   -0.045554        0.052795      9.3066e-05       0.0010137
v  r23                   -0.046704         0.05127      3.0345e-05      0.00057453
v  epsilon                0.068909          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9961e-05       0.0099174      0.00092476       0.0017426
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2774         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8774          0.7135         0.85283


 TIME FOR THE TIME STEP            10415:        0.14469E+03

===============================================================


 INSTANT    0.104160000E-01   TIME STEP NUMBER           10416
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.206326921E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.655202472E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.885173362E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242792373E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110036132E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81255E-03   0.45434E-02 0.19944E+01 
c  Velocity[X]                                      0.13899E-03 
c  Velocity[Y]                                      0.12880E-03 
c  Velocity[Z]                                      0.42756E-02 
c  Pressure     0.36346E-04     133   0.92555E-02   0.25637E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.70087E-08   0.16396E-08 0.10009E+00 
c  r22          0.10851E-01      13   0.50182E-08   0.18336E-08 0.10169E+00 
c  r33          0.21859E-01      15   0.72901E-08   0.12472E-07 0.12750E+00 
c  r12          0.93856E-03      18   0.66148E-08   0.29841E-09 0.60953E+00 
c  r13          0.46674E-02      20   0.56094E-08   0.15130E-08 0.20033E+00 
c  r23          0.39974E-02      19   0.69421E-08   0.12768E-08 0.19941E+00 
c  epsilon      0.10970E+02      11   0.33026E-08   0.98418E-02 0.16440E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.84053E-02 0.43254E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61359       0.0052558       0.0015072
v  Velocity[Y]            -0.57338         0.54432       0.0030806      0.00087341
v  Velocity[Z]              1.5652          5.4375          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4375          4.3406          4.3632
v  Pressure                -36.413          360.01          87.641          169.85
v  r11                   0.0010593        0.082005        0.013072        0.018285
v  r22                   0.0011113        0.082631        0.013352        0.018645
v  r33                   0.0016352         0.17432        0.027247        0.037205
v  r12                   -0.010654        0.013584     -0.00023379      -0.0003093
v  r13                   -0.045553        0.052797      9.3067e-05       0.0010137
v  r23                   -0.046705        0.051285      3.0345e-05      0.00057453
v  epsilon                 0.06891          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099175      0.00092476       0.0017426
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2772         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8772          0.7135         0.85283


 TIME FOR THE TIME STEP            10416:        0.12611E+03

===============================================================


 INSTANT    0.104170000E-01   TIME STEP NUMBER           10417
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.650336537E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.121265847E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.527438973E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.139868261E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.289744435E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81153E-03   0.45167E-02 0.19890E+01 
c  Velocity[X]                                      0.13839E-03 
c  Velocity[Y]                                      0.12824E-03 
c  Velocity[Z]                                      0.42500E-02 
c  Pressure     0.36473E-04     131   0.92795E-02   0.25727E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.70981E-08   0.16646E-08 0.10101E+00 
c  r22          0.10851E-01      13   0.48973E-08   0.18329E-08 0.10198E+00 
c  r33          0.21859E-01      15   0.68469E-08   0.12647E-07 0.12887E+00 
c  r12          0.93856E-03      18   0.65999E-08   0.31603E-09 0.61553E+00 
c  r13          0.46674E-02      19   0.72866E-08   0.15052E-08 0.20060E+00 
c  r23          0.39974E-02      19   0.64678E-08   0.13291E-08 0.20416E+00 
c  epsilon      0.10970E+02      11   0.32982E-08   0.10099E-01 0.16999E+00 
c  TempC        0.25716E+06      16   0.15121E-04   0.83943E-02 0.43244E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63403         0.61357       0.0052558       0.0015072
v  Velocity[Y]            -0.57348         0.54426       0.0030806      0.00087339
v  Velocity[Z]              1.5653          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4375          4.3406          4.3632
v  Pressure                -36.431          360.01          87.645          169.84
v  r11                   0.0010593        0.082003        0.013072        0.018285
v  r22                   0.0011113        0.082631        0.013352        0.018645
v  r33                   0.0016353         0.17435        0.027247        0.037205
v  r12                   -0.010653        0.013591     -0.00023379      -0.0003093
v  r13                   -0.045558        0.052798      9.3068e-05       0.0010137
v  r23                   -0.046705         0.05127      3.0346e-05      0.00057453
v  epsilon                0.068911          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099177      0.00092476       0.0017426
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2768         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8768          0.7135         0.85284


 TIME FOR THE TIME STEP            10417:        0.17150E+03

===============================================================


 INSTANT    0.104180000E-01   TIME STEP NUMBER           10418
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.686296129E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.351611814E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.454476943E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935015E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.651913706E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.254335392E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81267E-03   0.45426E-02 0.19989E+01 
c  Velocity[X]                                      0.13903E-03 
c  Velocity[Y]                                      0.13013E-03 
c  Velocity[Z]                                      0.42735E-02 
c  Pressure     0.36431E-04     133   0.92779E-02   0.25698E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.68528E-08   0.16368E-08 0.10016E+00 
c  r22          0.10851E-01      13   0.47624E-08   0.18377E-08 0.10185E+00 
c  r33          0.21859E-01      15   0.65538E-08   0.12594E-07 0.12816E+00 
c  r12          0.93856E-03      18   0.63199E-08   0.29996E-09 0.60766E+00 
c  r13          0.46674E-02      19   0.66280E-08   0.14884E-08 0.19975E+00 
c  r23          0.39974E-02      19   0.68703E-08   0.12844E-08 0.20024E+00 
c  epsilon      0.10970E+02      11   0.34805E-08   0.10072E-01 0.16738E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.84045E-02 0.43311E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63412          0.6136       0.0052559       0.0015073
v  Velocity[Y]            -0.57354         0.54436       0.0030806       0.0008734
v  Velocity[Z]              1.5651          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4375          4.3406          4.3632
v  Pressure                -36.469          360.01          87.641          169.84
v  r11                   0.0010593           0.082        0.013072        0.018285
v  r22                   0.0011113        0.082631        0.013352        0.018645
v  r33                   0.0016353         0.17432        0.027247        0.037205
v  r12                   -0.010654        0.013599     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052798      9.3068e-05       0.0010137
v  r23                   -0.046705        0.051254      3.0346e-05      0.00057453
v  epsilon                0.068912          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099178      0.00092476       0.0017426
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2768         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8768          0.7135         0.85283


 TIME FOR THE TIME STEP            10418:        0.12773E+03

===============================================================


 INSTANT    0.104190000E-01   TIME STEP NUMBER           10419
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.683168993E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.295298337E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.207332568E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.384672311E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.428015156E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81244E-03   0.45288E-02 0.19939E+01 
c  Velocity[X]                                      0.13891E-03 
c  Velocity[Y]                                      0.12904E-03 
c  Velocity[Z]                                      0.42609E-02 
c  Pressure     0.36334E-04     132   0.92486E-02   0.25629E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.61688E-08   0.16067E-08 0.99302E-01 
c  r22          0.10851E-01      13   0.47227E-08   0.17746E-08 0.10077E+00 
c  r33          0.21859E-01      15   0.58442E-08   0.12101E-07 0.12626E+00 
c  r12          0.93856E-03      18   0.57686E-08   0.30089E-09 0.60837E+00 
c  r13          0.46674E-02      19   0.67118E-08   0.14706E-08 0.19879E+00 
c  r23          0.39974E-02      19   0.60206E-08   0.12560E-08 0.19800E+00 
c  epsilon      0.10970E+02      11   0.34902E-08   0.93213E-02 0.16041E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.84475E-02 0.43316E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63411         0.61361       0.0052559       0.0015073
v  Velocity[Y]             -0.5737         0.54444       0.0030807      0.00087345
v  Velocity[Z]              1.5654          5.4376          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4376          4.3406          4.3632
v  Pressure                -36.406          360.01          87.634          169.84
v  r11                   0.0010593           0.082        0.013072        0.018285
v  r22                   0.0011113         0.08263        0.013352        0.018645
v  r33                   0.0016353         0.17428        0.027247        0.037205
v  r12                   -0.010654          0.0136     -0.00023379     -0.00030929
v  r13                   -0.045554        0.052795      9.3068e-05       0.0010137
v  r23                   -0.046706         0.05127      3.0347e-05      0.00057453
v  epsilon                0.068913          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099176      0.00092477       0.0017426
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2771         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8771          0.7135         0.85284


 TIME FOR THE TIME STEP            10419:        0.16235E+03

===============================================================


 INSTANT    0.104200000E-01   TIME STEP NUMBER           10420
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.544526990E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.238167436E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.542073621E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116571791E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.148894283E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81332E-03   0.44926E-02 0.19838E+01 
c  Velocity[X]                                      0.13786E-03 
c  Velocity[Y]                                      0.12807E-03 
c  Velocity[Z]                                      0.42267E-02 
c  Pressure     0.36588E-04     133   0.93174E-02   0.25809E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57337E-08   0.16023E-08 0.99162E-01 
c  r22          0.10851E-01      13   0.48612E-08   0.17980E-08 0.10139E+00 
c  r33          0.21859E-01      15   0.53037E-08   0.12269E-07 0.12704E+00 
c  r12          0.93856E-03      18   0.58615E-08   0.29606E-09 0.60452E+00 
c  r13          0.46674E-02      19   0.64824E-08   0.14774E-08 0.19928E+00 
c  r23          0.39974E-02      19   0.72547E-08   0.12487E-08 0.19818E+00 
c  epsilon      0.10970E+02      11   0.33141E-08   0.97074E-02 0.16409E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.83785E-02 0.43190E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63408         0.61355       0.0052558       0.0015073
v  Velocity[Y]            -0.57367         0.54423       0.0030806       0.0008734
v  Velocity[Z]              1.5655          5.4375          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4375          4.3406          4.3632
v  Pressure                -36.498          360.03          87.662          169.86
v  r11                   0.0010593        0.081995        0.013072        0.018285
v  r22                   0.0011113         0.08263        0.013352        0.018645
v  r33                   0.0016353         0.17428        0.027247        0.037205
v  r12                   -0.010659        0.013603     -0.00023379     -0.00030929
v  r13                   -0.045556        0.052796      9.3069e-05       0.0010137
v  r23                   -0.046706        0.051265      3.0347e-05      0.00057453
v  epsilon                0.068915          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9955e-05       0.0099175      0.00092477       0.0017426
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017846           5.278         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.878          0.7135         0.85283


 TIME FOR THE TIME STEP            10420:        0.12645E+03

===============================================================


 INSTANT    0.104210000E-01   TIME STEP NUMBER           10421
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285520690E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.205600662E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.124210413E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.748661144E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190890195E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81232E-03   0.45530E-02 0.19985E+01 
c  Velocity[X]                                      0.13832E-03 
c  Velocity[Y]                                      0.12895E-03 
c  Velocity[Z]                                      0.42857E-02 
c  Pressure     0.36390E-04     131   0.92704E-02   0.25668E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54460E-08   0.16176E-08 0.99921E-01 
c  r22          0.10851E-01      13   0.50647E-08   0.17999E-08 0.10152E+00 
c  r33          0.21859E-01      15   0.55263E-08   0.12281E-07 0.12736E+00 
c  r12          0.93856E-03      18   0.58638E-08   0.29737E-09 0.60632E+00 
c  r13          0.46674E-02      19   0.61628E-08   0.14718E-08 0.19873E+00 
c  r23          0.39974E-02      19   0.61208E-08   0.12665E-08 0.19988E+00 
c  epsilon      0.10970E+02      11   0.34109E-08   0.94162E-02 0.16153E+00 
c  TempC        0.25716E+06      16   0.15185E-04   0.84509E-02 0.43376E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63411          0.6136        0.005256       0.0015073
v  Velocity[Y]            -0.57371         0.54429       0.0030807      0.00087344
v  Velocity[Z]              1.5654          5.4376          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4376          4.3406          4.3632
v  Pressure                -36.445          360.03          87.639          169.85
v  r11                   0.0010593        0.081989        0.013072        0.018285
v  r22                   0.0011113        0.082625        0.013352        0.018645
v  r33                   0.0016353         0.17431        0.027247        0.037205
v  r12                   -0.010659        0.013606     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052798       9.307e-05       0.0010137
v  r23                   -0.046706        0.051256      3.0348e-05      0.00057453
v  epsilon                0.068916          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9954e-05       0.0099174      0.00092477       0.0017426
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2781         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781          0.7135         0.85283


 TIME FOR THE TIME STEP            10421:        0.20450E+03

===============================================================


 INSTANT    0.104220000E-01   TIME STEP NUMBER           10422
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.232452660E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.114223759E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.529462516E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.408919325E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.131192687E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81285E-03   0.45480E-02 0.19971E+01 
c  Velocity[X]                                      0.13916E-03 
c  Velocity[Y]                                      0.12941E-03 
c  Velocity[Z]                                      0.42794E-02 
c  Pressure     0.36482E-04     132   0.92857E-02   0.25733E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56532E-08   0.16761E-08 0.10155E+00 
c  r22          0.10851E-01      13   0.48480E-08   0.18264E-08 0.10206E+00 
c  r33          0.21859E-01      15   0.53645E-08   0.12643E-07 0.12917E+00 
c  r12          0.93856E-03      18   0.57709E-08   0.30821E-09 0.61669E+00 
c  r13          0.46674E-02      19   0.57158E-08   0.15021E-08 0.20099E+00 
c  r23          0.39974E-02      19   0.64156E-08   0.13093E-08 0.20405E+00 
c  epsilon      0.10970E+02      11   0.33229E-08   0.97768E-02 0.16507E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.84206E-02 0.43290E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63413         0.61357        0.005256       0.0015073
v  Velocity[Y]             -0.5737         0.54448       0.0030807      0.00087341
v  Velocity[Z]              1.5655          5.4376          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4376          4.3406          4.3632
v  Pressure                -36.447             360          87.625          169.83
v  r11                   0.0010593        0.081985        0.013072        0.018285
v  r22                   0.0011114        0.082627        0.013352        0.018645
v  r33                   0.0016353         0.17429        0.027247        0.037205
v  r12                   -0.010659        0.013608     -0.00023379      -0.0003093
v  r13                   -0.045554        0.052801      9.3072e-05       0.0010137
v  r23                   -0.046706        0.051248      3.0348e-05      0.00057453
v  epsilon                0.068917          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05       0.0099177      0.00092477       0.0017426
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2783         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8783          0.7135         0.85283


 TIME FOR THE TIME STEP            10422:        0.14373E+03

===============================================================


 INSTANT    0.104230000E-01   TIME STEP NUMBER           10423
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179445970E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154041893E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934912E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.345543084E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.300952583E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.335041686E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81273E-03   0.45057E-02 0.19865E+01 
c  Velocity[X]                                      0.13857E-03 
c  Velocity[Y]                                      0.12855E-03 
c  Velocity[Z]                                      0.42386E-02 
c  Pressure     0.36284E-04     132   0.92366E-02   0.25593E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52696E-08   0.17399E-08 0.10282E+00 
c  r22          0.10851E-01      13   0.47786E-08   0.18438E-08 0.10215E+00 
c  r33          0.21859E-01      14   0.68401E-08   0.13020E-07 0.13048E+00 
c  r12          0.93856E-03      18   0.59258E-08   0.30986E-09 0.61514E+00 
c  r13          0.46674E-02      19   0.56278E-08   0.14906E-08 0.20007E+00 
c  r23          0.39974E-02      19   0.57961E-08   0.13490E-08 0.20629E+00 
c  epsilon      0.10970E+02      11   0.34436E-08   0.10517E-01 0.17276E+00 
c  TempC        0.25716E+06      16   0.15094E-04   0.84252E-02 0.43340E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63414          0.6136       0.0052559       0.0015073
v  Velocity[Y]            -0.57379         0.54413       0.0030806      0.00087341
v  Velocity[Z]              1.5653          5.4376          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4376          4.3406          4.3632
v  Pressure                -36.435          360.06           87.67          169.88
v  r11                   0.0010594        0.081984        0.013072        0.018285
v  r22                   0.0011114         0.08263        0.013352        0.018645
v  r33                   0.0016353         0.17427        0.027247        0.037205
v  r12                   -0.010656        0.013602     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052799      9.3072e-05       0.0010137
v  r23                   -0.046706        0.051277       3.035e-05      0.00057453
v  epsilon                0.068918          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05       0.0099178      0.00092477       0.0017426
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2787         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8787          0.7135         0.85284


 TIME FOR THE TIME STEP            10423:        0.13575E+03

===============================================================


 INSTANT    0.104240000E-01   TIME STEP NUMBER           10424
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.137504333E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.107068064E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.224179937E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.641843830E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.590966040E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81242E-03   0.45112E-02 0.19892E+01 
c  Velocity[X]                                      0.13844E-03 
c  Velocity[Y]                                      0.12897E-03 
c  Velocity[Z]                                      0.42438E-02 
c  Pressure     0.36614E-04     132   0.93271E-02   0.25826E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52187E-08   0.16343E-08 0.10006E+00 
c  r22          0.10851E-01      13   0.49290E-08   0.18090E-08 0.10158E+00 
c  r33          0.21859E-01      15   0.50610E-08   0.12311E-07 0.12725E+00 
c  r12          0.93856E-03      18   0.57809E-08   0.29266E-09 0.60297E+00 
c  r13          0.46674E-02      18   0.71166E-08   0.14565E-08 0.19878E+00 
c  r23          0.39974E-02      19   0.58727E-08   0.12588E-08 0.19845E+00 
c  epsilon      0.10970E+02      11   0.35461E-08   0.95488E-02 0.16211E+00 
c  TempC        0.25716E+06      16   0.15172E-04   0.84387E-02 0.43322E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63409          0.6136       0.0052559       0.0015072
v  Velocity[Y]            -0.57366         0.54415       0.0030806      0.00087341
v  Velocity[Z]              1.5656          5.4376          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4376          4.3406          4.3632
v  Pressure                -36.448          360.01          87.655          169.85
v  r11                   0.0010594        0.081987        0.013072        0.018285
v  r22                   0.0011114        0.082632        0.013352        0.018645
v  r33                   0.0016353         0.17428        0.027247        0.037205
v  r12                   -0.010654          0.0136     -0.00023379     -0.00030929
v  r13                   -0.045553        0.052802      9.3073e-05       0.0010137
v  r23                   -0.046706        0.051276      3.0351e-05      0.00057453
v  epsilon                0.068919          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9951e-05       0.0099178      0.00092477       0.0017426
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2787         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8787          0.7135         0.85283


 TIME FOR THE TIME STEP            10424:        0.13608E+03

===============================================================


 INSTANT    0.104250000E-01   TIME STEP NUMBER           10425
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.475930291E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150573572E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.245158961E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.328618441E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.257669925E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81172E-03   0.45222E-02 0.19916E+01 
c  Velocity[X]                                      0.13946E-03 
c  Velocity[Y]                                      0.12855E-03 
c  Velocity[Z]                                      0.42542E-02 
c  Pressure     0.36553E-04     133   0.92973E-02   0.25783E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52855E-08   0.16542E-08 0.10090E+00 
c  r22          0.10851E-01      13   0.49022E-08   0.18003E-08 0.10178E+00 
c  r33          0.21859E-01      15   0.55446E-08   0.12386E-07 0.12826E+00 
c  r12          0.93856E-03      18   0.57264E-08   0.29898E-09 0.60875E+00 
c  r13          0.46674E-02      19   0.57371E-08   0.14628E-08 0.19862E+00 
c  r23          0.39974E-02      19   0.61082E-08   0.12942E-08 0.20148E+00 
c  epsilon      0.10970E+02      11   0.33701E-08   0.92413E-02 0.16123E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.84252E-02 0.43310E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63409          0.6136       0.0052559       0.0015073
v  Velocity[Y]            -0.57378          0.5443       0.0030806      0.00087339
v  Velocity[Z]              1.5658          5.4376          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4376          4.3406          4.3632
v  Pressure                -36.442          360.04          87.661          169.87
v  r11                   0.0010594        0.081983        0.013072        0.018285
v  r22                   0.0011114        0.082634        0.013352        0.018645
v  r33                   0.0016354         0.17431        0.027247        0.037205
v  r12                   -0.010653          0.0136     -0.00023379     -0.00030929
v  r13                   -0.045553        0.052802      9.3073e-05       0.0010137
v  r23                   -0.046705        0.051271      3.0351e-05      0.00057453
v  epsilon                 0.06892          271.29          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05       0.0099178      0.00092477       0.0017426
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2787         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8787          0.7135         0.85283


 TIME FOR THE TIME STEP            10425:        0.14130E+03

===============================================================


 INSTANT    0.104260000E-01   TIME STEP NUMBER           10426
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.220340130E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.723829944E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.475975258E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.801728249E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179511201E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81272E-03   0.45355E-02 0.19938E+01 
c  Velocity[X]                                      0.13848E-03 
c  Velocity[Y]                                      0.12868E-03 
c  Velocity[Z]                                      0.42683E-02 
c  Pressure     0.36948E-04     131   0.93968E-02   0.26062E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57767E-08   0.16515E-08 0.10025E+00 
c  r22          0.10851E-01      13   0.48343E-08   0.18594E-08 0.10259E+00 
c  r33          0.21859E-01      15   0.60138E-08   0.12714E-07 0.12850E+00 
c  r12          0.93856E-03      18   0.59455E-08   0.29866E-09 0.60744E+00 
c  r13          0.46674E-02      19   0.57184E-08   0.15026E-08 0.20044E+00 
c  r23          0.39974E-02      19   0.55013E-08   0.12938E-08 0.20062E+00 
c  epsilon      0.10970E+02      11   0.34405E-08   0.10003E-01 0.16628E+00 
c  TempC        0.25716E+06      16   0.15155E-04   0.84056E-02 0.43203E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63412         0.61357        0.005256       0.0015074
v  Velocity[Y]            -0.57374          0.5444       0.0030806      0.00087339
v  Velocity[Z]              1.5656          5.4376          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4376          4.3406          4.3632
v  Pressure                -36.483          360.07          87.681          169.89
v  r11                   0.0010594        0.081981        0.013072        0.018285
v  r22                   0.0011114        0.082636        0.013352        0.018645
v  r33                   0.0016354         0.17429        0.027247        0.037205
v  r12                   -0.010653        0.013599     -0.00023379     -0.00030929
v  r13                   -0.045556        0.052803      9.3074e-05       0.0010137
v  r23                   -0.046705         0.05127      3.0353e-05      0.00057453
v  epsilon                0.068922          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9954e-05       0.0099179      0.00092477       0.0017426
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2788         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8788          0.7135         0.85283


 TIME FOR THE TIME STEP            10426:        0.12900E+03

===============================================================


 INSTANT    0.104270000E-01   TIME STEP NUMBER           10427
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120581653E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201001517E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.149887821E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.266553601E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110021330E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81181E-03   0.45180E-02 0.19903E+01 
c  Velocity[X]                                      0.13777E-03 
c  Velocity[Y]                                      0.12895E-03 
c  Velocity[Z]                                      0.42512E-02 
c  Pressure     0.35980E-04     131   0.91551E-02   0.25379E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59453E-08   0.16752E-08 0.10078E+00 
c  r22          0.10851E-01      13   0.44947E-08   0.18597E-08 0.10225E+00 
c  r33          0.21859E-01      15   0.58137E-08   0.12767E-07 0.12876E+00 
c  r12          0.93856E-03      18   0.58841E-08   0.30191E-09 0.61042E+00 
c  r13          0.46674E-02      19   0.59943E-08   0.15056E-08 0.20057E+00 
c  r23          0.39974E-02      18   0.69591E-08   0.12895E-08 0.20162E+00 
c  epsilon      0.10970E+02      11   0.33468E-08   0.10108E-01 0.16629E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.84170E-02 0.43312E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63414         0.61359       0.0052561       0.0015073
v  Velocity[Y]            -0.57382         0.54424       0.0030807      0.00087342
v  Velocity[Z]              1.5655          5.4376          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4376          4.3406          4.3632
v  Pressure                -36.375          359.96          87.617          169.81
v  r11                   0.0010594        0.081985        0.013072        0.018285
v  r22                   0.0011114        0.082631        0.013352        0.018645
v  r33                   0.0016354         0.17427        0.027247        0.037205
v  r12                   -0.010652        0.013588     -0.00023379     -0.00030929
v  r13                   -0.045553        0.052803      9.3074e-05       0.0010137
v  r23                   -0.046705        0.051301      3.0352e-05      0.00057453
v  epsilon                0.068923          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099179      0.00092477       0.0017426
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2786         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8786          0.7135         0.85283


 TIME FOR THE TIME STEP            10427:        0.84616E+02

===============================================================


 INSTANT    0.104280000E-01   TIME STEP NUMBER           10428
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153474350E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160284509E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.336876419E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.246812757E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.448726519E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81278E-03   0.45121E-02 0.19905E+01 
c  Velocity[X]                                      0.13955E-03 
c  Velocity[Y]                                      0.12899E-03 
c  Velocity[Z]                                      0.42436E-02 
c  Pressure     0.36408E-04     131   0.92768E-02   0.25681E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53998E-08   0.16392E-08 0.10020E+00 
c  r22          0.10851E-01      13   0.46148E-08   0.18269E-08 0.10200E+00 
c  r33          0.21859E-01      16   0.60956E-08   0.12447E-07 0.12789E+00 
c  r12          0.93856E-03      18   0.60601E-08   0.29629E-09 0.60551E+00 
c  r13          0.46674E-02      19   0.71671E-08   0.14893E-08 0.20001E+00 
c  r23          0.39974E-02      19   0.51567E-08   0.12751E-08 0.20030E+00 
c  epsilon      0.10970E+02      11   0.35990E-08   0.97171E-02 0.16472E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.84773E-02 0.43470E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61359        0.005256       0.0015073
v  Velocity[Y]            -0.57376         0.54439       0.0030808      0.00087346
v  Velocity[Z]              1.5654          5.4376          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4376          4.3406          4.3632
v  Pressure                -36.461          359.99          87.638          169.83
v  r11                   0.0010594        0.081996        0.013072        0.018285
v  r22                   0.0011114        0.082633        0.013352        0.018645
v  r33                   0.0016354         0.17428        0.027248        0.037205
v  r12                   -0.010652        0.013586     -0.00023379     -0.00030929
v  r13                   -0.045552        0.052804      9.3076e-05       0.0010137
v  r23                   -0.046705        0.051296      3.0353e-05      0.00057453
v  epsilon                0.068924          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.996e-05       0.0099179      0.00092478       0.0017426
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2781         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781          0.7135         0.85283


 TIME FOR THE TIME STEP            10428:        0.82868E+02

===============================================================


 INSTANT    0.104290000E-01   TIME STEP NUMBER           10429
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.104171570E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.558703885E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.583211356E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.569152738E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.127004896E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81313E-03   0.45230E-02 0.19916E+01 
c  Velocity[X]                                      0.13750E-03 
c  Velocity[Y]                                      0.12887E-03 
c  Velocity[Z]                                      0.42566E-02 
c  Pressure     0.36471E-04     134   0.92843E-02   0.25726E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53659E-08   0.16750E-08 0.10087E+00 
c  r22          0.10851E-01      13   0.52285E-08   0.18224E-08 0.10140E+00 
c  r33          0.21859E-01      15   0.65160E-08   0.12651E-07 0.12835E+00 
c  r12          0.93856E-03      18   0.57356E-08   0.29941E-09 0.60625E+00 
c  r13          0.46674E-02      19   0.69164E-08   0.14995E-08 0.19988E+00 
c  r23          0.39974E-02      19   0.57459E-08   0.13130E-08 0.20227E+00 
c  epsilon      0.10970E+02      11   0.34603E-08   0.10322E-01 0.17151E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.83500E-02 0.43097E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61357        0.005256       0.0015073
v  Velocity[Y]            -0.57363         0.54406       0.0030808      0.00087345
v  Velocity[Z]              1.5653          5.4376          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4376          4.3406          4.3632
v  Pressure                -36.413          360.09           87.67           169.9
v  r11                   0.0010594        0.081999        0.013072        0.018285
v  r22                   0.0011114        0.082636        0.013352        0.018645
v  r33                   0.0016354          0.1743        0.027248        0.037205
v  r12                   -0.010655        0.013589     -0.00023379     -0.00030929
v  r13                   -0.045556        0.052805      9.3076e-05       0.0010137
v  r23                   -0.046705        0.051285      3.0354e-05      0.00057453
v  epsilon                0.068925          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9962e-05       0.0099179      0.00092478       0.0017426
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017846           5.277         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.877          0.7135         0.85283


 TIME FOR THE TIME STEP            10429:        0.83371E+02

===============================================================


 INSTANT    0.104300000E-01   TIME STEP NUMBER           10430
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.801475987E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.576053904E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.464184320E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294745486E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.224074744E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81152E-03   0.45607E-02 0.19980E+01 
c  Velocity[X]                                      0.13841E-03 
c  Velocity[Y]                                      0.12926E-03 
c  Velocity[Z]                                      0.42930E-02 
c  Pressure     0.36435E-04     134   0.92756E-02   0.25699E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57178E-08   0.16265E-08 0.99652E-01 
c  r22          0.10851E-01      13   0.50539E-08   0.18052E-08 0.10130E+00 
c  r33          0.21859E-01      15   0.68575E-08   0.12328E-07 0.12712E+00 
c  r12          0.93856E-03      18   0.51984E-08   0.29459E-09 0.60159E+00 
c  r13          0.46674E-02      19   0.54624E-08   0.14833E-08 0.19968E+00 
c  r23          0.39974E-02      19   0.57943E-08   0.12783E-08 0.19936E+00 
c  epsilon      0.10970E+02      11   0.34788E-08   0.95524E-02 0.16315E+00 
c  TempC        0.25716E+06      16   0.15121E-04   0.84080E-02 0.43260E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63404          0.6136        0.005256       0.0015073
v  Velocity[Y]            -0.57349         0.54411       0.0030806      0.00087336
v  Velocity[Z]              1.5653          5.4376          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4376          4.3406          4.3632
v  Pressure                -36.406          359.99           87.64          169.83
v  r11                   0.0010594           0.082        0.013072        0.018285
v  r22                   0.0011114        0.082639        0.013352        0.018645
v  r33                   0.0016354         0.17429        0.027248        0.037205
v  r12                   -0.010661        0.013582     -0.00023379     -0.00030929
v  r13                   -0.045553        0.052806      9.3078e-05       0.0010137
v  r23                   -0.046705        0.051281      3.0355e-05      0.00057453
v  epsilon                0.068926          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9961e-05       0.0099178      0.00092478       0.0017426
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2768         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8768          0.7135         0.85283


 TIME FOR THE TIME STEP            10430:        0.84278E+02

===============================================================


 INSTANT    0.104310000E-01   TIME STEP NUMBER           10431
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.271085314E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.113710552E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226555712E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.328678147E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.376904375E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81322E-03   0.45307E-02 0.19939E+01 
c  Velocity[X]                                      0.13934E-03 
c  Velocity[Y]                                      0.12967E-03 
c  Velocity[Z]                                      0.42617E-02 
c  Pressure     0.36435E-04     132   0.92732E-02   0.25700E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.59663E-08   0.16156E-08 0.99414E-01 
c  r22          0.10851E-01      13   0.50650E-08   0.18209E-08 0.10137E+00 
c  r33          0.21859E-01      15   0.57427E-08   0.12445E-07 0.12738E+00 
c  r12          0.93856E-03      18   0.66613E-08   0.29448E-09 0.60379E+00 
c  r13          0.46674E-02      19   0.57527E-08   0.14895E-08 0.19976E+00 
c  r23          0.39974E-02      19   0.57785E-08   0.12742E-08 0.19967E+00 
c  epsilon      0.10970E+02      11   0.32943E-08   0.98847E-02 0.16383E+00 
c  TempC        0.25716E+06      16   0.15120E-04   0.84484E-02 0.43374E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61363        0.005256       0.0015073
v  Velocity[Y]            -0.57358         0.54429       0.0030808      0.00087345
v  Velocity[Z]              1.5653          5.4376          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4376          4.3406          4.3632
v  Pressure                -36.384          360.05          87.672          169.87
v  r11                   0.0010594        0.082005        0.013072        0.018285
v  r22                   0.0011114         0.08264        0.013352        0.018645
v  r33                   0.0016354         0.17426        0.027248        0.037205
v  r12                    -0.01066        0.013585     -0.00023379     -0.00030929
v  r13                   -0.045553        0.052802      9.3078e-05       0.0010137
v  r23                   -0.046704        0.051309      3.0356e-05      0.00057453
v  epsilon                0.068928          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099177      0.00092478       0.0017426
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017846           5.276         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.876          0.7135         0.85283


 TIME FOR THE TIME STEP            10431:        0.82553E+02

===============================================================


 INSTANT    0.104320000E-01   TIME STEP NUMBER           10432
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.185585628E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188007210E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.174477685E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.405158262E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.349147750E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81249E-03   0.44949E-02 0.19862E+01 
c  Velocity[X]                                      0.13869E-03 
c  Velocity[Y]                                      0.12862E-03 
c  Velocity[Z]                                      0.42276E-02 
c  Pressure     0.36357E-04     132   0.92601E-02   0.25645E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.60330E-08   0.16276E-08 0.99734E-01 
c  r22          0.10851E-01      13   0.47208E-08   0.18385E-08 0.10187E+00 
c  r33          0.21859E-01      15   0.61148E-08   0.12578E-07 0.12827E+00 
c  r12          0.93856E-03      18   0.59938E-08   0.29684E-09 0.60396E+00 
c  r13          0.46674E-02      19   0.63067E-08   0.15144E-08 0.20068E+00 
c  r23          0.39974E-02      19   0.56395E-08   0.12843E-08 0.20085E+00 
c  epsilon      0.10970E+02      11   0.32612E-08   0.98254E-02 0.16467E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.84155E-02 0.43264E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63403         0.61359        0.005256       0.0015073
v  Velocity[Y]            -0.57357         0.54444       0.0030808      0.00087344
v  Velocity[Z]              1.5654          5.4376          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4376          4.3406          4.3632
v  Pressure                -36.457          360.06           87.67          169.88
v  r11                   0.0010594        0.082007        0.013072        0.018285
v  r22                   0.0011114        0.082642        0.013352        0.018645
v  r33                   0.0016355         0.17428        0.027248        0.037205
v  r12                   -0.010659        0.013587     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052804      9.3079e-05       0.0010137
v  r23                   -0.046703        0.051296      3.0356e-05      0.00057453
v  epsilon                0.068929          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9956e-05       0.0099176      0.00092478       0.0017426
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2765         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8765          0.7135         0.85283


 TIME FOR THE TIME STEP            10432:        0.86278E+02

===============================================================


 INSTANT    0.104330000E-01   TIME STEP NUMBER           10433
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249998220E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.114015454E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.313124883E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.323498094E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.374469059E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81214E-03   0.44948E-02 0.19863E+01 
c  Velocity[X]                                      0.13748E-03 
c  Velocity[Y]                                      0.12801E-03 
c  Velocity[Z]                                      0.42294E-02 
c  Pressure     0.36262E-04     133   0.92299E-02   0.25578E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.61650E-08   0.16275E-08 0.99503E-01 
c  r22          0.10851E-01      13   0.47772E-08   0.18046E-08 0.10122E+00 
c  r33          0.21859E-01      15   0.60084E-08   0.12412E-07 0.12730E+00 
c  r12          0.93856E-03      18   0.56927E-08   0.29594E-09 0.60458E+00 
c  r13          0.46674E-02      19   0.72511E-08   0.14868E-08 0.19906E+00 
c  r23          0.39974E-02      19   0.56212E-08   0.12918E-08 0.20057E+00 
c  epsilon      0.10970E+02      11   0.32070E-08   0.96919E-02 0.16345E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84283E-02 0.43358E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63403         0.61363        0.005256       0.0015073
v  Velocity[Y]            -0.57374         0.54424       0.0030808      0.00087343
v  Velocity[Z]              1.5656          5.4376          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4376          4.3406          4.3632
v  Pressure                -36.402          360.04          87.658          169.87
v  r11                   0.0010594        0.082011        0.013072        0.018285
v  r22                   0.0011114        0.082642        0.013352        0.018645
v  r33                   0.0016355         0.17432        0.027248        0.037205
v  r12                   -0.010657        0.013579     -0.00023379     -0.00030929
v  r13                   -0.045554        0.052804       9.308e-05       0.0010137
v  r23                   -0.046702        0.051278      3.0357e-05      0.00057453
v  epsilon                 0.06893          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9953e-05       0.0099175      0.00092478       0.0017426
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2771         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8771          0.7135         0.85283


 TIME FOR THE TIME STEP            10433:        0.84453E+02

===============================================================


 INSTANT    0.104340000E-01   TIME STEP NUMBER           10434
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.275726815E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.118909014E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.545037042E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.469078702E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.494691453E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81289E-03   0.45653E-02 0.19999E+01 
c  Velocity[X]                                      0.13866E-03 
c  Velocity[Y]                                      0.12948E-03 
c  Velocity[Z]                                      0.42971E-02 
c  Pressure     0.36489E-04     134   0.92887E-02   0.25738E-01 0.00000E+00 
c  r11          0.10584E-01      14   0.51556E-08   0.16489E-08 0.10026E+00 
c  r22          0.10851E-01      13   0.52190E-08   0.17995E-08 0.10092E+00 
c  r33          0.21859E-01      15   0.63467E-08   0.12448E-07 0.12745E+00 
c  r12          0.93856E-03      18   0.60885E-08   0.28860E-09 0.59797E+00 
c  r13          0.46674E-02      20   0.58287E-08   0.14709E-08 0.19870E+00 
c  r23          0.39974E-02      19   0.53958E-08   0.12898E-08 0.20023E+00 
c  epsilon      0.10970E+02      11   0.32656E-08   0.96239E-02 0.16293E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.84736E-02 0.43404E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61361       0.0052561       0.0015073
v  Velocity[Y]            -0.57367         0.54428       0.0030807       0.0008734
v  Velocity[Z]              1.5652          5.4376          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4376          4.3406          4.3632
v  Pressure                -36.434          360.04          87.679          169.88
v  r11                   0.0010594        0.082011        0.013072        0.018285
v  r22                   0.0011114        0.082643        0.013352        0.018645
v  r33                   0.0016355         0.17433        0.027248        0.037205
v  r12                   -0.010655        0.013578     -0.00023379     -0.00030929
v  r13                   -0.045553        0.052807      9.3081e-05       0.0010137
v  r23                   -0.046702        0.051275      3.0357e-05      0.00057453
v  epsilon                0.068931          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9949e-05       0.0099174      0.00092478       0.0017426
v  CourantNb               0.44257             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2777         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8777          0.7135         0.85283


 TIME FOR THE TIME STEP            10434:        0.87476E+02

===============================================================


 INSTANT    0.104350000E-01   TIME STEP NUMBER           10435
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.602240750E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.375900130E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122226854E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100939472E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.222280362E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81162E-03   0.45241E-02 0.19898E+01 
c  Velocity[X]                                      0.13842E-03 
c  Velocity[Y]                                      0.12885E-03 
c  Velocity[Z]                                      0.42568E-02 
c  Pressure     0.36357E-04     133   0.92492E-02   0.25645E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.66141E-08   0.16678E-08 0.10098E+00 
c  r22          0.10851E-01      13   0.49733E-08   0.18026E-08 0.10095E+00 
c  r33          0.21859E-01      15   0.58337E-08   0.12588E-07 0.12836E+00 
c  r12          0.93856E-03      18   0.57801E-08   0.29624E-09 0.60437E+00 
c  r13          0.46674E-02      19   0.66675E-08   0.14927E-08 0.19919E+00 
c  r23          0.39974E-02      19   0.58781E-08   0.13143E-08 0.20305E+00 
c  epsilon      0.10970E+02      11   0.31706E-08   0.10218E-01 0.17242E+00 
c  TempC        0.25716E+06      16   0.15091E-04   0.83885E-02 0.43174E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393          0.6136       0.0052561       0.0015073
v  Velocity[Y]             -0.5738         0.54432       0.0030807      0.00087341
v  Velocity[Z]              1.5653          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4377          4.3406          4.3632
v  Pressure                -36.407          359.99          87.642          169.84
v  r11                   0.0010594        0.082014        0.013072        0.018285
v  r22                   0.0011114         0.08264        0.013352        0.018645
v  r33                   0.0016355         0.17432        0.027248        0.037205
v  r12                   -0.010652        0.013573     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052807      9.3082e-05       0.0010137
v  r23                   -0.046701        0.051302      3.0358e-05      0.00057453
v  epsilon                0.068932          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099178      0.00092478       0.0017426
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2782         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8782          0.7135         0.85283


 TIME FOR THE TIME STEP            10435:        0.85096E+02

===============================================================


 INSTANT    0.104360000E-01   TIME STEP NUMBER           10436
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178112649E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.309566748E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.151978219E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191955526E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119294654E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81335E-03   0.45198E-02 0.19930E+01 
c  Velocity[X]                                      0.13809E-03 
c  Velocity[Y]                                      0.12871E-03 
c  Velocity[Z]                                      0.42530E-02 
c  Pressure     0.36685E-04     133   0.93462E-02   0.25877E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57288E-08   0.16502E-08 0.10064E+00 
c  r22          0.10851E-01      13   0.46326E-08   0.17975E-08 0.10169E+00 
c  r33          0.21859E-01      15   0.58525E-08   0.12446E-07 0.12834E+00 
c  r12          0.93856E-03      18   0.56352E-08   0.29655E-09 0.60575E+00 
c  r13          0.46674E-02      19   0.56319E-08   0.14681E-08 0.19923E+00 
c  r23          0.39974E-02      19   0.54462E-08   0.12897E-08 0.20124E+00 
c  epsilon      0.10970E+02      11   0.33642E-08   0.95854E-02 0.16624E+00 
c  TempC        0.25716E+06      16   0.15183E-04   0.83938E-02 0.43197E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63399          0.6136       0.0052561       0.0015073
v  Velocity[Y]             -0.5737         0.54441       0.0030807      0.00087339
v  Velocity[Z]              1.5651          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4377          4.3406          4.3632
v  Pressure                -36.426          359.99          87.643          169.84
v  r11                   0.0010594        0.082014        0.013072        0.018285
v  r22                   0.0011114         0.08264        0.013352        0.018645
v  r33                   0.0016355         0.17428        0.027248        0.037205
v  r12                   -0.010653        0.013571     -0.00023379     -0.00030929
v  r13                   -0.045553        0.052806      9.3083e-05       0.0010137
v  r23                     -0.0467        0.051288      3.0359e-05      0.00057453
v  epsilon                0.068934          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05        0.009918      0.00092478       0.0017426
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2781         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781          0.7135         0.85283


 TIME FOR THE TIME STEP            10436:        0.89723E+02

===============================================================


 INSTANT    0.104370000E-01   TIME STEP NUMBER           10437
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171887800E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.415490829E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.309987227E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.299787382E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.312354717E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81115E-03   0.45137E-02 0.19895E+01 
c  Velocity[X]                                      0.13811E-03 
c  Velocity[Y]                                      0.12895E-03 
c  Velocity[Z]                                      0.42467E-02 
c  Pressure     0.35866E-04     131   0.91305E-02   0.25299E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57696E-08   0.16687E-08 0.10088E+00 
c  r22          0.10851E-01      13   0.51977E-08   0.18125E-08 0.10136E+00 
c  r33          0.21859E-01      15   0.53861E-08   0.12547E-07 0.12779E+00 
c  r12          0.93856E-03      18   0.70110E-08   0.29552E-09 0.60721E+00 
c  r13          0.46674E-02      19   0.59297E-08   0.14666E-08 0.19857E+00 
c  r23          0.39974E-02      19   0.62921E-08   0.12841E-08 0.20034E+00 
c  epsilon      0.10970E+02      11   0.34444E-08   0.96759E-02 0.16437E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.83904E-02 0.43212E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63401         0.61361       0.0052561       0.0015073
v  Velocity[Y]            -0.57384         0.54413       0.0030808       0.0008734
v  Velocity[Z]              1.5654          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4377          4.3406          4.3632
v  Pressure                -36.402          360.03          87.656          169.86
v  r11                   0.0010595        0.082013        0.013072        0.018285
v  r22                   0.0011115        0.082641        0.013353        0.018645
v  r33                   0.0016355         0.17429        0.027248        0.037205
v  r12                   -0.010651        0.013568     -0.00023379     -0.00030929
v  r13                   -0.045553        0.052806      9.3084e-05       0.0010137
v  r23                   -0.046699         0.05127      3.0359e-05      0.00057453
v  epsilon                0.068935          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9939e-05       0.0099181      0.00092479       0.0017426
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2779         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8779          0.7135         0.85283


 TIME FOR THE TIME STEP            10437:        0.86004E+02

===============================================================


 INSTANT    0.104380000E-01   TIME STEP NUMBER           10438
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191061224E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.346591708E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242099563E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.833803411E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.251480576E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81320E-03   0.45190E-02 0.19907E+01 
c  Velocity[X]                                      0.13864E-03 
c  Velocity[Y]                                      0.12986E-03 
c  Velocity[Z]                                      0.42505E-02 
c  Pressure     0.36623E-04     132   0.93207E-02   0.25832E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.57056E-08   0.16548E-08 0.10037E+00 
c  r22          0.10851E-01      13   0.49514E-08   0.18509E-08 0.10223E+00 
c  r33          0.21859E-01      14   0.65509E-08   0.12736E-07 0.12848E+00 
c  r12          0.93857E-03      18   0.66162E-08   0.29807E-09 0.60562E+00 
c  r13          0.46674E-02      19   0.55686E-08   0.15155E-08 0.20069E+00 
c  r23          0.39974E-02      19   0.54542E-08   0.13013E-08 0.20154E+00 
c  epsilon      0.10970E+02      11   0.34675E-08   0.99773E-02 0.16710E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.83277E-02 0.43103E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63404         0.61358        0.005256       0.0015073
v  Velocity[Y]             -0.5738         0.54413       0.0030807      0.00087339
v  Velocity[Z]              1.5652          5.4377          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4377          4.3406          4.3632
v  Pressure                -36.442          360.05          87.679          169.88
v  r11                   0.0010595        0.081999        0.013072        0.018285
v  r22                   0.0011115        0.082641        0.013353        0.018645
v  r33                   0.0016355         0.17432        0.027248        0.037205
v  r12                   -0.010651        0.013565     -0.00023379     -0.00030929
v  r13                   -0.045555        0.052806      9.3084e-05       0.0010137
v  r23                   -0.046699        0.051255      3.0359e-05      0.00057452
v  epsilon                0.068936          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099181      0.00092479       0.0017426
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2782         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8782          0.7135         0.85283


 TIME FOR THE TIME STEP            10438:        0.82296E+02

===============================================================


 INSTANT    0.104390000E-01   TIME STEP NUMBER           10439
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.560335070E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.342090163E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.947024438E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.109758605E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.139897309E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69780E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81260E-03   0.45568E-02 0.19994E+01 
c  Velocity[X]                                      0.13847E-03 
c  Velocity[Y]                                      0.12900E-03 
c  Velocity[Z]                                      0.42893E-02 
c  Pressure     0.36622E-04     131   0.93231E-02   0.25832E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56614E-08   0.16571E-08 0.10018E+00 
c  r22          0.10851E-01      13   0.53850E-08   0.18669E-08 0.10290E+00 
c  r33          0.21859E-01      15   0.51766E-08   0.12717E-07 0.12850E+00 
c  r12          0.93857E-03      18   0.62872E-08   0.29801E-09 0.60526E+00 
c  r13          0.46674E-02      19   0.57779E-08   0.15089E-08 0.20096E+00 
c  r23          0.39974E-02      19   0.56331E-08   0.12961E-08 0.20049E+00 
c  epsilon      0.10970E+02      11   0.33031E-08   0.99736E-02 0.16579E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.84628E-02 0.43379E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61361        0.005256       0.0015073
v  Velocity[Y]            -0.57374         0.54423       0.0030807       0.0008734
v  Velocity[Z]              1.5651          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4377          4.3406          4.3632
v  Pressure                -36.401          360.02          87.647          169.85
v  r11                   0.0010595        0.081993        0.013072        0.018285
v  r22                   0.0011115        0.082639        0.013353        0.018645
v  r33                   0.0016356         0.17429        0.027248        0.037205
v  r12                    -0.01065        0.013572     -0.00023379     -0.00030929
v  r13                   -0.045552        0.052804      9.3086e-05       0.0010137
v  r23                   -0.046698        0.051284       3.036e-05      0.00057453
v  epsilon                0.068937          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099181      0.00092479       0.0017426
v  CourantNb               0.44259             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2778         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8778          0.7135         0.85283


 TIME FOR THE TIME STEP            10439:        0.84422E+02

===============================================================


 INSTANT    0.104400000E-01   TIME STEP NUMBER           10440
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.724209010E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.895535547E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.474156629E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.114814700E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.883992493E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81165E-03   0.45127E-02 0.19906E+01 
c  Velocity[X]                                      0.13912E-03 
c  Velocity[Y]                                      0.12851E-03 
c  Velocity[Z]                                      0.42451E-02 
c  Pressure     0.36271E-04     131   0.92401E-02   0.25584E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53363E-08   0.16484E-08 0.10023E+00 
c  r22          0.10851E-01      13   0.51977E-08   0.18413E-08 0.10235E+00 
c  r33          0.21859E-01      15   0.54970E-08   0.12538E-07 0.12828E+00 
c  r12          0.93857E-03      18   0.58869E-08   0.29831E-09 0.60569E+00 
c  r13          0.46674E-02      19   0.62399E-08   0.14772E-08 0.19976E+00 
c  r23          0.39975E-02      19   0.59213E-08   0.12805E-08 0.20075E+00 
c  epsilon      0.10970E+02      11   0.32707E-08   0.99421E-02 0.16550E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.84656E-02 0.43410E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63401         0.61361        0.005256       0.0015073
v  Velocity[Y]            -0.57362         0.54441       0.0030807       0.0008734
v  Velocity[Z]              1.5653          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4377          4.3406          4.3632
v  Pressure                -36.405          360.03          87.669          169.87
v  r11                   0.0010595        0.081987        0.013072        0.018285
v  r22                   0.0011115        0.082638        0.013353        0.018645
v  r33                   0.0016356         0.17427        0.027248        0.037205
v  r12                   -0.010652        0.013572     -0.00023379     -0.00030929
v  r13                   -0.045551        0.052805      9.3087e-05       0.0010137
v  r23                   -0.046698        0.051273      3.0361e-05      0.00057453
v  epsilon                0.068938          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05        0.009918      0.00092479       0.0017426
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2767         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8767          0.7135         0.85284


 TIME FOR THE TIME STEP            10440:        0.10283E+03

===============================================================


 INSTANT    0.104410000E-01   TIME STEP NUMBER           10441
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.284547799E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.297163206E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.273498140E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.295343874E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.446341543E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81256E-03   0.45095E-02 0.19874E+01 
c  Velocity[X]                                      0.13723E-03 
c  Velocity[Y]                                      0.12841E-03 
c  Velocity[Z]                                      0.42438E-02 
c  Pressure     0.36396E-04     132   0.92597E-02   0.25672E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51071E-08   0.16748E-08 0.10121E+00 
c  r22          0.10851E-01      13   0.49770E-08   0.18485E-08 0.10234E+00 
c  r33          0.21859E-01      15   0.55734E-08   0.12719E-07 0.12905E+00 
c  r12          0.93857E-03      18   0.60238E-08   0.30069E-09 0.60697E+00 
c  r13          0.46674E-02      19   0.54461E-08   0.15003E-08 0.20040E+00 
c  r23          0.39975E-02      18   0.67791E-08   0.13162E-08 0.20395E+00 
c  epsilon      0.10970E+02      11   0.32466E-08   0.10186E-01 0.17018E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.84131E-02 0.43268E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63403         0.61358       0.0052561       0.0015073
v  Velocity[Y]            -0.57366         0.54409       0.0030807      0.00087338
v  Velocity[Z]              1.5652          5.4377          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4377          4.3406          4.3632
v  Pressure                -36.399          359.96           87.61           169.8
v  r11                   0.0010595        0.081979        0.013072        0.018285
v  r22                   0.0011115        0.082632        0.013353        0.018645
v  r33                   0.0016356         0.17429        0.027248        0.037205
v  r12                   -0.010651         0.01357     -0.00023379     -0.00030929
v  r13                   -0.045554        0.052805      9.3088e-05       0.0010137
v  r23                   -0.046699        0.051266      3.0361e-05      0.00057453
v  epsilon                 0.06894          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9939e-05        0.009918      0.00092479       0.0017426
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2767         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8767          0.7135         0.85283


 TIME FOR THE TIME STEP            10441:        0.14618E+03

===============================================================


 INSTANT    0.104420000E-01   TIME STEP NUMBER           10442
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.307674322E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.947639073E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.104775746E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.104757554E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.468028985E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81258E-03   0.45228E-02 0.19929E+01 
c  Velocity[X]                                      0.13804E-03 
c  Velocity[Y]                                      0.12952E-03 
c  Velocity[Z]                                      0.42552E-02 
c  Pressure     0.36341E-04     133   0.92517E-02   0.25634E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52659E-08   0.15944E-08 0.99492E-01 
c  r22          0.10851E-01      13   0.48705E-08   0.17855E-08 0.10154E+00 
c  r33          0.21859E-01      15   0.54622E-08   0.12130E-07 0.12706E+00 
c  r12          0.93857E-03      18   0.59258E-08   0.28546E-09 0.59720E+00 
c  r13          0.46674E-02      18   0.69283E-08   0.14728E-08 0.20000E+00 
c  r23          0.39975E-02      19   0.52186E-08   0.12492E-08 0.19990E+00 
c  epsilon      0.10970E+02      11   0.33088E-08   0.92883E-02 0.16119E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.84319E-02 0.43333E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63409         0.61362       0.0052562       0.0015074
v  Velocity[Y]            -0.57366         0.54413       0.0030806      0.00087334
v  Velocity[Z]              1.5654          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4377          4.3406          4.3632
v  Pressure                -36.434             360          87.652          169.84
v  r11                   0.0010595        0.081978        0.013072        0.018285
v  r22                   0.0011115        0.082633        0.013353        0.018645
v  r33                   0.0016356          0.1743        0.027248        0.037205
v  r12                   -0.010653        0.013576     -0.00023379      -0.0003093
v  r13                   -0.045552        0.052807      9.3089e-05       0.0010137
v  r23                     -0.0467        0.051288      3.0361e-05      0.00057452
v  epsilon                0.068941          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099177      0.00092479       0.0017426
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2775         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8775          0.7135         0.85283


 TIME FOR THE TIME STEP            10442:        0.12884E+03

===============================================================


 INSTANT    0.104430000E-01   TIME STEP NUMBER           10443
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106637725E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.231554930E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.359258829E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123843417E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.233219229E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81215E-03   0.45157E-02 0.19899E+01 
c  Velocity[X]                                      0.13834E-03 
c  Velocity[Y]                                      0.12856E-03 
c  Velocity[Z]                                      0.42488E-02 
c  Pressure     0.36251E-04     132   0.92219E-02   0.25570E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.46124E-08   0.16323E-08 0.10009E+00 
c  r22          0.10851E-01      13   0.45494E-08   0.18264E-08 0.10265E+00 
c  r33          0.21859E-01      15   0.51693E-08   0.12489E-07 0.12858E+00 
c  r12          0.93857E-03      18   0.60050E-08   0.29632E-09 0.60556E+00 
c  r13          0.46674E-02      19   0.56920E-08   0.14724E-08 0.20119E+00 
c  r23          0.39975E-02      18   0.66372E-08   0.13039E-08 0.20242E+00 
c  epsilon      0.10970E+02      11   0.31148E-08   0.94856E-02 0.16152E+00 
c  TempC        0.25716E+06      16   0.15121E-04   0.84442E-02 0.43391E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63402         0.61361       0.0052561       0.0015073
v  Velocity[Y]            -0.57384         0.54429       0.0030807      0.00087337
v  Velocity[Z]              1.5653          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4377          4.3406          4.3632
v  Pressure                -36.409          360.02          87.649          169.86
v  r11                   0.0010595        0.081985        0.013072        0.018285
v  r22                   0.0011115        0.082633        0.013353        0.018645
v  r33                   0.0016356         0.17434        0.027248        0.037205
v  r12                   -0.010653        0.013573     -0.00023379     -0.00030929
v  r13                   -0.045551        0.052803       9.309e-05       0.0010137
v  r23                     -0.0467        0.051271      3.0363e-05      0.00057453
v  epsilon                0.068942          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9945e-05       0.0099177      0.00092479       0.0017426
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2784         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8784          0.7135         0.85283


 TIME FOR THE TIME STEP            10443:        0.13395E+03

===============================================================


 INSTANT    0.104440000E-01   TIME STEP NUMBER           10444
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.767969802E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208009391E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.619870838E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107159137E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.293038678E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81304E-03   0.45019E-02 0.19881E+01 
c  Velocity[X]                                      0.13792E-03 
c  Velocity[Y]                                      0.12893E-03 
c  Velocity[Z]                                      0.42351E-02 
c  Pressure     0.36467E-04     132   0.92884E-02   0.25722E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55392E-08   0.16719E-08 0.10105E+00 
c  r22          0.10851E-01      13   0.50043E-08   0.18603E-08 0.10269E+00 
c  r33          0.21859E-01      14   0.70029E-08   0.12721E-07 0.12874E+00 
c  r12          0.93857E-03      18   0.59654E-08   0.30842E-09 0.61123E+00 
c  r13          0.46674E-02      19   0.58088E-08   0.14992E-08 0.20034E+00 
c  r23          0.39975E-02      19   0.53977E-08   0.13129E-08 0.20249E+00 
c  epsilon      0.10970E+02      11   0.31390E-08   0.98061E-02 0.16549E+00 
c  TempC        0.25716E+06      16   0.15173E-04   0.83855E-02 0.43181E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -0.634         0.61362       0.0052561       0.0015073
v  Velocity[Y]            -0.57378         0.54447       0.0030806      0.00087337
v  Velocity[Z]              1.5654          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4377          4.3406          4.3632
v  Pressure                -36.454          360.05          87.669          169.88
v  r11                   0.0010595        0.081982        0.013072        0.018285
v  r22                   0.0011115        0.082632        0.013353        0.018645
v  r33                   0.0016356         0.17432        0.027248        0.037205
v  r12                   -0.010658        0.013576     -0.00023379      -0.0003093
v  r13                   -0.045554        0.052802      9.3091e-05       0.0010137
v  r23                     -0.0467        0.051264      3.0365e-05      0.00057453
v  epsilon                0.068943          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9945e-05       0.0099178      0.00092479       0.0017426
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2785         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8785          0.7135         0.85283


 TIME FOR THE TIME STEP            10444:        0.12261E+03

===============================================================


 INSTANT    0.104450000E-01   TIME STEP NUMBER           10445
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.229895968E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.592399790E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.435088817E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.130345024E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.292235141E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81209E-03   0.45528E-02 0.19967E+01 
c  Velocity[X]                                      0.13809E-03 
c  Velocity[Y]                                      0.12919E-03 
c  Velocity[Z]                                      0.42856E-02 
c  Pressure     0.36338E-04     132   0.92456E-02   0.25631E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54268E-08   0.16740E-08 0.10186E+00 
c  r22          0.10851E-01      13   0.50035E-08   0.18407E-08 0.10279E+00 
c  r33          0.21859E-01      14   0.68218E-08   0.12588E-07 0.12935E+00 
c  r12          0.93857E-03      18   0.61683E-08   0.30279E-09 0.61211E+00 
c  r13          0.46674E-02      19   0.56043E-08   0.14894E-08 0.20036E+00 
c  r23          0.39975E-02      18   0.71016E-08   0.13010E-08 0.20361E+00 
c  epsilon      0.10970E+02      11   0.32254E-08   0.94918E-02 0.16285E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84300E-02 0.43304E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63395         0.61363       0.0052561       0.0015073
v  Velocity[Y]             -0.5739         0.54411       0.0030807      0.00087336
v  Velocity[Z]              1.5657          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4377          4.3406          4.3632
v  Pressure                -36.429          360.07          87.677          169.89
v  r11                   0.0010595        0.081986        0.013073        0.018285
v  r22                   0.0011115        0.082631        0.013353        0.018645
v  r33                   0.0016356         0.17428        0.027248        0.037205
v  r12                    -0.01066        0.013577     -0.00023379      -0.0003093
v  r13                   -0.045553        0.052802      9.3093e-05       0.0010137
v  r23                     -0.0467        0.051278      3.0366e-05      0.00057453
v  epsilon                0.068944          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099178      0.00092479       0.0017426
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2788         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8788          0.7135         0.85283


 TIME FOR THE TIME STEP            10445:        0.14676E+03

===============================================================


 INSTANT    0.104460000E-01   TIME STEP NUMBER           10446
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.643450049E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.167326270E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.241956445E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.581463327E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.529818915E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81324E-03   0.45335E-02 0.19954E+01 
c  Velocity[X]                                      0.13891E-03 
c  Velocity[Y]                                      0.12897E-03 
c  Velocity[Z]                                      0.42656E-02 
c  Pressure     0.36938E-04     132   0.94065E-02   0.26055E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53250E-08   0.16475E-08 0.10050E+00 
c  r22          0.10851E-01      13   0.51789E-08   0.18432E-08 0.10252E+00 
c  r33          0.21859E-01      15   0.54706E-08   0.12637E-07 0.12894E+00 
c  r12          0.93857E-03      18   0.63319E-08   0.29301E-09 0.60350E+00 
c  r13          0.46674E-02      19   0.64263E-08   0.15010E-08 0.20078E+00 
c  r23          0.39975E-02      19   0.55109E-08   0.12842E-08 0.20141E+00 
c  epsilon      0.10970E+02      11   0.34646E-08   0.98960E-02 0.16488E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.83908E-02 0.43183E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61359       0.0052561       0.0015073
v  Velocity[Y]            -0.57396         0.54417       0.0030807      0.00087335
v  Velocity[Z]              1.5653          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4377          4.3406          4.3632
v  Pressure                -36.427          360.01           87.64          169.83
v  r11                   0.0010595        0.081976        0.013073        0.018285
v  r22                   0.0011115        0.082632        0.013353        0.018645
v  r33                   0.0016357          0.1743        0.027248        0.037205
v  r12                   -0.010658        0.013576     -0.00023379      -0.0003093
v  r13                   -0.045551        0.052803      9.3094e-05       0.0010137
v  r23                   -0.046699        0.051265      3.0367e-05      0.00057453
v  epsilon                0.068946          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099177       0.0009248       0.0017426
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2789         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8789          0.7135         0.85283


 TIME FOR THE TIME STEP            10446:        0.15559E+03

===============================================================


 INSTANT    0.104470000E-01   TIME STEP NUMBER           10447
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.693987355E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.273245999E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.260023396E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.931011394E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.253719889E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81285E-03   0.45296E-02 0.19927E+01 
c  Velocity[X]                                      0.13775E-03 
c  Velocity[Y]                                      0.12805E-03 
c  Velocity[Z]                                      0.42638E-02 
c  Pressure     0.36328E-04     133   0.92457E-02   0.25624E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.58050E-08   0.17057E-08 0.10172E+00 
c  r22          0.10851E-01      13   0.55395E-08   0.18355E-08 0.10201E+00 
c  r33          0.21859E-01      15   0.63252E-08   0.12799E-07 0.12913E+00 
c  r12          0.93857E-03      18   0.60462E-08   0.29791E-09 0.60390E+00 
c  r13          0.46674E-02      19   0.67897E-08   0.14925E-08 0.19921E+00 
c  r23          0.39975E-02      19   0.58291E-08   0.13249E-08 0.20320E+00 
c  epsilon      0.10970E+02      11   0.35137E-08   0.10339E-01 0.17163E+00 
c  TempC        0.25716E+06      16   0.15094E-04   0.84033E-02 0.43265E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61364       0.0052562       0.0015073
v  Velocity[Y]            -0.57402         0.54427       0.0030807      0.00087332
v  Velocity[Z]              1.5654          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4377          4.3406          4.3632
v  Pressure                -36.399          360.01          87.629          169.84
v  r11                   0.0010595        0.081974        0.013073        0.018285
v  r22                   0.0011115        0.082629        0.013353        0.018645
v  r33                   0.0016357         0.17432        0.027248        0.037205
v  r12                    -0.01066        0.013578     -0.00023379      -0.0003093
v  r13                   -0.045553        0.052805      9.3095e-05       0.0010137
v  r23                   -0.046699        0.051249      3.0367e-05      0.00057453
v  epsilon                0.068947          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9949e-05       0.0099176       0.0009248       0.0017426
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2782         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8782          0.7135         0.85283


 TIME FOR THE TIME STEP            10447:        0.14629E+03

===============================================================


 INSTANT    0.104480000E-01   TIME STEP NUMBER           10448
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.309534047E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.143444756E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934907E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.331752725E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.384032238E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.149045740E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81291E-03   0.45085E-02 0.19899E+01 
c  Velocity[X]                                      0.13750E-03 
c  Velocity[Y]                                      0.12869E-03 
c  Velocity[Z]                                      0.42423E-02 
c  Pressure     0.36313E-04     136   0.92524E-02   0.25614E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.50777E-08   0.16237E-08 0.99700E-01 
c  r22          0.10851E-01      13   0.54452E-08   0.18229E-08 0.10179E+00 
c  r33          0.21859E-01      15   0.61423E-08   0.12484E-07 0.12787E+00 
c  r12          0.93857E-03      18   0.54669E-08   0.29183E-09 0.60048E+00 
c  r13          0.46674E-02      19   0.60351E-08   0.15056E-08 0.20018E+00 
c  r23          0.39975E-02      19   0.51846E-08   0.12922E-08 0.20078E+00 
c  epsilon      0.10970E+02      11   0.32666E-08   0.99184E-02 0.16625E+00 
c  TempC        0.25716E+06      16   0.15190E-04   0.84548E-02 0.43416E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61359       0.0052562       0.0015073
v  Velocity[Y]            -0.57397         0.54439       0.0030806      0.00087332
v  Velocity[Z]              1.5651          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4377          4.3406          4.3632
v  Pressure                -36.468          360.02           87.65          169.85
v  r11                   0.0010595        0.081959        0.013073        0.018285
v  r22                   0.0011116         0.08263        0.013353        0.018645
v  r33                   0.0016357          0.1743        0.027248        0.037205
v  r12                    -0.01066        0.013574     -0.00023379      -0.0003093
v  r13                   -0.045551        0.052805      9.3096e-05       0.0010137
v  r23                   -0.046699        0.051235      3.0367e-05      0.00057453
v  epsilon                0.068948          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9949e-05       0.0099174       0.0009248       0.0017426
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2786         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8786          0.7135         0.85283


 TIME FOR THE TIME STEP            10448:        0.98160E+02

===============================================================


 INSTANT    0.104490000E-01   TIME STEP NUMBER           10449
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.238768591E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.554069899E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.554957188E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158177594E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.199195293E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81165E-03   0.45188E-02 0.19904E+01 
c  Velocity[X]                                      0.13864E-03 
c  Velocity[Y]                                      0.12867E-03 
c  Velocity[Z]                                      0.42515E-02 
c  Pressure     0.36316E-04     133   0.92437E-02   0.25615E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.51514E-08   0.16480E-08 0.10027E+00 
c  r22          0.10851E-01      13   0.54987E-08   0.18304E-08 0.10166E+00 
c  r33          0.21859E-01      15   0.69156E-08   0.12518E-07 0.12766E+00 
c  r12          0.93857E-03      18   0.52120E-08   0.29942E-09 0.60343E+00 
c  r13          0.46674E-02      19   0.56669E-08   0.14938E-08 0.19928E+00 
c  r23          0.39975E-02      19   0.52927E-08   0.12920E-08 0.20107E+00 
c  epsilon      0.10970E+02      11   0.33770E-08   0.97747E-02 0.16468E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.84369E-02 0.43355E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63403         0.61356       0.0052561       0.0015073
v  Velocity[Y]            -0.57394         0.54417       0.0030807      0.00087336
v  Velocity[Z]              1.5652          5.4377          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4377          4.3406          4.3632
v  Pressure                -36.409          360.03          87.658          169.86
v  r11                   0.0010595        0.081953        0.013073        0.018285
v  r22                   0.0011116        0.082633        0.013353        0.018645
v  r33                   0.0016357         0.17427        0.027248        0.037205
v  r12                   -0.010658        0.013576     -0.00023379      -0.0003093
v  r13                   -0.045552        0.052803      9.3097e-05       0.0010137
v  r23                   -0.046698         0.05125      3.0368e-05      0.00057453
v  epsilon                0.068949          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099174       0.0009248       0.0017426
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2782         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8782          0.7135         0.85283


 TIME FOR THE TIME STEP            10449:        0.77507E+02

===============================================================


 INSTANT    0.104500000E-01   TIME STEP NUMBER           10450
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.854408686E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.153373341E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.901141869E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.714869733E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.282055212E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81268E-03   0.45499E-02 0.19973E+01 
c  Velocity[X]                                      0.13820E-03 
c  Velocity[Y]                                      0.12936E-03 
c  Velocity[Z]                                      0.42824E-02 
c  Pressure     0.36541E-04     133   0.93075E-02   0.25774E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.52952E-08   0.16442E-08 0.10041E+00 
c  r22          0.10851E-01      13   0.52475E-08   0.18424E-08 0.10234E+00 
c  r33          0.21859E-01      15   0.71784E-08   0.12671E-07 0.12856E+00 
c  r12          0.93857E-03      18   0.49286E-08   0.30325E-09 0.60988E+00 
c  r13          0.46674E-02      19   0.58827E-08   0.15125E-08 0.20054E+00 
c  r23          0.39975E-02      19   0.54785E-08   0.13108E-08 0.20278E+00 
c  epsilon      0.10970E+02      11   0.34062E-08   0.95566E-02 0.16298E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.84175E-02 0.43292E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63403          0.6136       0.0052561       0.0015073
v  Velocity[Y]            -0.57396         0.54426       0.0030806      0.00087335
v  Velocity[Z]              1.5653          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4377          4.3406          4.3632
v  Pressure                -36.452          360.03           87.65          169.85
v  r11                   0.0010595        0.081946        0.013073        0.018285
v  r22                   0.0011116        0.082635        0.013353        0.018645
v  r33                   0.0016357         0.17429        0.027248        0.037205
v  r12                   -0.010657        0.013573     -0.00023379      -0.0003093
v  r13                   -0.045554        0.052804      9.3098e-05       0.0010137
v  r23                   -0.046697        0.051245      3.0369e-05      0.00057453
v  epsilon                 0.06895          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9953e-05       0.0099174       0.0009248       0.0017426
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2787         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8787          0.7135         0.85283


 TIME FOR THE TIME STEP            10450:        0.77650E+02

===============================================================


 INSTANT    0.104510000E-01   TIME STEP NUMBER           10451
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.437814621E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.617580219E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141926845E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.936930115E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.135799644E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81367E-03   0.45218E-02 0.19910E+01 
c  Velocity[X]                                      0.13748E-03 
c  Velocity[Y]                                      0.12903E-03 
c  Velocity[Z]                                      0.42553E-02 
c  Pressure     0.36332E-04     132   0.92459E-02   0.25626E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.55236E-08   0.16522E-08 0.10084E+00 
c  r22          0.10851E-01      13   0.57548E-08   0.18398E-08 0.10230E+00 
c  r33          0.21859E-01      15   0.66538E-08   0.12580E-07 0.12822E+00 
c  r12          0.93857E-03      18   0.61394E-08   0.30238E-09 0.60878E+00 
c  r13          0.46674E-02      19   0.64942E-08   0.14968E-08 0.20062E+00 
c  r23          0.39975E-02      18   0.67457E-08   0.12897E-08 0.20086E+00 
c  epsilon      0.10970E+02      11   0.34267E-08   0.96784E-02 0.16414E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.83594E-02 0.43088E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63405         0.61358       0.0052562       0.0015073
v  Velocity[Y]            -0.57405         0.54443       0.0030807      0.00087336
v  Velocity[Z]              1.5652          5.4377          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4377          4.3406          4.3632
v  Pressure                -36.382          359.98          87.626          169.82
v  r11                   0.0010595        0.081941        0.013073        0.018285
v  r22                   0.0011116        0.082635        0.013353        0.018645
v  r33                   0.0016357         0.17431        0.027248        0.037205
v  r12                   -0.010655        0.013578     -0.00023379      -0.0003093
v  r13                   -0.045551        0.052801      9.3099e-05       0.0010137
v  r23                   -0.046697        0.051229       3.037e-05      0.00057453
v  epsilon                0.068951           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9956e-05       0.0099174       0.0009248       0.0017426
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2777         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8777          0.7135         0.85284


 TIME FOR THE TIME STEP            10451:        0.78999E+02

===============================================================


 INSTANT    0.104520000E-01   TIME STEP NUMBER           10452
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.186439714E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.452330478E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934913E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.951568884E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.264470083E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154341349E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81245E-03   0.45202E-02 0.19906E+01 
c  Velocity[X]                                      0.13897E-03 
c  Velocity[Y]                                      0.12837E-03 
c  Velocity[Z]                                      0.42528E-02 
c  Pressure     0.36563E-04     133   0.93103E-02   0.25790E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.56755E-08   0.16279E-08 0.99871E-01 
c  r22          0.10851E-01      13   0.51187E-08   0.18191E-08 0.10169E+00 
c  r33          0.21859E-01      15   0.66772E-08   0.12445E-07 0.12765E+00 
c  r12          0.93857E-03      18   0.56468E-08   0.29205E-09 0.60132E+00 
c  r13          0.46674E-02      19   0.57925E-08   0.14679E-08 0.19954E+00 
c  r23          0.39975E-02      19   0.51620E-08   0.12695E-08 0.19918E+00 
c  epsilon      0.10970E+02      11   0.35681E-08   0.96737E-02 0.16412E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.84249E-02 0.43327E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63396         0.61357       0.0052561       0.0015073
v  Velocity[Y]            -0.57408         0.54408       0.0030807      0.00087332
v  Velocity[Z]              1.5652          5.4377          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4377          4.3406          4.3632
v  Pressure                -36.417          360.06          87.684          169.89
v  r11                   0.0010596         0.08193        0.013073        0.018285
v  r22                   0.0011116        0.082636        0.013353        0.018645
v  r33                   0.0016358          0.1743        0.027248        0.037205
v  r12                   -0.010658        0.013578     -0.00023379      -0.0003093
v  r13                    -0.04555        0.052801        9.31e-05       0.0010137
v  r23                   -0.046696        0.051252       3.037e-05      0.00057453
v  epsilon                0.068952           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9956e-05       0.0099173       0.0009248       0.0017426
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2779         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8779          0.7135         0.85283


 TIME FOR THE TIME STEP            10452:        0.78816E+02

===============================================================


 INSTANT    0.104530000E-01   TIME STEP NUMBER           10453
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.951574615E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.244699985E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.456501213E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.189491226E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.355117781E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81246E-03   0.45222E-02 0.19919E+01 
c  Velocity[X]                                      0.13762E-03 
c  Velocity[Y]                                      0.12805E-03 
c  Velocity[Z]                                      0.42565E-02 
c  Pressure     0.36237E-04     133   0.92224E-02   0.25560E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.53062E-08   0.16917E-08 0.10171E+00 
c  r22          0.10851E-01      13   0.47834E-08   0.18601E-08 0.10289E+00 
c  r33          0.21859E-01      15   0.75164E-08   0.12849E-07 0.12956E+00 
c  r12          0.93857E-03      18   0.61950E-08   0.30437E-09 0.61188E+00 
c  r13          0.46674E-02      19   0.67538E-08   0.14998E-08 0.20112E+00 
c  r23          0.39975E-02      19   0.63065E-08   0.13347E-08 0.20396E+00 
c  epsilon      0.10970E+02      11   0.36472E-08   0.10167E-01 0.17102E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.83915E-02 0.43270E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61361       0.0052561       0.0015073
v  Velocity[Y]            -0.57412          0.5441       0.0030807      0.00087331
v  Velocity[Z]              1.5651          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4377          4.3406          4.3632
v  Pressure                -36.438          360.06          87.667          169.88
v  r11                   0.0010596        0.081933        0.013073        0.018285
v  r22                   0.0011116        0.082633        0.013353        0.018645
v  r33                   0.0016358         0.17428        0.027248        0.037205
v  r12                   -0.010659        0.013576     -0.00023379      -0.0003093
v  r13                   -0.045554        0.052805      9.3101e-05       0.0010137
v  r23                   -0.046694        0.051237       3.037e-05      0.00057453
v  epsilon                0.068954          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9958e-05       0.0099175       0.0009248       0.0017426
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2785         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8785          0.7135         0.85283


 TIME FOR THE TIME STEP            10453:        0.80049E+02

===============================================================


 INSTANT    0.104540000E-01   TIME STEP NUMBER           10454
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.411230620E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.289540778E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.524246677E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935012E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.156176236E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158555291E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81234E-03   0.44990E-02 0.19884E+01 
c  Velocity[X]                                      0.13839E-03 
c  Velocity[Y]                                      0.12888E-03 
c  Velocity[Z]                                      0.42317E-02 
c  Pressure     0.36198E-04     132   0.92150E-02   0.25532E-01 0.00000E+00 
c  r11          0.10584E-01      13   0.54847E-08   0.16138E-08 0.99724E-01 
c  r22          0.10851E-01      13   0.45958E-08   0.18711E-08 0.10291E+00 
c  r33          0.21859E-01      15   0.63430E-08   0.12599E-07 0.12844E+00 
c  r12          0.93857E-03      18   0.52338E-08   0.30136E-09 0.61129E+00 
c  r13          0.46674E-02      19   0.53981E-08   0.15227E-08 0.20140E+00 
c  r23          0.39975E-02      19   0.61591E-08   0.12692E-08 0.19970E+00 
c  epsilon      0.10970E+02      11   0.33650E-08   0.96412E-02 0.16344E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.84231E-02 0.43254E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63402         0.61357       0.0052561       0.0015073
v  Velocity[Y]            -0.57401         0.54424       0.0030806      0.00087329
v  Velocity[Z]              1.5652          5.4377          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4377          4.3406          4.3632
v  Pressure                -36.485          359.98          87.628          169.82
v  r11                   0.0010596        0.081927        0.013073        0.018285
v  r22                   0.0011116        0.082635        0.013353        0.018645
v  r33                   0.0016358         0.17429        0.027248        0.037205
v  r12                   -0.010661        0.013581     -0.00023379      -0.0003093
v  r13                   -0.045551        0.052806      9.3101e-05       0.0010137
v  r23                   -0.046693        0.051226      3.0371e-05      0.00057453
v  epsilon                0.068955           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099176       0.0009248       0.0017426
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017845           5.279         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.879          0.7135         0.85284


 TIME FOR THE TIME STEP            10454:        0.78986E+02

===============================================================


 INSTANT    0.104550000E-01   TIME STEP NUMBER           10455
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151156195E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.706811607E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.182588805E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.198743733E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.671468135E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81234E-03   0.45365E-02 0.19954E+01 
c  Velocity[X]                                      0.13944E-03 
c  Velocity[Y]                                      0.12937E-03 
c  Velocity[Z]                                      0.42677E-02 
c  Pressure     0.36713E-04     133   0.93457E-02   0.25895E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54588E-08   0.16597E-08 0.10087E+00 
c  r22          0.10851E-01      13   0.46091E-08   0.18674E-08 0.10283E+00 
c  r33          0.21859E-01      15   0.52294E-08   0.12731E-07 0.12889E+00 
c  r12          0.93857E-03      18   0.53311E-08   0.29876E-09 0.60790E+00 
c  r13          0.46674E-02      18   0.65738E-08   0.14943E-08 0.20046E+00 
c  r23          0.39975E-02      19   0.58081E-08   0.12715E-08 0.20070E+00 
c  epsilon      0.10970E+02      11   0.32587E-08   0.10028E-01 0.16497E+00 
c  TempC        0.25716E+06      16   0.15101E-04   0.84910E-02 0.43428E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63405         0.61361       0.0052561       0.0015073
v  Velocity[Y]            -0.57391         0.54439       0.0030806       0.0008733
v  Velocity[Z]              1.5651          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4377          4.3406          4.3632
v  Pressure                -36.428          360.04          87.647          169.86
v  r11                   0.0010596        0.081925        0.013073        0.018285
v  r22                   0.0011116        0.082637        0.013353        0.018645
v  r33                   0.0016358         0.17432        0.027248        0.037205
v  r12                   -0.010661        0.013587     -0.00023379      -0.0003093
v  r13                   -0.045551        0.052804      9.3102e-05       0.0010137
v  r23                   -0.046692        0.051247      3.0373e-05      0.00057453
v  epsilon                0.068956          271.31          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099178      0.00092481       0.0017426
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2784         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8784          0.7135         0.85283


 TIME FOR THE TIME STEP            10455:        0.80941E+02

===============================================================


 INSTANT    0.104560000E-01   TIME STEP NUMBER           10456
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.842299589E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.386839703E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.193933439E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.570015083E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.861419005E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81354E-03   0.45111E-02 0.19892E+01 
c  Velocity[X]                                      0.13820E-03 
c  Velocity[Y]                                      0.12839E-03 
c  Velocity[Z]                                      0.42446E-02 
c  Pressure     0.36508E-04     132   0.92967E-02   0.25752E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52655E-08   0.16606E-08 0.10076E+00 
c  r22          0.10851E-01      13   0.47171E-08   0.18933E-08 0.10296E+00 
c  r33          0.21859E-01      15   0.62058E-08   0.12843E-07 0.12911E+00 
c  r12          0.93857E-03      18   0.57099E-08   0.29891E-09 0.60648E+00 
c  r13          0.46674E-02      18   0.71904E-08   0.15398E-08 0.20176E+00 
c  r23          0.39975E-02      19   0.57956E-08   0.12785E-08 0.20077E+00 
c  epsilon      0.10970E+02      11   0.34096E-08   0.10207E-01 0.16735E+00 
c  TempC        0.25716E+06      16   0.15169E-04   0.83809E-02 0.43222E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63401          0.6136       0.0052561       0.0015073
v  Velocity[Y]            -0.57387         0.54424       0.0030806      0.00087328
v  Velocity[Z]              1.5652          5.4377          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4377          4.3406          4.3632
v  Pressure                -36.484          360.04          87.648          169.85
v  r11                   0.0010596        0.081924        0.013073        0.018285
v  r22                   0.0011116        0.082638        0.013353        0.018645
v  r33                   0.0016358          0.1743        0.027248        0.037205
v  r12                   -0.010661         0.01359     -0.00023379      -0.0003093
v  r13                   -0.045554        0.052805      9.3103e-05       0.0010137
v  r23                   -0.046691        0.051233      3.0373e-05      0.00057453
v  epsilon                0.068957           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9956e-05       0.0099179      0.00092481       0.0017426
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2788         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8788          0.7135         0.85283


 TIME FOR THE TIME STEP            10456:        0.80716E+02

===============================================================


 INSTANT    0.104570000E-01   TIME STEP NUMBER           10457
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.439367489E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.273717979E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150367976E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184286999E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.298773902E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81160E-03   0.45182E-02 0.19902E+01 
c  Velocity[X]                                      0.13763E-03 
c  Velocity[Y]                                      0.12903E-03 
c  Velocity[Z]                                      0.42515E-02 
c  Pressure     0.36481E-04     133   0.92888E-02   0.25733E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54220E-08   0.16612E-08 0.10038E+00 
c  r22          0.10851E-01      13   0.54937E-08   0.18723E-08 0.10291E+00 
c  r33          0.21859E-01      14   0.70041E-08   0.12819E-07 0.12879E+00 
c  r12          0.93857E-03      18   0.63671E-08   0.29826E-09 0.60570E+00 
c  r13          0.46674E-02      19   0.55800E-08   0.15345E-08 0.20139E+00 
c  r23          0.39975E-02      19   0.64264E-08   0.13049E-08 0.20083E+00 
c  epsilon      0.10970E+02      11   0.34359E-08   0.10171E-01 0.16749E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.83964E-02 0.43271E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63402         0.61361       0.0052562       0.0015073
v  Velocity[Y]            -0.57405         0.54421       0.0030806      0.00087329
v  Velocity[Z]              1.5654          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4377          4.3406          4.3632
v  Pressure                -36.424          359.97          87.625          169.82
v  r11                   0.0010596        0.081923        0.013073        0.018285
v  r22                   0.0011116        0.082639        0.013353        0.018645
v  r33                   0.0016358         0.17427        0.027248        0.037205
v  r12                   -0.010666        0.013591     -0.00023379      -0.0003093
v  r13                   -0.045552        0.052802      9.3104e-05       0.0010137
v  r23                   -0.046691        0.051215      3.0374e-05      0.00057453
v  epsilon                0.068958          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9956e-05       0.0099179      0.00092481       0.0017426
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2784         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8784          0.7135         0.85283


 TIME FOR THE TIME STEP            10457:        0.80824E+02

===============================================================


 INSTANT    0.104580000E-01   TIME STEP NUMBER           10458
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.719870157E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.111735489E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145975852E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108606266E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108514261E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81197E-03   0.45385E-02 0.19947E+01 
c  Velocity[X]                                      0.13830E-03 
c  Velocity[Y]                                      0.12925E-03 
c  Velocity[Z]                                      0.42710E-02 
c  Pressure     0.36640E-04     132   0.93289E-02   0.25845E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51709E-08   0.16236E-08 0.10013E+00 
c  r22          0.10851E-01      13   0.55025E-08   0.18211E-08 0.10226E+00 
c  r33          0.21859E-01      15   0.59807E-08   0.12405E-07 0.12812E+00 
c  r12          0.93857E-03      18   0.62699E-08   0.29416E-09 0.60351E+00 
c  r13          0.46674E-02      19   0.74974E-08   0.14628E-08 0.19922E+00 
c  r23          0.39975E-02      19   0.61833E-08   0.12607E-08 0.19952E+00 
c  epsilon      0.10970E+02      11   0.34665E-08   0.95187E-02 0.16338E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.84431E-02 0.43344E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63408         0.61358       0.0052563       0.0015074
v  Velocity[Y]            -0.57397         0.54428       0.0030806      0.00087328
v  Velocity[Z]              1.5652          5.4377          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4377          4.3406          4.3632
v  Pressure                 -36.44             360          87.643          169.83
v  r11                   0.0010596        0.081935        0.013073        0.018285
v  r22                   0.0011116         0.08264        0.013353        0.018645
v  r33                   0.0016358         0.17429        0.027248        0.037205
v  r12                   -0.010669        0.013591     -0.00023379      -0.0003093
v  r13                    -0.04555        0.052804      9.3105e-05       0.0010137
v  r23                   -0.046691        0.051227      3.0375e-05      0.00057453
v  epsilon                0.068959          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9953e-05        0.009918      0.00092481       0.0017426
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2773         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8773          0.7135         0.85283


 TIME FOR THE TIME STEP            10458:        0.77783E+02

===============================================================


 INSTANT    0.104590000E-01   TIME STEP NUMBER           10459
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.167034419E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.274810637E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133182993E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100043780E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.308686365E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81251E-03   0.45196E-02 0.19918E+01 
c  Velocity[X]                                      0.13772E-03 
c  Velocity[Y]                                      0.12802E-03 
c  Velocity[Z]                                      0.42539E-02 
c  Pressure     0.36702E-04     132   0.93323E-02   0.25888E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52293E-08   0.16532E-08 0.10048E+00 
c  r22          0.10851E-01      13   0.53943E-08   0.18338E-08 0.10195E+00 
c  r33          0.21859E-01      15   0.63481E-08   0.12657E-07 0.12847E+00 
c  r12          0.93857E-03      18   0.62228E-08   0.30496E-09 0.61117E+00 
c  r13          0.46674E-02      19   0.74984E-08   0.14836E-08 0.19912E+00 
c  r23          0.39975E-02      19   0.64040E-08   0.12939E-08 0.20136E+00 
c  epsilon      0.10970E+02      11   0.34031E-08   0.10153E-01 0.17089E+00 
c  TempC        0.25716E+06      16   0.15121E-04   0.84341E-02 0.43293E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161988


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61362       0.0052562       0.0015074
v  Velocity[Y]            -0.57399         0.54439       0.0030806      0.00087329
v  Velocity[Z]              1.5652          5.4377          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4377          4.3406          4.3632
v  Pressure                -36.451          360.07          87.653          169.88
v  r11                   0.0010596        0.081945        0.013073        0.018285
v  r22                   0.0011116        0.082635        0.013353        0.018645
v  r33                   0.0016359         0.17432        0.027248        0.037205
v  r12                   -0.010669        0.013594     -0.00023379      -0.0003093
v  r13                   -0.045553        0.052803      9.3105e-05       0.0010137
v  r23                   -0.046691        0.051212      3.0375e-05      0.00057453
v  epsilon                0.068961          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05       0.0099181      0.00092481       0.0017426
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2771         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8771          0.7135         0.85284


 TIME FOR THE TIME STEP            10459:        0.80383E+02

===============================================================


 INSTANT    0.104600000E-01   TIME STEP NUMBER           10460
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.272496086E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.323808847E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.325805551E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.457082863E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188640943E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81222E-03   0.45228E-02 0.19935E+01 
c  Velocity[X]                                      0.13883E-03 
c  Velocity[Y]                                      0.12871E-03 
c  Velocity[Z]                                      0.42552E-02 
c  Pressure     0.36300E-04     131   0.92346E-02   0.25606E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57637E-08   0.16660E-08 0.10099E+00 
c  r22          0.10851E-01      13   0.53904E-08   0.18487E-08 0.10230E+00 
c  r33          0.21859E-01      15   0.68735E-08   0.12626E-07 0.12836E+00 
c  r12          0.93857E-03      18   0.60606E-08   0.30045E-09 0.61142E+00 
c  r13          0.46674E-02      20   0.63442E-08   0.14993E-08 0.20036E+00 
c  r23          0.39975E-02      19   0.70210E-08   0.12795E-08 0.20031E+00 
c  epsilon      0.10970E+02      11   0.33876E-08   0.99264E-02 0.16567E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.83775E-02 0.43192E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61359       0.0052562       0.0015074
v  Velocity[Y]            -0.57395         0.54418       0.0030807      0.00087334
v  Velocity[Z]               1.565          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4377          4.3406          4.3632
v  Pressure                -36.498          360.04           87.65          169.85
v  r11                   0.0010596        0.081945        0.013073        0.018285
v  r22                   0.0011117        0.082634        0.013353        0.018645
v  r33                   0.0016359         0.17429        0.027248        0.037205
v  r12                   -0.010667        0.013589     -0.00023379      -0.0003093
v  r13                   -0.045551        0.052803      9.3106e-05       0.0010137
v  r23                   -0.046691        0.051199      3.0377e-05      0.00057453
v  epsilon                0.068962          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9948e-05       0.0099183      0.00092481       0.0017426
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2767         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8767          0.7135         0.85283


 TIME FOR THE TIME STEP            10460:        0.78850E+02

===============================================================


 INSTANT    0.104610000E-01   TIME STEP NUMBER           10461
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.180709839E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276307261E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.318829717E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.401826181E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221933790E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81270E-03   0.45076E-02 0.19898E+01 
c  Velocity[X]                                      0.13868E-03 
c  Velocity[Y]                                      0.12969E-03 
c  Velocity[Z]                                      0.42393E-02 
c  Pressure     0.36513E-04     132   0.92971E-02   0.25756E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56211E-08   0.16362E-08 0.10021E+00 
c  r22          0.10851E-01      13   0.58657E-08   0.18196E-08 0.10186E+00 
c  r33          0.21859E-01      15   0.74029E-08   0.12461E-07 0.12789E+00 
c  r12          0.93857E-03      18   0.55451E-08   0.29520E-09 0.60705E+00 
c  r13          0.46674E-02      20   0.59426E-08   0.14754E-08 0.19977E+00 
c  r23          0.39975E-02      20   0.59922E-08   0.12618E-08 0.19970E+00 
c  epsilon      0.10970E+02      11   0.33448E-08   0.96848E-02 0.16275E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84114E-02 0.43322E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63399         0.61361       0.0052562       0.0015074
v  Velocity[Y]            -0.57403         0.54429       0.0030807      0.00087332
v  Velocity[Z]              1.5653          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4377          4.3406          4.3632
v  Pressure                -36.424          360.05          87.667          169.87
v  r11                   0.0010596        0.081947        0.013073        0.018285
v  r22                   0.0011117        0.082635        0.013353        0.018645
v  r33                   0.0016359         0.17427        0.027248        0.037205
v  r12                   -0.010664        0.013581     -0.00023379      -0.0003093
v  r13                   -0.045553        0.052803      9.3107e-05       0.0010137
v  r23                   -0.046692        0.051192      3.0377e-05      0.00057453
v  epsilon                0.068963          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9944e-05       0.0099184      0.00092481       0.0017426
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2769         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8769          0.7135         0.85283


 TIME FOR THE TIME STEP            10461:        0.11456E+03

===============================================================


 INSTANT    0.104620000E-01   TIME STEP NUMBER           10462
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.432062374E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.499395243E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.731416012E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150733851E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.982386650E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81320E-03   0.45108E-02 0.19900E+01 
c  Velocity[X]                                      0.13757E-03 
c  Velocity[Y]                                      0.12811E-03 
c  Velocity[Z]                                      0.42451E-02 
c  Pressure     0.36351E-04     133   0.92511E-02   0.25641E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61631E-08   0.16540E-08 0.10010E+00 
c  r22          0.10851E-01      13   0.60111E-08   0.18582E-08 0.10209E+00 
c  r33          0.21859E-01      15   0.72209E-08   0.12760E-07 0.12812E+00 
c  r12          0.93857E-03      18   0.59633E-08   0.29937E-09 0.60705E+00 
c  r13          0.46674E-02      19   0.67130E-08   0.15128E-08 0.20073E+00 
c  r23          0.39975E-02      19   0.70383E-08   0.12878E-08 0.19992E+00 
c  epsilon      0.10970E+02      11   0.34213E-08   0.10402E-01 0.16930E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.83853E-02 0.43161E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63407          0.6136       0.0052563       0.0015074
v  Velocity[Y]            -0.57399         0.54443       0.0030805      0.00087327
v  Velocity[Z]              1.5656          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4377          4.3406          4.3632
v  Pressure                 -36.47          360.01          87.641          169.84
v  r11                   0.0010596        0.081948        0.013073        0.018285
v  r22                   0.0011117        0.082637        0.013353        0.018645
v  r33                   0.0016359         0.17428        0.027248        0.037205
v  r12                    -0.01066        0.013575     -0.00023379      -0.0003093
v  r13                   -0.045555        0.052802      9.3108e-05       0.0010138
v  r23                   -0.046693        0.051221      3.0378e-05      0.00057453
v  epsilon                0.068964          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099183      0.00092481       0.0017426
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2767         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8767          0.7135         0.85283


 TIME FOR THE TIME STEP            10462:        0.12480E+03

===============================================================


 INSTANT    0.104630000E-01   TIME STEP NUMBER           10463
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136998482E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.721603446E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.880729651E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130738450E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182915143E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81131E-03   0.45410E-02 0.19957E+01 
c  Velocity[X]                                      0.13894E-03 
c  Velocity[Y]                                      0.12839E-03 
c  Velocity[Z]                                      0.42736E-02 
c  Pressure     0.36223E-04     133   0.92181E-02   0.25550E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61764E-08   0.16289E-08 0.99540E-01 
c  r22          0.10851E-01      13   0.58759E-08   0.18531E-08 0.10211E+00 
c  r33          0.21859E-01      16   0.57766E-08   0.12576E-07 0.12756E+00 
c  r12          0.93857E-03      18   0.61469E-08   0.29695E-09 0.60465E+00 
c  r13          0.46674E-02      19   0.62213E-08   0.15093E-08 0.19981E+00 
c  r23          0.39975E-02      20   0.62681E-08   0.12728E-08 0.19865E+00 
c  epsilon      0.10970E+02      11   0.35344E-08   0.98142E-02 0.16491E+00 
c  TempC        0.25716E+06      16   0.15093E-04   0.84643E-02 0.43434E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63404         0.61362       0.0052563       0.0015074
v  Velocity[Y]            -0.57403         0.54415       0.0030806       0.0008733
v  Velocity[Z]              1.5653          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4377          4.3406          4.3632
v  Pressure                -36.423          360.05           87.65          169.87
v  r11                   0.0010596        0.081947        0.013073        0.018285
v  r22                   0.0011117        0.082636        0.013353        0.018645
v  r33                   0.0016359         0.17431        0.027248        0.037205
v  r12                   -0.010657         0.01358     -0.00023379      -0.0003093
v  r13                   -0.045552        0.052799      9.3109e-05       0.0010138
v  r23                   -0.046694        0.051209      3.0379e-05      0.00057453
v  epsilon                0.068965          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099182      0.00092481       0.0017426
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2766         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8766          0.7135         0.85283


 TIME FOR THE TIME STEP            10463:        0.13602E+03

===============================================================


 INSTANT    0.104640000E-01   TIME STEP NUMBER           10464
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.880745313E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.223688119E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.951145986E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.910008087E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.458728699E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81349E-03   0.44949E-02 0.19878E+01 
c  Velocity[X]                                      0.13895E-03 
c  Velocity[Y]                                      0.12866E-03 
c  Velocity[Z]                                      0.42273E-02 
c  Pressure     0.36327E-04     133   0.92563E-02   0.25625E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.62015E-08   0.16413E-08 0.99968E-01 
c  r22          0.10851E-01      13   0.64848E-08   0.18512E-08 0.10217E+00 
c  r33          0.21859E-01      16   0.57870E-08   0.12646E-07 0.12793E+00 
c  r12          0.93857E-03      18   0.58531E-08   0.30121E-09 0.60679E+00 
c  r13          0.46674E-02      19   0.59998E-08   0.15206E-08 0.20104E+00 
c  r23          0.39975E-02      20   0.60124E-08   0.12823E-08 0.19960E+00 
c  epsilon      0.10970E+02      11   0.35548E-08   0.10018E-01 0.16710E+00 
c  TempC        0.25716E+06      16   0.15184E-04   0.84602E-02 0.43391E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63406         0.61358       0.0052563       0.0015074
v  Velocity[Y]            -0.57397         0.54419       0.0030806      0.00087333
v  Velocity[Z]              1.5655          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4377          4.3406          4.3632
v  Pressure                -36.456          359.99          87.626          169.82
v  r11                   0.0010596        0.081944        0.013073        0.018285
v  r22                   0.0011117        0.082636        0.013353        0.018645
v  r33                   0.0016359         0.17435        0.027248        0.037205
v  r12                   -0.010663         0.01358     -0.00023379      -0.0003093
v  r13                   -0.045551          0.0528       9.311e-05       0.0010138
v  r23                   -0.046694        0.051201      3.0381e-05      0.00057454
v  epsilon                0.068966          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099181      0.00092482       0.0017426
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2772         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8772          0.7135         0.85283


 TIME FOR THE TIME STEP            10464:        0.81655E+02

===============================================================


 INSTANT    0.104650000E-01   TIME STEP NUMBER           10465
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.442108210E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136206785E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.595133061E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.639562634E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.168527323E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81155E-03   0.45199E-02 0.19890E+01 
c  Velocity[X]                                      0.13778E-03 
c  Velocity[Y]                                      0.12820E-03 
c  Velocity[Z]                                      0.42539E-02 
c  Pressure     0.36331E-04     131   0.92482E-02   0.25626E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59019E-08   0.16455E-08 0.10001E+00 
c  r22          0.10852E-01      13   0.64290E-08   0.18063E-08 0.10107E+00 
c  r33          0.21859E-01      15   0.73747E-08   0.12566E-07 0.12768E+00 
c  r12          0.93858E-03      18   0.55119E-08   0.29835E-09 0.60351E+00 
c  r13          0.46674E-02      19   0.62610E-08   0.14888E-08 0.19875E+00 
c  r23          0.39975E-02      19   0.74449E-08   0.13012E-08 0.20115E+00 
c  epsilon      0.10970E+02      11   0.35946E-08   0.10215E-01 0.17127E+00 
c  TempC        0.25716E+06      16   0.15105E-04   0.83706E-02 0.43149E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63407          0.6136       0.0052564       0.0015074
v  Velocity[Y]            -0.57401         0.54432       0.0030807      0.00087334
v  Velocity[Z]              1.5655          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4377          4.3406          4.3632
v  Pressure                -36.465          359.98          87.607          169.81
v  r11                   0.0010596        0.081945        0.013073        0.018285
v  r22                   0.0011117        0.082636        0.013353        0.018645
v  r33                   0.0016359         0.17432        0.027248        0.037205
v  r12                   -0.010662        0.013579     -0.00023379      -0.0003093
v  r13                   -0.045555        0.052798      9.3111e-05       0.0010138
v  r23                   -0.046694        0.051227      3.0381e-05      0.00057454
v  epsilon                0.068968          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05        0.009918      0.00092482       0.0017426
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2772         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8772          0.7135         0.85283


 TIME FOR THE TIME STEP            10465:        0.81639E+02

===============================================================


 INSTANT    0.104660000E-01   TIME STEP NUMBER           10466
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.320319069E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.167649627E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.129879254E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.882857388E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.491352006E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81283E-03   0.45515E-02 0.19973E+01 
c  Velocity[X]                                      0.13837E-03 
c  Velocity[Y]                                      0.12914E-03 
c  Velocity[Z]                                      0.42839E-02 
c  Pressure     0.36395E-04     132   0.92582E-02   0.25672E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59375E-08   0.16367E-08 0.99901E-01 
c  r22          0.10852E-01      13   0.62326E-08   0.18228E-08 0.10205E+00 
c  r33          0.21859E-01      15   0.60687E-08   0.12419E-07 0.12770E+00 
c  r12          0.93858E-03      18   0.57803E-08   0.30179E-09 0.60795E+00 
c  r13          0.46674E-02      18   0.71675E-08   0.14770E-08 0.19969E+00 
c  r23          0.39975E-02      19   0.73596E-08   0.12789E-08 0.20024E+00 
c  epsilon      0.10970E+02      11   0.33502E-08   0.96688E-02 0.16471E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.83835E-02 0.43186E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63414         0.61358       0.0052564       0.0015074
v  Velocity[Y]            -0.57392         0.54413       0.0030806       0.0008733
v  Velocity[Z]              1.5654          5.4377          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4377          4.3406          4.3632
v  Pressure                -36.446          360.01          87.664          169.85
v  r11                   0.0010597         0.08195        0.013073        0.018285
v  r22                   0.0011117        0.082635        0.013353        0.018645
v  r33                    0.001636         0.17428        0.027248        0.037205
v  r12                    -0.01066        0.013577     -0.00023379      -0.0003093
v  r13                   -0.045552        0.052799      9.3113e-05       0.0010138
v  r23                   -0.046694        0.051216      3.0383e-05      0.00057454
v  epsilon                0.068969          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099178      0.00092482       0.0017426
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2773         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8773          0.7135         0.85283


 TIME FOR THE TIME STEP            10466:        0.82501E+02

===============================================================


 INSTANT    0.104670000E-01   TIME STEP NUMBER           10467
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.261805106E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.376174202E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.341189975E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.807129100E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110340434E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      45   0.81246E-03   0.45126E-02 0.19897E+01 
c  Velocity[X]                                      0.13798E-03 
c  Velocity[Y]                                      0.12910E-03 
c  Velocity[Z]                                      0.42455E-02 
c  Pressure     0.36443E-04     131   0.92730E-02   0.25705E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56499E-08   0.16608E-08 0.10028E+00 
c  r22          0.10852E-01      13   0.64032E-08   0.18681E-08 0.10240E+00 
c  r33          0.21859E-01      15   0.61003E-08   0.12757E-07 0.12855E+00 
c  r12          0.93858E-03      18   0.58035E-08   0.29969E-09 0.60915E+00 
c  r13          0.46674E-02      19   0.58312E-08   0.15231E-08 0.20132E+00 
c  r23          0.39975E-02      19   0.71295E-08   0.12911E-08 0.20099E+00 
c  epsilon      0.10970E+02      11   0.34169E-08   0.10263E-01 0.16834E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.84559E-02 0.43375E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61357       0.0052563       0.0015074
v  Velocity[Y]            -0.57399         0.54426       0.0030807      0.00087339
v  Velocity[Z]              1.5654          5.4378          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4378          4.3406          4.3632
v  Pressure                -36.425          360.01          87.644          169.85
v  r11                   0.0010597        0.081951        0.013073        0.018285
v  r22                   0.0011117        0.082631        0.013353        0.018645
v  r33                    0.001636         0.17429        0.027248        0.037205
v  r12                   -0.010656        0.013583     -0.00023379      -0.0003093
v  r13                    -0.04555        0.052801      9.3113e-05       0.0010138
v  r23                   -0.046694        0.051203      3.0383e-05      0.00057454
v  epsilon                 0.06897          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099177      0.00092482       0.0017426
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2775         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8775          0.7135         0.85283


 TIME FOR THE TIME STEP            10467:        0.81531E+02

===============================================================


 INSTANT    0.104680000E-01   TIME STEP NUMBER           10468
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.436636150E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.354890363E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.266162848E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.246711689E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.369682090E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81310E-03   0.45131E-02 0.19893E+01 
c  Velocity[X]                                      0.13811E-03 
c  Velocity[Y]                                      0.12767E-03 
c  Velocity[Z]                                      0.42473E-02 
c  Pressure     0.36480E-04     134   0.92869E-02   0.25731E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58330E-08   0.16479E-08 0.99809E-01 
c  r22          0.10852E-01      13   0.61848E-08   0.18406E-08 0.10164E+00 
c  r33          0.21859E-01      15   0.65076E-08   0.12646E-07 0.12802E+00 
c  r12          0.93858E-03      18   0.56119E-08   0.31059E-09 0.61154E+00 
c  r13          0.46674E-02      19   0.58590E-08   0.15215E-08 0.20057E+00 
c  r23          0.39975E-02      19   0.65471E-08   0.12923E-08 0.20071E+00 
c  epsilon      0.10970E+02      11   0.33777E-08   0.10178E-01 0.16750E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.84084E-02 0.43308E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61359       0.0052564       0.0015074
v  Velocity[Y]            -0.57387         0.54444       0.0030807      0.00087337
v  Velocity[Z]              1.5652          5.4378          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4378          4.3406          4.3632
v  Pressure                -36.473          360.04          87.642          169.86
v  r11                   0.0010597        0.081946        0.013073        0.018285
v  r22                   0.0011117        0.082633        0.013353        0.018645
v  r33                    0.001636         0.17432        0.027248        0.037205
v  r12                   -0.010663        0.013581     -0.00023379      -0.0003093
v  r13                   -0.045553        0.052802      9.3114e-05       0.0010138
v  r23                   -0.046694        0.051198      3.0383e-05      0.00057454
v  epsilon                0.068971          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099176      0.00092482       0.0017426
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2776         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8776          0.7135         0.85283


 TIME FOR THE TIME STEP            10468:        0.81323E+02

===============================================================


 INSTANT    0.104690000E-01   TIME STEP NUMBER           10469
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.582989309E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.293825411E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.333286561E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.192636555E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285716885E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81230E-03   0.45187E-02 0.19939E+01 
c  Velocity[X]                                      0.13860E-03 
c  Velocity[Y]                                      0.12854E-03 
c  Velocity[Z]                                      0.42515E-02 
c  Pressure     0.36358E-04     132   0.92540E-02   0.25645E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61778E-08   0.16482E-08 0.10018E+00 
c  r22          0.10852E-01      13   0.60676E-08   0.18514E-08 0.10218E+00 
c  r33          0.21859E-01      15   0.52111E-08   0.12652E-07 0.12855E+00 
c  r12          0.93858E-03      18   0.55489E-08   0.30542E-09 0.61215E+00 
c  r13          0.46674E-02      19   0.53771E-08   0.15207E-08 0.20097E+00 
c  r23          0.39975E-02      19   0.66806E-08   0.12900E-08 0.20177E+00 
c  epsilon      0.10970E+02      11   0.33379E-08   0.96915E-02 0.16377E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.84133E-02 0.43280E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63401         0.61359       0.0052564       0.0015074
v  Velocity[Y]            -0.57388         0.54412       0.0030807      0.00087336
v  Velocity[Z]              1.5654          5.4378          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4378          4.3406          4.3632
v  Pressure                  -36.4          360.01          87.634          169.84
v  r11                   0.0010597         0.08194        0.013073        0.018285
v  r22                   0.0011117        0.082635        0.013353        0.018645
v  r33                    0.001636         0.17429        0.027248        0.037205
v  r12                   -0.010665        0.013579     -0.00023379      -0.0003093
v  r13                   -0.045553        0.052801      9.3114e-05       0.0010138
v  r23                   -0.046693        0.051228      3.0384e-05      0.00057454
v  epsilon                0.068972          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099177      0.00092482       0.0017426
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2773         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8773          0.7135         0.85283


 TIME FOR THE TIME STEP            10469:        0.81159E+02

===============================================================


 INSTANT    0.104700000E-01   TIME STEP NUMBER           10470
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.188369187E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.210113563E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.265069677E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.322434179E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.265880146E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81208E-03   0.45521E-02 0.19988E+01 
c  Velocity[X]                                      0.13945E-03 
c  Velocity[Y]                                      0.13000E-03 
c  Velocity[Z]                                      0.42827E-02 
c  Pressure     0.36268E-04     133   0.92388E-02   0.25582E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56345E-08   0.16497E-08 0.10029E+00 
c  r22          0.10852E-01      13   0.56461E-08   0.18462E-08 0.10185E+00 
c  r33          0.21859E-01      15   0.61194E-08   0.12602E-07 0.12792E+00 
c  r12          0.93858E-03      18   0.52623E-08   0.30290E-09 0.60729E+00 
c  r13          0.46674E-02      19   0.67011E-08   0.15031E-08 0.20009E+00 
c  r23          0.39975E-02      19   0.60387E-08   0.12648E-08 0.19926E+00 
c  epsilon      0.10970E+02      11   0.34708E-08   0.98624E-02 0.16485E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84383E-02 0.43338E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63403         0.61358       0.0052564       0.0015074
v  Velocity[Y]            -0.57385         0.54418       0.0030807      0.00087337
v  Velocity[Z]              1.5654          5.4378          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4378          4.3406          4.3632
v  Pressure                 -36.46          360.02           87.65          169.85
v  r11                   0.0010597        0.081938        0.013073        0.018285
v  r22                   0.0011117        0.082637        0.013353        0.018645
v  r33                    0.001636         0.17427        0.027248        0.037205
v  r12                   -0.010667        0.013578     -0.00023379      -0.0003093
v  r13                   -0.045551        0.052802      9.3116e-05       0.0010138
v  r23                   -0.046693        0.051221      3.0385e-05      0.00057454
v  epsilon                0.068973          271.19          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099177      0.00092482       0.0017426
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2772         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8772          0.7135         0.85283


 TIME FOR THE TIME STEP            10470:        0.81679E+02

===============================================================


 INSTANT    0.104710000E-01   TIME STEP NUMBER           10471
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.212430749E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.334202115E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.307856455E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935019E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.895952315E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.177156063E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81303E-03   0.45206E-02 0.19931E+01 
c  Velocity[X]                                      0.13781E-03 
c  Velocity[Y]                                      0.12839E-03 
c  Velocity[Z]                                      0.42544E-02 
c  Pressure     0.36791E-04     133   0.93591E-02   0.25951E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56017E-08   0.16762E-08 0.10051E+00 
c  r22          0.10852E-01      13   0.55266E-08   0.18542E-08 0.10221E+00 
c  r33          0.21859E-01      15   0.58584E-08   0.12739E-07 0.12866E+00 
c  r12          0.93858E-03      18   0.54210E-08   0.30622E-09 0.60993E+00 
c  r13          0.46674E-02      19   0.58837E-08   0.15215E-08 0.20079E+00 
c  r23          0.39975E-02      19   0.64472E-08   0.13081E-08 0.20202E+00 
c  epsilon      0.10970E+02      11   0.34417E-08   0.10233E-01 0.17101E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.84436E-02 0.43329E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63404         0.61364       0.0052564       0.0015074
v  Velocity[Y]             -0.5739          0.5443       0.0030808      0.00087347
v  Velocity[Z]              1.5652          5.4378          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4378          4.3406          4.3632
v  Pressure                -36.408          360.01          87.624          169.84
v  r11                   0.0010597        0.081939        0.013073        0.018285
v  r22                   0.0011117        0.082638        0.013353        0.018645
v  r33                    0.001636         0.17428        0.027248        0.037205
v  r12                   -0.010666        0.013584     -0.00023379      -0.0003093
v  r13                   -0.045553        0.052801      9.3117e-05       0.0010138
v  r23                   -0.046694        0.051213      3.0386e-05      0.00057454
v  epsilon                0.068974          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099177      0.00092482       0.0017426
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2768         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8768          0.7135         0.85283


 TIME FOR THE TIME STEP            10471:        0.81078E+02

===============================================================


 INSTANT    0.104720000E-01   TIME STEP NUMBER           10472
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145683634E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.536831686E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.304600310E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.244888833E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.508893137E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81247E-03   0.45220E-02 0.19927E+01 
c  Velocity[X]                                      0.13822E-03 
c  Velocity[Y]                                      0.12918E-03 
c  Velocity[Z]                                      0.42546E-02 
c  Pressure     0.36481E-04     132   0.92933E-02   0.25733E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57935E-08   0.16372E-08 0.99419E-01 
c  r22          0.10852E-01      13   0.58125E-08   0.18462E-08 0.10186E+00 
c  r33          0.21859E-01      15   0.72104E-08   0.12606E-07 0.12764E+00 
c  r12          0.93858E-03      18   0.58305E-08   0.30051E-09 0.60543E+00 
c  r13          0.46674E-02      19   0.62866E-08   0.15039E-08 0.19958E+00 
c  r23          0.39975E-02      19   0.66528E-08   0.12789E-08 0.19949E+00 
c  epsilon      0.10970E+02      11   0.34250E-08   0.10016E-01 0.16668E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.84018E-02 0.43264E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63413          0.6136       0.0052563       0.0015074
v  Velocity[Y]            -0.57381         0.54412       0.0030808      0.00087346
v  Velocity[Z]              1.5653          5.4378          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4378          4.3406          4.3632
v  Pressure                -36.421          359.96          87.621          169.81
v  r11                   0.0010597        0.081935        0.013073        0.018285
v  r22                   0.0011118        0.082639        0.013353        0.018645
v  r33                    0.001636          0.1743        0.027248        0.037205
v  r12                   -0.010665        0.013583     -0.00023379      -0.0003093
v  r13                    -0.04555        0.052801      9.3117e-05       0.0010138
v  r23                   -0.046694        0.051201      3.0386e-05      0.00057454
v  epsilon                0.068976          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099178      0.00092482       0.0017426
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2773         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8773          0.7135         0.85283


 TIME FOR THE TIME STEP            10472:        0.84502E+02

===============================================================


 INSTANT    0.104730000E-01   TIME STEP NUMBER           10473
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.541532690E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.204385326E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.291173877E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.479825290E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.647287278E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81302E-03   0.44957E-02 0.19863E+01 
c  Velocity[X]                                      0.13921E-03 
c  Velocity[Y]                                      0.12856E-03 
c  Velocity[Z]                                      0.42279E-02 
c  Pressure     0.36376E-04     131   0.92522E-02   0.25659E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55949E-08   0.16476E-08 0.99603E-01 
c  r22          0.10852E-01      13   0.54883E-08   0.18425E-08 0.10192E+00 
c  r33          0.21859E-01      15   0.65045E-08   0.12588E-07 0.12771E+00 
c  r12          0.93858E-03      18   0.56533E-08   0.30018E-09 0.60545E+00 
c  r13          0.46674E-02      19   0.58689E-08   0.14964E-08 0.19955E+00 
c  r23          0.39975E-02      19   0.57459E-08   0.12759E-08 0.19989E+00 
c  epsilon      0.10970E+02      11   0.33074E-08   0.98093E-02 0.16424E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.84465E-02 0.43387E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63409         0.61359       0.0052563       0.0015074
v  Velocity[Y]            -0.57391         0.54416       0.0030808      0.00087344
v  Velocity[Z]              1.5652          5.4378          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4378          4.3406          4.3632
v  Pressure                -36.399          360.03          87.661          169.86
v  r11                   0.0010597        0.081932        0.013073        0.018285
v  r22                   0.0011118        0.082641        0.013353        0.018645
v  r33                   0.0016361         0.17434        0.027248        0.037205
v  r12                   -0.010661        0.013584     -0.00023379      -0.0003093
v  r13                   -0.045551        0.052803      9.3118e-05       0.0010138
v  r23                   -0.046695        0.051222      3.0387e-05      0.00057454
v  epsilon                0.068977          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9941e-05       0.0099179      0.00092483       0.0017426
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2775         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8775          0.7135         0.85283


 TIME FOR THE TIME STEP            10473:        0.82122E+02

===============================================================


 INSTANT    0.104740000E-01   TIME STEP NUMBER           10474
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.235294699E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.113131525E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.121772279E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.966424297E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154865375E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81239E-03   0.45361E-02 0.19941E+01 
c  Velocity[X]                                      0.13869E-03 
c  Velocity[Y]                                      0.12820E-03 
c  Velocity[Z]                                      0.42692E-02 
c  Pressure     0.36214E-04     132   0.92179E-02   0.25543E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58232E-08   0.16310E-08 0.99609E-01 
c  r22          0.10852E-01      13   0.53562E-08   0.18188E-08 0.10125E+00 
c  r33          0.21859E-01      15   0.52274E-08   0.12500E-07 0.12716E+00 
c  r12          0.93858E-03      18   0.57689E-08   0.29186E-09 0.59881E+00 
c  r13          0.46674E-02      19   0.54195E-08   0.14935E-08 0.19873E+00 
c  r23          0.39975E-02      19   0.56655E-08   0.12833E-08 0.19996E+00 
c  epsilon      0.10970E+02      11   0.32369E-08   0.98001E-02 0.16497E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.83725E-02 0.43137E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63412         0.61364       0.0052563       0.0015074
v  Velocity[Y]            -0.57389         0.54426       0.0030808      0.00087345
v  Velocity[Z]              1.5654          5.4378          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4378          4.3406          4.3632
v  Pressure                -36.455          359.98          87.626          169.82
v  r11                   0.0010597        0.081926        0.013073        0.018285
v  r22                   0.0011118        0.082643        0.013353        0.018645
v  r33                   0.0016361         0.17432        0.027248        0.037205
v  r12                   -0.010665        0.013582     -0.00023379      -0.0003093
v  r13                   -0.045553        0.052805      9.3119e-05       0.0010138
v  r23                   -0.046696        0.051208      3.0388e-05      0.00057454
v  epsilon                0.068978          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9944e-05       0.0099179      0.00092483       0.0017426
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2778         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8778          0.7135         0.85283


 TIME FOR THE TIME STEP            10474:        0.82012E+02

===============================================================


 INSTANT    0.104750000E-01   TIME STEP NUMBER           10475
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242123551E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.797968325E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.471209681E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153388551E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201383483E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81244E-03   0.45342E-02 0.19959E+01 
c  Velocity[X]                                      0.13785E-03 
c  Velocity[Y]                                      0.12904E-03 
c  Velocity[Z]                                      0.42673E-02 
c  Pressure     0.36516E-04     133   0.92921E-02   0.25757E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58452E-08   0.16484E-08 0.99629E-01 
c  r22          0.10852E-01      13   0.52570E-08   0.18520E-08 0.10181E+00 
c  r33          0.21859E-01      15   0.52179E-08   0.12684E-07 0.12772E+00 
c  r12          0.93858E-03      18   0.60520E-08   0.30240E-09 0.60501E+00 
c  r13          0.46674E-02      19   0.57514E-08   0.15182E-08 0.20047E+00 
c  r23          0.39975E-02      19   0.51002E-08   0.12997E-08 0.20024E+00 
c  epsilon      0.10970E+02      11   0.33761E-08   0.10192E-01 0.16713E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.83850E-02 0.43183E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6341         0.61363       0.0052564       0.0015074
v  Velocity[Y]            -0.57384         0.54432       0.0030808      0.00087347
v  Velocity[Z]              1.5655          5.4379          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4379          4.3406          4.3632
v  Pressure                -36.378          360.05          87.661          169.88
v  r11                   0.0010597        0.081928        0.013073        0.018285
v  r22                   0.0011118         0.08264        0.013353        0.018645
v  r33                   0.0016361         0.17429        0.027248        0.037205
v  r12                   -0.010664        0.013585     -0.00023379      -0.0003093
v  r13                   -0.045551        0.052807      9.3119e-05       0.0010138
v  r23                   -0.046697        0.051194      3.0388e-05      0.00057454
v  epsilon                0.068979          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9949e-05        0.009918      0.00092483       0.0017426
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2784         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8784          0.7135         0.85283


 TIME FOR THE TIME STEP            10475:        0.81109E+02

===============================================================


 INSTANT    0.104760000E-01   TIME STEP NUMBER           10476
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169005883E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.114959629E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.257276921E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115421333E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.212328943E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81317E-03   0.45285E-02 0.19928E+01 
c  Velocity[X]                                      0.13903E-03 
c  Velocity[Y]                                      0.12871E-03 
c  Velocity[Z]                                      0.42607E-02 
c  Pressure     0.36767E-04     131   0.93618E-02   0.25935E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61645E-08   0.16301E-08 0.99334E-01 
c  r22          0.10852E-01      13   0.51497E-08   0.18427E-08 0.10201E+00 
c  r33          0.21859E-01      15   0.58034E-08   0.12512E-07 0.12748E+00 
c  r12          0.93858E-03      18   0.66338E-08   0.29271E-09 0.59877E+00 
c  r13          0.46674E-02      19   0.64662E-08   0.15070E-08 0.20061E+00 
c  r23          0.39975E-02      19   0.60880E-08   0.12823E-08 0.19891E+00 
c  epsilon      0.10970E+02      11   0.33996E-08   0.98226E-02 0.16435E+00 
c  TempC        0.25716E+06      16   0.15177E-04   0.84204E-02 0.43318E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63407          0.6136       0.0052564       0.0015074
v  Velocity[Y]            -0.57377         0.54414       0.0030808      0.00087347
v  Velocity[Z]              1.5654          5.4379          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4379          4.3406          4.3632
v  Pressure                -36.445          360.07          87.685           169.9
v  r11                   0.0010597        0.081923        0.013073        0.018285
v  r22                   0.0011118        0.082643        0.013353        0.018645
v  r33                   0.0016361          0.1743        0.027248        0.037205
v  r12                   -0.010662        0.013584     -0.00023379      -0.0003093
v  r13                   -0.045549        0.052809       9.312e-05       0.0010138
v  r23                   -0.046698         0.05122      3.0389e-05      0.00057454
v  epsilon                 0.06898          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9949e-05        0.009918      0.00092483       0.0017426
v  CourantNb               0.44218             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2783         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8783          0.7135         0.85283


 TIME FOR THE TIME STEP            10476:        0.82344E+02

===============================================================


 INSTANT    0.104770000E-01   TIME STEP NUMBER           10477
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.380520541E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.110346696E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.344329972E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935019E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.142309281E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155011915E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81215E-03   0.45075E-02 0.19882E+01 
c  Velocity[X]                                      0.13730E-03 
c  Velocity[Y]                                      0.12809E-03 
c  Velocity[Z]                                      0.42421E-02 
c  Pressure     0.36318E-04     131   0.92378E-02   0.25616E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.63622E-08   0.16548E-08 0.10015E+00 
c  r22          0.10852E-01      13   0.50846E-08   0.18080E-08 0.10102E+00 
c  r33          0.21859E-01      15   0.56548E-08   0.12484E-07 0.12722E+00 
c  r12          0.93858E-03      18   0.63357E-08   0.29960E-09 0.60283E+00 
c  r13          0.46674E-02      19   0.64210E-08   0.14883E-08 0.19915E+00 
c  r23          0.39975E-02      19   0.56876E-08   0.12964E-08 0.20084E+00 
c  epsilon      0.10969E+02      11   0.33768E-08   0.10080E-01 0.17064E+00 
c  TempC        0.25716E+06      16   0.15104E-04   0.84435E-02 0.43355E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63406         0.61364       0.0052564       0.0015074
v  Velocity[Y]            -0.57388         0.54425       0.0030808      0.00087343
v  Velocity[Z]              1.5653          5.4379          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4379          4.3406          4.3632
v  Pressure                 -36.43          360.01          87.617          169.83
v  r11                   0.0010597        0.081924        0.013073        0.018285
v  r22                   0.0011118        0.082647        0.013353        0.018645
v  r33                   0.0016361         0.17432        0.027248        0.037205
v  r12                    -0.01066        0.013585     -0.00023379      -0.0003093
v  r13                   -0.045553        0.052809      9.3121e-05       0.0010138
v  r23                   -0.046699        0.051211       3.039e-05      0.00057454
v  epsilon                0.068981          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05        0.009918      0.00092483       0.0017426
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2772         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8772          0.7135         0.85283


 TIME FOR THE TIME STEP            10477:        0.81524E+02

===============================================================


 INSTANT    0.104780000E-01   TIME STEP NUMBER           10478
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.520644538E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171636634E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.270957128E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.144886122E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.161423537E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81233E-03   0.45197E-02 0.19917E+01 
c  Velocity[X]                                      0.13812E-03 
c  Velocity[Y]                                      0.12945E-03 
c  Velocity[Z]                                      0.42522E-02 
c  Pressure     0.36412E-04     132   0.92733E-02   0.25685E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59673E-08   0.16056E-08 0.98912E-01 
c  r22          0.10852E-01      13   0.54847E-08   0.17920E-08 0.10095E+00 
c  r33          0.21859E-01      14   0.69404E-08   0.12245E-07 0.12638E+00 
c  r12          0.93858E-03      18   0.59662E-08   0.28605E-09 0.59395E+00 
c  r13          0.46674E-02      19   0.61438E-08   0.14681E-08 0.19859E+00 
c  r23          0.39975E-02      19   0.71263E-08   0.12666E-08 0.19816E+00 
c  epsilon      0.10969E+02      11   0.32178E-08   0.95991E-02 0.16471E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.84126E-02 0.43296E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63414         0.61359       0.0052563       0.0015074
v  Velocity[Y]            -0.57383         0.54399       0.0030807      0.00087337
v  Velocity[Z]              1.5649          5.4379          4.3388          4.3625
v  ǁVelocityǁ               1.5787          5.4379          4.3406          4.3632
v  Pressure                -36.463          359.96          87.617           169.8
v  r11                   0.0010597        0.081925        0.013073        0.018285
v  r22                   0.0011118        0.082649        0.013353        0.018645
v  r33                   0.0016361          0.1743        0.027248        0.037205
v  r12                   -0.010659        0.013583     -0.00023379      -0.0003093
v  r13                    -0.04555        0.052809      9.3121e-05       0.0010138
v  r23                     -0.0467        0.051199      3.0391e-05      0.00057454
v  epsilon                0.068983          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9951e-05        0.009918      0.00092483       0.0017426
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2762         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8762          0.7135         0.85283


 TIME FOR THE TIME STEP            10478:        0.83396E+02

===============================================================


 INSTANT    0.104790000E-01   TIME STEP NUMBER           10479
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.912873823E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.380571241E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.282884052E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.724808389E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.375955977E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81206E-03   0.45548E-02 0.19993E+01 
c  Velocity[X]                                      0.13940E-03 
c  Velocity[Y]                                      0.12887E-03 
c  Velocity[Z]                                      0.42866E-02 
c  Pressure     0.36571E-04     132   0.93148E-02   0.25797E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61754E-08   0.16195E-08 0.99302E-01 
c  r22          0.10852E-01      13   0.56213E-08   0.18316E-08 0.10143E+00 
c  r33          0.21859E-01      14   0.69321E-08   0.12459E-07 0.12683E+00 
c  r12          0.93858E-03      18   0.63831E-08   0.29440E-09 0.60003E+00 
c  r13          0.46674E-02      19   0.55279E-08   0.15093E-08 0.19986E+00 
c  r23          0.39975E-02      20   0.58019E-08   0.12677E-08 0.19829E+00 
c  epsilon      0.10969E+02      11   0.32570E-08   0.99095E-02 0.16480E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.84564E-02 0.43360E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162017


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63412         0.61358       0.0052563       0.0015074
v  Velocity[Y]            -0.57386         0.54406       0.0030808      0.00087344
v  Velocity[Z]               1.565          5.4379          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4379          4.3406          4.3632
v  Pressure                 -36.42          360.09          87.682           169.9
v  r11                   0.0010597        0.081927        0.013073        0.018285
v  r22                   0.0011118         0.08265        0.013353        0.018645
v  r33                   0.0016361         0.17427        0.027248        0.037205
v  r12                   -0.010656         0.01359     -0.00023379      -0.0003093
v  r13                    -0.04555        0.052809      9.3122e-05       0.0010138
v  r23                   -0.046701        0.051226      3.0392e-05      0.00057455
v  epsilon                0.068984          271.18          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9953e-05       0.0099179      0.00092483       0.0017426
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2762         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8762          0.7135         0.85283


 TIME FOR THE TIME STEP            10479:        0.82013E+02

===============================================================


 INSTANT    0.104800000E-01   TIME STEP NUMBER           10480
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.380459473E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239941561E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115307682E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.360532057E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.443402193E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81249E-03   0.45047E-02 0.19880E+01 
c  Velocity[X]                                      0.13841E-03 
c  Velocity[Y]                                      0.12819E-03 
c  Velocity[Z]                                      0.42381E-02 
c  Pressure     0.36304E-04     131   0.92459E-02   0.25608E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59484E-08   0.16419E-08 0.99632E-01 
c  r22          0.10852E-01      13   0.55045E-08   0.18459E-08 0.10191E+00 
c  r33          0.21859E-01      15   0.51701E-08   0.12639E-07 0.12762E+00 
c  r12          0.93858E-03      18   0.60828E-08   0.29950E-09 0.60381E+00 
c  r13          0.46674E-02      19   0.62292E-08   0.15160E-08 0.20054E+00 
c  r23          0.39975E-02      20   0.56512E-08   0.12825E-08 0.19939E+00 
c  epsilon      0.10969E+02      11   0.33538E-08   0.10103E-01 0.16636E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.83784E-02 0.43215E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63407         0.61363       0.0052563       0.0015074
v  Velocity[Y]            -0.57366         0.54424       0.0030808      0.00087343
v  Velocity[Z]              1.5651          5.4379          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4379          4.3406          4.3632
v  Pressure                -36.429          360.04          87.663          169.87
v  r11                   0.0010598        0.081929        0.013073        0.018285
v  r22                   0.0011118        0.082651        0.013353        0.018645
v  r33                   0.0016362         0.17428        0.027248        0.037205
v  r12                   -0.010657        0.013588     -0.00023379      -0.0003093
v  r13                   -0.045552         0.05281      9.3123e-05       0.0010138
v  r23                   -0.046702        0.051216      3.0392e-05      0.00057455
v  epsilon                0.068985           271.2          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9953e-05       0.0099179      0.00092483       0.0017426
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017845           5.277         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.877          0.7135         0.85283


 TIME FOR THE TIME STEP            10480:        0.85030E+02

===============================================================


 INSTANT    0.104810000E-01   TIME STEP NUMBER           10481
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.506947811E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173875030E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.253051097E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.163463308E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.142796265E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81222E-03   0.45142E-02 0.19902E+01 
c  Velocity[X]                                      0.13812E-03 
c  Velocity[Y]                                      0.12786E-03 
c  Velocity[Z]                                      0.42483E-02 
c  Pressure     0.36388E-04     133   0.92573E-02   0.25668E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54308E-08   0.16198E-08 0.99083E-01 
c  r22          0.10852E-01      13   0.57893E-08   0.18318E-08 0.10178E+00 
c  r33          0.21859E-01      15   0.53111E-08   0.12512E-07 0.12726E+00 
c  r12          0.93858E-03      18   0.57131E-08   0.29904E-09 0.60302E+00 
c  r13          0.46674E-02      19   0.58126E-08   0.15046E-08 0.19990E+00 
c  r23          0.39975E-02      19   0.67961E-08   0.12847E-08 0.19961E+00 
c  epsilon      0.10969E+02      11   0.34332E-08   0.98226E-02 0.16465E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84013E-02 0.43240E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162016


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63408         0.61362       0.0052563       0.0015074
v  Velocity[Y]             -0.5737         0.54437       0.0030808      0.00087342
v  Velocity[Z]               1.565          5.4379          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4379          4.3406          4.3632
v  Pressure                -36.396          360.06           87.66          169.87
v  r11                   0.0010598        0.081926        0.013073        0.018285
v  r22                   0.0011118        0.082646        0.013353        0.018645
v  r33                   0.0016362         0.17431        0.027248        0.037205
v  r12                   -0.010655        0.013586     -0.00023379      -0.0003093
v  r13                   -0.045551         0.05281      9.3123e-05       0.0010138
v  r23                   -0.046702        0.051209      3.0393e-05      0.00057455
v  epsilon                0.068986          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9953e-05       0.0099177      0.00092483       0.0017426
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2769         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8769         0.71351         0.85284


 TIME FOR THE TIME STEP            10481:        0.83233E+02

===============================================================


 INSTANT    0.104820000E-01   TIME STEP NUMBER           10482
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172764374E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.198364067E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.130551337E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.362531563E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.409426555E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81259E-03   0.45382E-02 0.19945E+01 
c  Velocity[X]                                      0.13890E-03 
c  Velocity[Y]                                      0.12907E-03 
c  Velocity[Z]                                      0.42703E-02 
c  Pressure     0.36237E-04     133   0.92295E-02   0.25561E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54699E-08   0.16205E-08 0.99137E-01 
c  r22          0.10852E-01      13   0.54136E-08   0.18118E-08 0.10068E+00 
c  r33          0.21859E-01      15   0.57349E-08   0.12464E-07 0.12638E+00 
c  r12          0.93858E-03      18   0.54419E-08   0.29546E-09 0.60183E+00 
c  r13          0.46674E-02      18   0.68939E-08   0.15079E-08 0.19906E+00 
c  r23          0.39975E-02      19   0.58979E-08   0.12793E-08 0.19876E+00 
c  epsilon      0.10969E+02      11   0.35136E-08   0.10098E-01 0.16642E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84696E-02 0.43417E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63413         0.61361       0.0052563       0.0015074
v  Velocity[Y]            -0.57371         0.54415       0.0030808      0.00087342
v  Velocity[Z]              1.5651          5.4379          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4379          4.3406          4.3632
v  Pressure                -36.458          360.01          87.645          169.83
v  r11                   0.0010598        0.081933        0.013073        0.018285
v  r22                   0.0011118         0.08265        0.013353        0.018645
v  r33                   0.0016362         0.17434        0.027248        0.037205
v  r12                   -0.010653        0.013585     -0.00023379      -0.0003093
v  r13                   -0.045549        0.052814      9.3124e-05       0.0010138
v  r23                   -0.046701        0.051225      3.0395e-05      0.00057455
v  epsilon                0.068987          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9954e-05       0.0099176      0.00092484       0.0017426
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2774         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8774         0.71351         0.85284


 TIME FOR THE TIME STEP            10482:        0.83060E+02

===============================================================


 INSTANT    0.104830000E-01   TIME STEP NUMBER           10483
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.937855731E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.555265339E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.177080400E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.257027180E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239389004E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81266E-03   0.45136E-02 0.19882E+01 
c  Velocity[X]                                      0.13790E-03 
c  Velocity[Y]                                      0.12815E-03 
c  Velocity[Z]                                      0.42476E-02 
c  Pressure     0.36500E-04     133   0.92901E-02   0.25746E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52938E-08   0.16420E-08 0.99813E-01 
c  r22          0.10852E-01      13   0.52206E-08   0.17980E-08 0.10075E+00 
c  r33          0.21859E-01      14   0.65540E-08   0.12418E-07 0.12717E+00 
c  r12          0.93858E-03      18   0.58479E-08   0.29951E-09 0.60415E+00 
c  r13          0.46674E-02      19   0.58756E-08   0.14719E-08 0.19870E+00 
c  r23          0.39975E-02      19   0.57870E-08   0.12786E-08 0.20050E+00 
c  epsilon      0.10969E+02      11   0.33852E-08   0.10052E-01 0.16967E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.83881E-02 0.43275E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6341         0.61365       0.0052563       0.0015073
v  Velocity[Y]            -0.57377         0.54432       0.0030809      0.00087343
v  Velocity[Z]              1.5652          5.4379          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4379          4.3406          4.3632
v  Pressure                -36.409          359.97          87.613          169.81
v  r11                   0.0010598         0.08193        0.013073        0.018285
v  r22                   0.0011118        0.082652        0.013353        0.018645
v  r33                   0.0016362         0.17432        0.027248        0.037205
v  r12                   -0.010653         0.01359     -0.00023379      -0.0003093
v  r13                   -0.045552        0.052812      9.3125e-05       0.0010138
v  r23                     -0.0467        0.051214      3.0395e-05      0.00057455
v  epsilon                0.068988          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9958e-05       0.0099175      0.00092484       0.0017426
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2775         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8775          0.7135         0.85283


 TIME FOR THE TIME STEP            10483:        0.81445E+02

===============================================================


 INSTANT    0.104840000E-01   TIME STEP NUMBER           10484
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.400094468E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.298410307E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934894E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.113019695E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.124001304E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.321473850E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81273E-03   0.45437E-02 0.19948E+01 
c  Velocity[X]                                      0.13839E-03 
c  Velocity[Y]                                      0.12857E-03 
c  Velocity[Z]                                      0.42767E-02 
c  Pressure     0.36776E-04     133   0.93617E-02   0.25942E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55165E-08   0.16148E-08 0.99384E-01 
c  r22          0.10852E-01      13   0.49503E-08   0.18207E-08 0.10145E+00 
c  r33          0.21859E-01      14   0.70669E-08   0.12509E-07 0.12780E+00 
c  r12          0.93858E-03      18   0.62476E-08   0.29572E-09 0.60164E+00 
c  r13          0.46674E-02      19   0.67176E-08   0.15161E-08 0.20119E+00 
c  r23          0.39975E-02      19   0.60691E-08   0.12899E-08 0.20084E+00 
c  epsilon      0.10969E+02      11   0.34279E-08   0.99773E-02 0.16652E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.84215E-02 0.43273E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162019


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63415         0.61361       0.0052563       0.0015073
v  Velocity[Y]            -0.57372         0.54401       0.0030808      0.00087341
v  Velocity[Z]              1.5651          5.4379          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4379          4.3406          4.3632
v  Pressure                -36.444          360.03          87.679          169.88
v  r11                   0.0010598        0.081917        0.013073        0.018285
v  r22                   0.0011119        0.082654        0.013353        0.018645
v  r33                   0.0016362         0.17427        0.027249        0.037205
v  r12                   -0.010653        0.013589     -0.00023379      -0.0003093
v  r13                   -0.045549        0.052813      9.3125e-05       0.0010138
v  r23                     -0.0467        0.051208      3.0395e-05      0.00057455
v  epsilon                 0.06899          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9958e-05       0.0099176      0.00092484       0.0017426
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2771         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8771          0.7135         0.85283


 TIME FOR THE TIME STEP            10484:        0.81594E+02

===============================================================


 INSTANT    0.104850000E-01   TIME STEP NUMBER           10485
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.806200505E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.199903480E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.391262142E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.904559225E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.240647310E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81117E-03   0.45329E-02 0.19905E+01 
c  Velocity[X]                                      0.13937E-03 
c  Velocity[Y]                                      0.12890E-03 
c  Velocity[Z]                                      0.42646E-02 
c  Pressure     0.36044E-04     133   0.91723E-02   0.25424E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54454E-08   0.16279E-08 0.99281E-01 
c  r22          0.10852E-01      13   0.50455E-08   0.18128E-08 0.10090E+00 
c  r33          0.21859E-01      14   0.67303E-08   0.12463E-07 0.12682E+00 
c  r12          0.93858E-03      18   0.62507E-08   0.29405E-09 0.60109E+00 
c  r13          0.46674E-02      19   0.60609E-08   0.15128E-08 0.20019E+00 
c  r23          0.39975E-02      19   0.60358E-08   0.12816E-08 0.19912E+00 
c  epsilon      0.10969E+02      11   0.33691E-08   0.99028E-02 0.16391E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.84273E-02 0.43294E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63419          0.6136       0.0052563       0.0015073
v  Velocity[Y]            -0.57382         0.54404       0.0030808       0.0008734
v  Velocity[Z]              1.5651          5.4379          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4379          4.3406          4.3632
v  Pressure                -36.418          360.05          87.659          169.87
v  r11                   0.0010598        0.081913        0.013073        0.018285
v  r22                   0.0011119        0.082655        0.013353        0.018645
v  r33                   0.0016362         0.17428        0.027249        0.037205
v  r12                    -0.01065        0.013595      -0.0002338      -0.0003093
v  r13                   -0.045551        0.052813      9.3126e-05       0.0010138
v  r23                     -0.0467        0.051202      3.0396e-05      0.00057455
v  epsilon                0.068991          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099176      0.00092484       0.0017426
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2773         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8773          0.7135         0.85283


 TIME FOR THE TIME STEP            10485:        0.81033E+02

===============================================================


 INSTANT    0.104860000E-01   TIME STEP NUMBER           10486
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.818082763E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.346079752E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.688880323E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183536515E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172970033E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81353E-03   0.45161E-02 0.19904E+01 
c  Velocity[X]                                      0.13797E-03 
c  Velocity[Y]                                      0.12831E-03 
c  Velocity[Z]                                      0.42498E-02 
c  Pressure     0.36337E-04     132   0.92522E-02   0.25630E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55817E-08   0.16149E-08 0.99529E-01 
c  r22          0.10852E-01      13   0.49036E-08   0.18173E-08 0.10122E+00 
c  r33          0.21859E-01      15   0.57018E-08   0.12468E-07 0.12731E+00 
c  r12          0.93858E-03      18   0.60214E-08   0.28900E-09 0.60028E+00 
c  r13          0.46674E-02      19   0.67541E-08   0.15014E-08 0.20011E+00 
c  r23          0.39975E-02      19   0.64576E-08   0.12662E-08 0.19946E+00 
c  epsilon      0.10969E+02      11   0.34536E-08   0.98442E-02 0.16395E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.83714E-02 0.43150E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162015


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63402         0.61364       0.0052563       0.0015073
v  Velocity[Y]            -0.57379         0.54424       0.0030807      0.00087335
v  Velocity[Z]              1.5652          5.4379          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4379          4.3406          4.3632
v  Pressure                -36.437          360.02          87.665          169.86
v  r11                   0.0010598        0.081906        0.013073        0.018285
v  r22                   0.0011119        0.082656        0.013353        0.018645
v  r33                   0.0016362         0.17432        0.027249        0.037205
v  r12                   -0.010653        0.013591      -0.0002338      -0.0003093
v  r13                   -0.045553        0.052813      9.3127e-05       0.0010138
v  r23                     -0.0467        0.051232      3.0397e-05      0.00057455
v  epsilon                0.068992           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9962e-05       0.0099177      0.00092484       0.0017426
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2779         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8779          0.7135         0.85283


 TIME FOR THE TIME STEP            10486:        0.78994E+02

===============================================================


 INSTANT    0.104870000E-01   TIME STEP NUMBER           10487
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.306313201E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.245623693E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160775963E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.510391647E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.214364258E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81201E-03   0.45141E-02 0.19916E+01 
c  Velocity[X]                                      0.13778E-03 
c  Velocity[Y]                                      0.12876E-03 
c  Velocity[Z]                                      0.42476E-02 
c  Pressure     0.36156E-04     133   0.92002E-02   0.25503E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60173E-08   0.16357E-08 0.10038E+00 
c  r22          0.10852E-01      13   0.51666E-08   0.18253E-08 0.10174E+00 
c  r33          0.21859E-01      15   0.63072E-08   0.12459E-07 0.12800E+00 
c  r12          0.93858E-03      18   0.62735E-08   0.29956E-09 0.60742E+00 
c  r13          0.46674E-02      20   0.56792E-08   0.14995E-08 0.20058E+00 
c  r23          0.39975E-02      19   0.60920E-08   0.12694E-08 0.19987E+00 
c  epsilon      0.10969E+02      11   0.34454E-08   0.97406E-02 0.16380E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.84691E-02 0.43451E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6341         0.61363       0.0052562       0.0015073
v  Velocity[Y]            -0.57378         0.54439       0.0030807      0.00087335
v  Velocity[Z]              1.5652          5.4379          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4379          4.3406          4.3632
v  Pressure                -36.394          360.03          87.649          169.86
v  r11                   0.0010598        0.081908        0.013073        0.018285
v  r22                   0.0011119        0.082652        0.013353        0.018645
v  r33                   0.0016363         0.17429        0.027249        0.037205
v  r12                   -0.010651        0.013586     -0.00023379      -0.0003093
v  r13                    -0.04555        0.052815      9.3128e-05       0.0010138
v  r23                     -0.0467         0.05122      3.0398e-05      0.00057455
v  epsilon                0.068993           271.3          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9964e-05       0.0099177      0.00092484       0.0017426
v  CourantNb               0.44219             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2781         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781          0.7135         0.85283


 TIME FOR THE TIME STEP            10487:        0.80318E+02

===============================================================


 INSTANT    0.104880000E-01   TIME STEP NUMBER           10488
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.287642542E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.933740157E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282159301E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.332132977E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.969957037E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81162E-03   0.45187E-02 0.19902E+01 
c  Velocity[X]                                      0.13912E-03 
c  Velocity[Y]                                      0.12827E-03 
c  Velocity[Z]                                      0.42513E-02 
c  Pressure     0.36412E-04     132   0.92714E-02   0.25684E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.65128E-08   0.16178E-08 0.99454E-01 
c  r22          0.10852E-01      13   0.54248E-08   0.18249E-08 0.10154E+00 
c  r33          0.21859E-01      15   0.61885E-08   0.12445E-07 0.12742E+00 
c  r12          0.93858E-03      18   0.70805E-08   0.29665E-09 0.60430E+00 
c  r13          0.46674E-02      20   0.63027E-08   0.15111E-08 0.20056E+00 
c  r23          0.39975E-02      19   0.67407E-08   0.12602E-08 0.19830E+00 
c  epsilon      0.10969E+02      11   0.34060E-08   0.98253E-02 0.16413E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.84138E-02 0.43274E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63408          0.6136       0.0052563       0.0015073
v  Velocity[Y]             -0.5736         0.54418       0.0030807      0.00087332
v  Velocity[Z]              1.5652          5.4379          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4379          4.3406          4.3632
v  Pressure                -36.425          359.99          87.642          169.83
v  r11                   0.0010598        0.081903        0.013073        0.018285
v  r22                   0.0011119        0.082654        0.013353        0.018645
v  r33                   0.0016363         0.17427        0.027249        0.037205
v  r12                   -0.010651        0.013583     -0.00023379      -0.0003093
v  r13                   -0.045548        0.052815      9.3129e-05       0.0010138
v  r23                     -0.0467        0.051211      3.0399e-05      0.00057455
v  epsilon                0.068994          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9966e-05       0.0099177      0.00092484       0.0017426
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2781         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781          0.7135         0.85283


 TIME FOR THE TIME STEP            10488:        0.81033E+02

===============================================================


 INSTANT    0.104890000E-01   TIME STEP NUMBER           10489
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.771400008E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.370435612E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.961342913E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178440915E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.513319967E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81335E-03   0.44903E-02 0.19811E+01 
c  Velocity[X]                                      0.13779E-03 
c  Velocity[Y]                                      0.12803E-03 
c  Velocity[Z]                                      0.42245E-02 
c  Pressure     0.36010E-04     133   0.91645E-02   0.25400E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60041E-08   0.16632E-08 0.10051E+00 
c  r22          0.10852E-01      13   0.56880E-08   0.18010E-08 0.10102E+00 
c  r33          0.21859E-01      15   0.58758E-08   0.12599E-07 0.12798E+00 
c  r12          0.93858E-03      19   0.58276E-08   0.29814E-09 0.60226E+00 
c  r13          0.46674E-02      20   0.67356E-08   0.14925E-08 0.20005E+00 
c  r23          0.39975E-02      19   0.66217E-08   0.13050E-08 0.20177E+00 
c  epsilon      0.10969E+02      11   0.34645E-08   0.10267E-01 0.17241E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.84056E-02 0.43225E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63411         0.61367       0.0052563       0.0015073
v  Velocity[Y]             -0.5737         0.54424       0.0030808      0.00087334
v  Velocity[Z]              1.5652          5.4379          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4379          4.3406          4.3632
v  Pressure                -36.415          360.05          87.656          169.87
v  r11                   0.0010598        0.081902        0.013073        0.018285
v  r22                   0.0011119        0.082656        0.013353        0.018645
v  r33                   0.0016363         0.17428        0.027249        0.037205
v  r12                   -0.010658        0.013583     -0.00023379      -0.0003093
v  r13                   -0.045553        0.052815      9.3129e-05       0.0010138
v  r23                   -0.046701        0.051229        3.04e-05      0.00057455
v  epsilon                0.068995          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9968e-05       0.0099178      0.00092484       0.0017426
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2774         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8774          0.7135         0.85283


 TIME FOR THE TIME STEP            10489:        0.82274E+02

===============================================================


 INSTANT    0.104900000E-01   TIME STEP NUMBER           10490
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.525389938E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.163839463E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934909E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.268408535E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.616181113E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.875594114E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81222E-03   0.45454E-02 0.19976E+01 
c  Velocity[X]                                      0.13916E-03 
c  Velocity[Y]                                      0.12959E-03 
c  Velocity[Z]                                      0.42767E-02 
c  Pressure     0.36541E-04     133   0.92997E-02   0.25774E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56770E-08   0.16257E-08 0.99609E-01 
c  r22          0.10852E-01      13   0.56953E-08   0.17961E-08 0.10084E+00 
c  r33          0.21859E-01      15   0.56640E-08   0.12314E-07 0.12680E+00 
c  r12          0.93859E-03      19   0.62403E-08   0.29494E-09 0.59909E+00 
c  r13          0.46674E-02      20   0.60123E-08   0.14718E-08 0.19844E+00 
c  r23          0.39975E-02      19   0.68745E-08   0.12687E-08 0.19864E+00 
c  epsilon      0.10969E+02      11   0.33424E-08   0.97392E-02 0.16450E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.84492E-02 0.43368E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63422         0.61364       0.0052562       0.0015073
v  Velocity[Y]            -0.57361         0.54441       0.0030807       0.0008733
v  Velocity[Z]              1.5653          5.4379          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4379          4.3406          4.3632
v  Pressure                -36.416          360.01          87.664          169.85
v  r11                   0.0010598        0.081899        0.013073        0.018285
v  r22                   0.0011119        0.082658        0.013353        0.018645
v  r33                   0.0016363         0.17431        0.027249        0.037205
v  r12                    -0.01066        0.013592     -0.00023379      -0.0003093
v  r13                    -0.04555        0.052817      9.3131e-05       0.0010138
v  r23                   -0.046702        0.051219      3.0401e-05      0.00057455
v  epsilon                0.068996          271.27          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9972e-05       0.0099178      0.00092484       0.0017426
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2779         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8779          0.7135         0.85283


 TIME FOR THE TIME STEP            10490:        0.84202E+02

===============================================================


 INSTANT    0.104910000E-01   TIME STEP NUMBER           10491
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.322948247E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.152504418E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.710300908E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.174557402E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107793616E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81301E-03   0.45392E-02 0.19948E+01 
c  Velocity[X]                                      0.13886E-03 
c  Velocity[Y]                                      0.12899E-03 
c  Velocity[Z]                                      0.42714E-02 
c  Pressure     0.36226E-04     132   0.92186E-02   0.25552E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55584E-08   0.16067E-08 0.99207E-01 
c  r22          0.10852E-01      13   0.53481E-08   0.17908E-08 0.10065E+00 
c  r33          0.21859E-01      15   0.58688E-08   0.12179E-07 0.12594E+00 
c  r12          0.93859E-03      19   0.55465E-08   0.29322E-09 0.60052E+00 
c  r13          0.46675E-02      20   0.57574E-08   0.14741E-08 0.19853E+00 
c  r23          0.39975E-02      19   0.73327E-08   0.12582E-08 0.19803E+00 
c  epsilon      0.10969E+02      11   0.33568E-08   0.94966E-02 0.16122E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.84547E-02 0.43412E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63418         0.61361       0.0052562       0.0015073
v  Velocity[Y]            -0.57364         0.54406       0.0030807       0.0008733
v  Velocity[Z]              1.5652          5.4379          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4379          4.3406          4.3632
v  Pressure                -36.346          360.07          87.691          169.89
v  r11                   0.0010598        0.081897        0.013073        0.018285
v  r22                   0.0011119        0.082658        0.013353        0.018645
v  r33                   0.0016363         0.17434        0.027249        0.037205
v  r12                   -0.010658        0.013592     -0.00023379      -0.0003093
v  r13                    -0.04555         0.05281      9.3131e-05       0.0010138
v  r23                   -0.046702        0.051209      3.0402e-05      0.00057456
v  epsilon                0.068998          271.28          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9973e-05       0.0099178      0.00092484       0.0017426
v  CourantNb               0.44219             0.6         0.59908         0.59839
v  FourierNb             0.0017845           5.278         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.878          0.7135         0.85283


 TIME FOR THE TIME STEP            10491:        0.11763E+03

===============================================================


 INSTANT    0.104920000E-01   TIME STEP NUMBER           10492
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107888047E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.134995731E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.104338698E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.356074019E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.738570348E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81300E-03   0.45128E-02 0.19892E+01 
c  Velocity[X]                                      0.13810E-03 
c  Velocity[Y]                                      0.12838E-03 
c  Velocity[Z]                                      0.42463E-02 
c  Pressure     0.36566E-04     132   0.93094E-02   0.25793E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55174E-08   0.16423E-08 0.99806E-01 
c  r22          0.10852E-01      13   0.54930E-08   0.18309E-08 0.10154E+00 
c  r33          0.21859E-01      15   0.54295E-08   0.12619E-07 0.12766E+00 
c  r12          0.93859E-03      19   0.55325E-08   0.29959E-09 0.60539E+00 
c  r13          0.46675E-02      19   0.69796E-08   0.15049E-08 0.20089E+00 
c  r23          0.39975E-02      19   0.72534E-08   0.12856E-08 0.19965E+00 
c  epsilon      0.10969E+02      11   0.34830E-08   0.99583E-02 0.16574E+00 
c  TempC        0.25716E+06      16   0.15179E-04   0.83137E-02 0.43006E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63415         0.61367       0.0052562       0.0015072
v  Velocity[Y]            -0.57366         0.54404       0.0030807       0.0008733
v  Velocity[Z]              1.5651          5.4379          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4379          4.3406          4.3632
v  Pressure                -36.432          360.06          87.676          169.88
v  r11                   0.0010599        0.081887        0.013073        0.018285
v  r22                   0.0011119        0.082657        0.013353        0.018645
v  r33                   0.0016363         0.17433        0.027249        0.037205
v  r12                   -0.010661        0.013587     -0.00023379      -0.0003093
v  r13                   -0.045552        0.052807      9.3131e-05       0.0010138
v  r23                   -0.046703        0.051229      3.0403e-05      0.00057456
v  epsilon                0.068999          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.997e-05       0.0099179      0.00092485       0.0017426
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2783         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8783         0.71351         0.85284


 TIME FOR THE TIME STEP            10492:        0.12361E+03

===============================================================


 INSTANT    0.104930000E-01   TIME STEP NUMBER           10493
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158307800E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.234207207E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.777814935E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.530199284E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.151531639E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81176E-03   0.45221E-02 0.19909E+01 
c  Velocity[X]                                      0.13726E-03 
c  Velocity[Y]                                      0.12822E-03 
c  Velocity[Z]                                      0.42566E-02 
c  Pressure     0.36256E-04     133   0.92284E-02   0.25574E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53914E-08   0.16806E-08 0.10047E+00 
c  r22          0.10852E-01      13   0.53762E-08   0.18561E-08 0.10251E+00 
c  r33          0.21859E-01      15   0.54540E-08   0.12926E-07 0.12924E+00 
c  r12          0.93859E-03      18   0.72018E-08   0.31774E-09 0.61848E+00 
c  r13          0.46675E-02      19   0.64747E-08   0.15239E-08 0.20205E+00 
c  r23          0.39975E-02      20   0.56063E-08   0.13443E-08 0.20401E+00 
c  epsilon      0.10969E+02      11   0.36173E-08   0.10051E-01 0.16671E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.83770E-02 0.43199E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6341         0.61365       0.0052563       0.0015073
v  Velocity[Y]            -0.57363         0.54418       0.0030807      0.00087328
v  Velocity[Z]              1.5652          5.4379          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4379          4.3406          4.3632
v  Pressure                -36.387          360.09          87.677           169.9
v  r11                   0.0010599         0.08189        0.013073        0.018285
v  r22                   0.0011119         0.08265        0.013353        0.018645
v  r33                   0.0016363         0.17429        0.027249        0.037205
v  r12                   -0.010663        0.013594      -0.0002338      -0.0003093
v  r13                   -0.045551        0.052807      9.3131e-05       0.0010138
v  r23                   -0.046703        0.051214      3.0403e-05      0.00057456
v  epsilon                   0.069          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9969e-05       0.0099178      0.00092485       0.0017426
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2782         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8782          0.7135         0.85283


 TIME FOR THE TIME STEP            10493:        0.11710E+03

===============================================================


 INSTANT    0.104940000E-01   TIME STEP NUMBER           10494
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.357256312E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.496616983E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.176449652E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182618674E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.795760611E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81210E-03   0.45298E-02 0.19934E+01 
c  Velocity[X]                                      0.13922E-03 
c  Velocity[Y]                                      0.12880E-03 
c  Velocity[Z]                                      0.42618E-02 
c  Pressure     0.36285E-04     133   0.92353E-02   0.25594E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50196E-08   0.16392E-08 0.99883E-01 
c  r22          0.10852E-01      13   0.51487E-08   0.18314E-08 0.10174E+00 
c  r33          0.21859E-01      15   0.54233E-08   0.12506E-07 0.12764E+00 
c  r12          0.93859E-03      18   0.67087E-08   0.30096E-09 0.60657E+00 
c  r13          0.46675E-02      19   0.71048E-08   0.15002E-08 0.20010E+00 
c  r23          0.39975E-02      19   0.68356E-08   0.12771E-08 0.19918E+00 
c  epsilon      0.10969E+02      11   0.34088E-08   0.95542E-02 0.16307E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.84718E-02 0.43429E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161985


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63409         0.61361       0.0052562       0.0015073
v  Velocity[Y]            -0.57361         0.54433       0.0030807      0.00087329
v  Velocity[Z]              1.5652          5.4379          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4379          4.3406          4.3632
v  Pressure                -36.439          360.06          87.685          169.89
v  r11                   0.0010599        0.081884        0.013073        0.018285
v  r22                    0.001112         0.08265        0.013353        0.018645
v  r33                   0.0016364         0.17431        0.027249        0.037205
v  r12                   -0.010657        0.013592      -0.0002338      -0.0003093
v  r13                   -0.045549        0.052809      9.3132e-05       0.0010138
v  r23                   -0.046703        0.051205      3.0403e-05      0.00057456
v  epsilon                0.069001          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9966e-05       0.0099179      0.00092485       0.0017426
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2791         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8791         0.71351         0.85284


 TIME FOR THE TIME STEP            10494:        0.29297E+03

===============================================================


 INSTANT    0.104950000E-01   TIME STEP NUMBER           10495
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.354058785E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.277831751E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136799330E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.438268320E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.293513056E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81227E-03   0.45115E-02 0.19880E+01 
c  Velocity[X]                                      0.13855E-03 
c  Velocity[Y]                                      0.12791E-03 
c  Velocity[Z]                                      0.42450E-02 
c  Pressure     0.35891E-04     132   0.91314E-02   0.25316E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52030E-08   0.16504E-08 0.99781E-01 
c  r22          0.10852E-01      13   0.49616E-08   0.17948E-08 0.10071E+00 
c  r33          0.21859E-01      15   0.64153E-08   0.12522E-07 0.12732E+00 
c  r12          0.93859E-03      18   0.61855E-08   0.29732E-09 0.60209E+00 
c  r13          0.46675E-02      19   0.73104E-08   0.14755E-08 0.19837E+00 
c  r23          0.39975E-02      19   0.62744E-08   0.12947E-08 0.20040E+00 
c  epsilon      0.10969E+02      11   0.32622E-08   0.10149E-01 0.17029E+00 
c  TempC        0.25716E+06      16   0.15101E-04   0.84215E-02 0.43281E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63411         0.61367       0.0052562       0.0015073
v  Velocity[Y]            -0.57373         0.54416       0.0030808      0.00087334
v  Velocity[Z]              1.5651          5.4379          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4379          4.3406          4.3632
v  Pressure                -36.426          359.99          87.627          169.83
v  r11                   0.0010599        0.081882        0.013073        0.018285
v  r22                    0.001112         0.08265        0.013353        0.018645
v  r33                   0.0016364         0.17434        0.027249        0.037205
v  r12                   -0.010652        0.013589      -0.0002338      -0.0003093
v  r13                   -0.045552        0.052807      9.3133e-05       0.0010138
v  r23                   -0.046703        0.051203      3.0404e-05      0.00057456
v  epsilon                0.069002          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9962e-05       0.0099179      0.00092485       0.0017426
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2793         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8793          0.7135         0.85283


 TIME FOR THE TIME STEP            10495:        0.29698E+03

===============================================================


 INSTANT    0.104960000E-01   TIME STEP NUMBER           10496
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.222666706E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.292677104E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178800264E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.888087571E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.728615747E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81319E-03   0.45182E-02 0.19924E+01 
c  Velocity[X]                                      0.13842E-03 
c  Velocity[Y]                                      0.12894E-03 
c  Velocity[Z]                                      0.42508E-02 
c  Pressure     0.36751E-04     133   0.93592E-02   0.25923E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56202E-08   0.16366E-08 0.99301E-01 
c  r22          0.10852E-01      13   0.49910E-08   0.18293E-08 0.10145E+00 
c  r33          0.21859E-01      15   0.60979E-08   0.12652E-07 0.12778E+00 
c  r12          0.93859E-03      18   0.56193E-08   0.29708E-09 0.60358E+00 
c  r13          0.46675E-02      19   0.67111E-08   0.14979E-08 0.19995E+00 
c  r23          0.39975E-02      19   0.56025E-08   0.13087E-08 0.20040E+00 
c  epsilon      0.10969E+02      11   0.34120E-08   0.10061E-01 0.16632E+00 
c  TempC        0.25716E+06      16   0.15181E-04   0.84007E-02 0.43266E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63413         0.61362       0.0052563       0.0015073
v  Velocity[Y]            -0.57363         0.54424       0.0030807       0.0008733
v  Velocity[Z]              1.5654          5.4379          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4379          4.3406          4.3632
v  Pressure                -36.427          360.02          87.662          169.86
v  r11                   0.0010599        0.081879        0.013073        0.018285
v  r22                    0.001112        0.082649        0.013353        0.018645
v  r33                   0.0016364         0.17431        0.027249        0.037205
v  r12                    -0.01065        0.013596      -0.0002338      -0.0003093
v  r13                   -0.045549        0.052808      9.3134e-05       0.0010138
v  r23                   -0.046703        0.051224      3.0405e-05      0.00057456
v  epsilon                0.069003          271.26          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9956e-05       0.0099179      0.00092485       0.0017426
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2788         0.11442         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8788         0.71351         0.85284


 TIME FOR THE TIME STEP            10496:        0.24137E+03

===============================================================


 INSTANT    0.104970000E-01   TIME STEP NUMBER           10497
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.656056791E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.687571224E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226511145E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.973302801E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.449112142E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81202E-03   0.45386E-02 0.19933E+01 
c  Velocity[X]                                      0.13890E-03 
c  Velocity[Y]                                      0.12864E-03 
c  Velocity[Z]                                      0.42711E-02 
c  Pressure     0.36388E-04     133   0.92602E-02   0.25667E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61048E-08   0.16170E-08 0.99097E-01 
c  r22          0.10852E-01      13   0.48226E-08   0.18247E-08 0.10127E+00 
c  r33          0.21859E-01      15   0.52416E-08   0.12386E-07 0.12666E+00 
c  r12          0.93859E-03      18   0.52714E-08   0.29804E-09 0.60321E+00 
c  r13          0.46675E-02      20   0.57961E-08   0.14932E-08 0.19920E+00 
c  r23          0.39975E-02      18   0.69780E-08   0.12649E-08 0.19821E+00 
c  epsilon      0.10969E+02      11   0.33761E-08   0.97330E-02 0.16383E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84757E-02 0.43467E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63414         0.61362       0.0052564       0.0015073
v  Velocity[Y]            -0.57372         0.54437       0.0030808      0.00087333
v  Velocity[Z]              1.5654          5.4379          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4379          4.3406          4.3632
v  Pressure                -36.394          360.07          87.667          169.89
v  r11                   0.0010599         0.08189        0.013073        0.018285
v  r22                    0.001112        0.082651        0.013353        0.018645
v  r33                   0.0016364         0.17429        0.027249        0.037205
v  r12                   -0.010648        0.013599      -0.0002338      -0.0003093
v  r13                    -0.04555         0.05281      9.3135e-05       0.0010138
v  r23                   -0.046703        0.051209      3.0406e-05      0.00057456
v  epsilon                0.069005          271.19          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9953e-05       0.0099179      0.00092485       0.0017426
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2794         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8794          0.7135         0.85284


 TIME FOR THE TIME STEP            10497:        0.20111E+03

===============================================================


 INSTANT    0.104980000E-01   TIME STEP NUMBER           10498
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.379278480E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.456406507E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.258311668E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.206739012E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107439115E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81287E-03   0.45120E-02 0.19906E+01 
c  Velocity[X]                                      0.13930E-03 
c  Velocity[Y]                                      0.12879E-03 
c  Velocity[Z]                                      0.42439E-02 
c  Pressure     0.36488E-04     133   0.92884E-02   0.25737E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.62681E-08   0.16474E-08 0.10012E+00 
c  r22          0.10852E-01      13   0.45709E-08   0.18314E-08 0.10179E+00 
c  r33          0.21859E-01      15   0.57283E-08   0.12525E-07 0.12756E+00 
c  r12          0.93859E-03      18   0.53573E-08   0.30269E-09 0.60827E+00 
c  r13          0.46675E-02      19   0.70435E-08   0.15011E-08 0.20023E+00 
c  r23          0.39975E-02      19   0.51679E-08   0.12764E-08 0.19903E+00 
c  epsilon      0.10969E+02      11   0.34247E-08   0.97654E-02 0.16485E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83874E-02 0.43190E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63422         0.61365       0.0052563       0.0015073
v  Velocity[Y]            -0.57374         0.54421       0.0030807       0.0008733
v  Velocity[Z]               1.565           5.438          4.3388          4.3625
v  ǁVelocityǁ               1.5788           5.438          4.3406          4.3632
v  Pressure                -36.451             360          87.634          169.83
v  r11                   0.0010599        0.081893        0.013073        0.018285
v  r22                    0.001112        0.082652        0.013353        0.018645
v  r33                   0.0016364          0.1743        0.027249        0.037205
v  r12                   -0.010649        0.013599      -0.0002338      -0.0003093
v  r13                   -0.045552        0.052809      9.3136e-05       0.0010138
v  r23                   -0.046704        0.051194      3.0407e-05      0.00057456
v  epsilon                0.069006          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9949e-05       0.0099178      0.00092485       0.0017426
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017845          5.2797         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8797         0.71351         0.85284


 TIME FOR THE TIME STEP            10498:        0.80869E+02

===============================================================


 INSTANT    0.104990000E-01   TIME STEP NUMBER           10499
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.447623525E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.156611961E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.517239722E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319364842E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.212910093E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81198E-03   0.45350E-02 0.19964E+01 
c  Velocity[X]                                      0.13800E-03 
c  Velocity[Y]                                      0.12836E-03 
c  Velocity[Z]                                      0.42687E-02 
c  Pressure     0.36279E-04     131   0.92275E-02   0.25590E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.66883E-08   0.16549E-08 0.10031E+00 
c  r22          0.10852E-01      12   0.65943E-08   0.18167E-08 0.10129E+00 
c  r33          0.21859E-01      14   0.70059E-08   0.12535E-07 0.12741E+00 
c  r12          0.93859E-03      18   0.54862E-08   0.29717E-09 0.60300E+00 
c  r13          0.46675E-02      19   0.56548E-08   0.14834E-08 0.19926E+00 
c  r23          0.39975E-02      18   0.66121E-08   0.12938E-08 0.19941E+00 
c  epsilon      0.10969E+02      11   0.32882E-08   0.97702E-02 0.16481E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84575E-02 0.43346E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63412         0.61364       0.0052563       0.0015073
v  Velocity[Y]            -0.57373         0.54419       0.0030807      0.00087332
v  Velocity[Z]              1.5651           5.438          4.3388          4.3625
v  ǁVelocityǁ               1.5788           5.438          4.3406          4.3632
v  Pressure                -36.387          360.02          87.653          169.85
v  r11                   0.0010599        0.081889        0.013073        0.018285
v  r22                    0.001112        0.082651        0.013353        0.018645
v  r33                   0.0016364         0.17432        0.027249        0.037205
v  r12                   -0.010648          0.0136      -0.0002338      -0.0003093
v  r13                   -0.045549        0.052808      9.3138e-05       0.0010138
v  r23                   -0.046704        0.051183      3.0407e-05      0.00057456
v  epsilon                0.069007          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099177      0.00092485       0.0017426
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2794         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8794          0.7135         0.85283


 TIME FOR THE TIME STEP            10499:        0.79140E+02

===============================================================


 INSTANT    0.105000000E-01   TIME STEP NUMBER           10500
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.337210083E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.176605773E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208848404E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.560579495E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.241407530E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81257E-03   0.44950E-02 0.19851E+01 
c  Velocity[X]                                      0.13877E-03 
c  Velocity[Y]                                      0.12932E-03 
c  Velocity[Z]                                      0.42269E-02 
c  Pressure     0.36135E-04     131   0.91944E-02   0.25488E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59258E-08   0.16422E-08 0.10016E+00 
c  r22          0.10852E-01      13   0.45576E-08   0.18078E-08 0.10107E+00 
c  r33          0.21859E-01      15   0.52825E-08   0.12448E-07 0.12715E+00 
c  r12          0.93859E-03      18   0.54960E-08   0.29880E-09 0.60577E+00 
c  r13          0.46675E-02      19   0.54560E-08   0.14903E-08 0.19926E+00 
c  r23          0.39975E-02      19   0.51796E-08   0.12797E-08 0.19960E+00 
c  epsilon      0.10969E+02      11   0.31547E-08   0.99370E-02 0.16887E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84091E-02 0.43297E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6341         0.61359       0.0052564       0.0015073
v  Velocity[Y]             -0.5736         0.54428       0.0030807      0.00087333
v  Velocity[Z]              1.5652           5.438          4.3388          4.3625
v  ǁVelocityǁ                1.579           5.438          4.3406          4.3632
v  Pressure                -36.444          360.01           87.64          169.84
v  r11                   0.0010599        0.081886        0.013073        0.018285
v  r22                    0.001112        0.082651        0.013353        0.018645
v  r33                   0.0016364         0.17435        0.027249        0.037205
v  r12                   -0.010649        0.013599      -0.0002338      -0.0003093
v  r13                   -0.045548         0.05281      9.3139e-05       0.0010138
v  r23                   -0.046703        0.051214      3.0408e-05      0.00057456
v  epsilon                0.069008          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099178      0.00092485       0.0017426
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2794         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8794         0.71351         0.85284


 TIME FOR THE TIME STEP            10500:        0.83393E+02

===============================================================


 INSTANT    0.105010000E-01   TIME STEP NUMBER           10501
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172642784E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.328953047E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.235299137E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.238437109E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.934946754E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81336E-03   0.45117E-02 0.19887E+01 
c  Velocity[X]                                      0.13778E-03 
c  Velocity[Y]                                      0.12833E-03 
c  Velocity[Z]                                      0.42456E-02 
c  Pressure     0.36436E-04     131   0.92689E-02   0.25700E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55807E-08   0.16548E-08 0.10008E+00 
c  r22          0.10852E-01      13   0.48441E-08   0.17955E-08 0.10114E+00 
c  r33          0.21859E-01      14   0.69495E-08   0.12372E-07 0.12711E+00 
c  r12          0.93859E-03      18   0.58775E-08   0.29736E-09 0.60341E+00 
c  r13          0.46675E-02      19   0.60975E-08   0.14625E-08 0.19841E+00 
c  r23          0.39975E-02      19   0.54379E-08   0.12775E-08 0.19916E+00 
c  epsilon      0.10969E+02      11   0.31742E-08   0.96178E-02 0.16289E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.83571E-02 0.43140E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161982


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63413         0.61362       0.0052563       0.0015073
v  Velocity[Y]            -0.57365         0.54437       0.0030806      0.00087328
v  Velocity[Z]              1.5656           5.438          4.3388          4.3625
v  ǁVelocityǁ               1.5794           5.438          4.3406          4.3632
v  Pressure                -36.424          360.07          87.674          169.89
v  r11                   0.0010599        0.081876        0.013073        0.018285
v  r22                    0.001112        0.082646        0.013353        0.018645
v  r33                   0.0016365         0.17432        0.027249        0.037205
v  r12                   -0.010648        0.013603      -0.0002338      -0.0003093
v  r13                   -0.045552        0.052812       9.314e-05       0.0010138
v  r23                   -0.046703        0.051209      3.0409e-05      0.00057456
v  epsilon                0.069009          271.25          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.994e-05       0.0099178      0.00092486       0.0017426
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2798         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8798          0.7135         0.85283


 TIME FOR THE TIME STEP            10501:        0.79682E+02

===============================================================


 INSTANT    0.105020000E-01   TIME STEP NUMBER           10502
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157931199E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.717868183E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.170043838E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.617112063E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.128106911E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81153E-03   0.45239E-02 0.19940E+01 
c  Velocity[X]                                      0.13800E-03 
c  Velocity[Y]                                      0.12893E-03 
c  Velocity[Z]                                      0.42569E-02 
c  Pressure     0.36360E-04     133   0.92577E-02   0.25648E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54485E-08   0.16422E-08 0.99584E-01 
c  r22          0.10852E-01      13   0.49441E-08   0.18179E-08 0.10113E+00 
c  r33          0.21859E-01      15   0.64794E-08   0.12459E-07 0.12676E+00 
c  r12          0.93859E-03      18   0.56569E-08   0.29303E-09 0.59952E+00 
c  r13          0.46675E-02      19   0.64624E-08   0.14722E-08 0.19847E+00 
c  r23          0.39975E-02      19   0.56830E-08   0.12826E-08 0.19908E+00 
c  epsilon      0.10969E+02      11   0.34043E-08   0.98147E-02 0.16383E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.83955E-02 0.43209E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63418         0.61361       0.0052563       0.0015073
v  Velocity[Y]            -0.57349         0.54422       0.0030806      0.00087328
v  Velocity[Z]              1.5655           5.438          4.3388          4.3625
v  ǁVelocityǁ               1.5793           5.438          4.3406          4.3632
v  Pressure                 -36.43          360.01          87.662          169.85
v  r11                   0.0010599        0.081872        0.013073        0.018285
v  r22                    0.001112        0.082648        0.013353        0.018645
v  r33                   0.0016365         0.17429        0.027249        0.037205
v  r12                   -0.010647        0.013598      -0.0002338      -0.0003093
v  r13                   -0.045548        0.052814       9.314e-05       0.0010138
v  r23                   -0.046703          0.0512      3.0409e-05      0.00057456
v  epsilon                 0.06901           271.2          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099176      0.00092486       0.0017426
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2799         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8799          0.7135         0.85283


 TIME FOR THE TIME STEP            10502:        0.82970E+02

===============================================================


 INSTANT    0.105030000E-01   TIME STEP NUMBER           10503
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.282856474E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.560929708E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.425502758E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319232493E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151031949E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81254E-03   0.45035E-02 0.19882E+01 
c  Velocity[X]                                      0.13884E-03 
c  Velocity[Y]                                      0.12891E-03 
c  Velocity[Z]                                      0.42357E-02 
c  Pressure     0.36036E-04     132   0.91819E-02   0.25419E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55848E-08   0.16165E-08 0.98928E-01 
c  r22          0.10852E-01      13   0.51223E-08   0.17783E-08 0.10013E+00 
c  r33          0.21859E-01      15   0.60195E-08   0.12276E-07 0.12606E+00 
c  r12          0.93859E-03      18   0.53376E-08   0.30082E-09 0.60638E+00 
c  r13          0.46675E-02      19   0.61957E-08   0.14802E-08 0.19825E+00 
c  r23          0.39975E-02      19   0.52838E-08   0.12698E-08 0.19777E+00 
c  epsilon      0.10969E+02      11   0.34603E-08   0.93841E-02 0.16008E+00 
c  TempC        0.25716E+06      16   0.15106E-04   0.84989E-02 0.43504E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63415         0.61358       0.0052563       0.0015073
v  Velocity[Y]            -0.57347          0.5442       0.0030807      0.00087331
v  Velocity[Z]              1.5653           5.438          4.3388          4.3625
v  ǁVelocityǁ               1.5792           5.438          4.3406          4.3632
v  Pressure                -36.401          360.01          87.632          169.84
v  r11                   0.0010599        0.081868        0.013073        0.018285
v  r22                   0.0011121        0.082649        0.013353        0.018645
v  r33                   0.0016365          0.1743        0.027249        0.037205
v  r12                   -0.010649          0.0136      -0.0002338      -0.0003093
v  r13                   -0.045547        0.052811      9.3141e-05       0.0010138
v  r23                   -0.046703        0.051226       3.041e-05      0.00057456
v  epsilon                0.069011          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05       0.0099176      0.00092486       0.0017426
v  CourantNb               0.44258             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2794         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8794          0.7135         0.85283


 TIME FOR THE TIME STEP            10503:        0.79495E+02

===============================================================


 INSTANT    0.105040000E-01   TIME STEP NUMBER           10504
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162501101E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.932564076E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160352789E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.998765415E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.247726108E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81290E-03   0.45058E-02 0.19862E+01 
c  Velocity[X]                                      0.13771E-03 
c  Velocity[Y]                                      0.12842E-03 
c  Velocity[Z]                                      0.42396E-02 
c  Pressure     0.36514E-04     133   0.93039E-02   0.25756E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55268E-08   0.16503E-08 0.99374E-01 
c  r22          0.10852E-01      13   0.53816E-08   0.18154E-08 0.10055E+00 
c  r33          0.21859E-01      14   0.65443E-08   0.12524E-07 0.12690E+00 
c  r12          0.93859E-03      18   0.63196E-08   0.29417E-09 0.60047E+00 
c  r13          0.46675E-02      19   0.57964E-08   0.14824E-08 0.19882E+00 
c  r23          0.39975E-02      19   0.58233E-08   0.12826E-08 0.19868E+00 
c  epsilon      0.10969E+02      11   0.32973E-08   0.10076E-01 0.16709E+00 
c  TempC        0.25716E+06      16   0.15166E-04   0.84323E-02 0.43321E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63417         0.61363       0.0052563       0.0015073
v  Velocity[Y]            -0.57351         0.54429       0.0030806      0.00087328
v  Velocity[Z]              1.5651           5.438          4.3388          4.3625
v  ǁVelocityǁ                1.579           5.438          4.3406          4.3632
v  Pressure                -36.444          360.05          87.658          169.87
v  r11                   0.0010599        0.081866        0.013073        0.018285
v  r22                   0.0011121         0.08265        0.013353        0.018645
v  r33                   0.0016365         0.17432        0.027249        0.037205
v  r12                   -0.010651        0.013601      -0.0002338      -0.0003093
v  r13                    -0.04555         0.05281      9.3142e-05       0.0010138
v  r23                   -0.046703         0.05121      3.0411e-05      0.00057456
v  epsilon                0.069013          271.24          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9929e-05       0.0099175      0.00092486       0.0017426
v  CourantNb               0.44258             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2787         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8787          0.7135         0.85284


 TIME FOR THE TIME STEP            10504:        0.82183E+02

===============================================================


 INSTANT    0.105050000E-01   TIME STEP NUMBER           10505
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.145337933E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.336464195E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249157840E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.360642527E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172617250E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81160E-03   0.45163E-02 0.19912E+01 
c  Velocity[X]                                      0.13819E-03 
c  Velocity[Y]                                      0.12830E-03 
c  Velocity[Z]                                      0.42498E-02 
c  Pressure     0.36256E-04     131   0.92259E-02   0.25574E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52936E-08   0.16669E-08 0.10017E+00 
c  r22          0.10852E-01      13   0.51809E-08   0.18581E-08 0.10181E+00 
c  r33          0.21859E-01      14   0.65304E-08   0.12852E-07 0.12841E+00 
c  r12          0.93859E-03      18   0.52792E-08   0.30476E-09 0.60981E+00 
c  r13          0.46675E-02      18   0.69438E-08   0.15107E-08 0.20035E+00 
c  r23          0.39975E-02      19   0.59363E-08   0.13081E-08 0.20129E+00 
c  epsilon      0.10969E+02      11   0.33363E-08   0.10116E-01 0.16642E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.84233E-02 0.43268E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -0.634          0.6136       0.0052564       0.0015073
v  Velocity[Y]            -0.57344         0.54438       0.0030806      0.00087329
v  Velocity[Z]              1.5651           5.438          4.3388          4.3625
v  ǁVelocityǁ                1.579           5.438          4.3406          4.3632
v  Pressure                  -36.4          360.01          87.633          169.84
v  r11                   0.0010599        0.081858        0.013073        0.018285
v  r22                   0.0011121         0.08265        0.013353        0.018645
v  r33                   0.0016365          0.1743        0.027249        0.037205
v  r12                   -0.010652        0.013601      -0.0002338      -0.0003093
v  r13                   -0.045549         0.05281      9.3144e-05       0.0010138
v  r23                   -0.046703        0.051196      3.0412e-05      0.00057457
v  epsilon                0.069014          271.23          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099175      0.00092486       0.0017426
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2787         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8787          0.7135         0.85284


 TIME FOR THE TIME STEP            10505:        0.82325E+02

===============================================================


 INSTANT    0.105060000E-01   TIME STEP NUMBER           10506
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.627801838E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.638536403E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.299052183E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.499501416E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.818832347E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81324E-03   0.45354E-02 0.19943E+01 
c  Velocity[X]                                      0.13877E-03 
c  Velocity[Y]                                      0.12815E-03 
c  Velocity[Z]                                      0.42685E-02 
c  Pressure     0.36588E-04     133   0.93111E-02   0.25808E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54224E-08   0.16940E-08 0.10156E+00 
c  r22          0.10852E-01      13   0.53284E-08   0.18466E-08 0.10229E+00 
c  r33          0.21859E-01      14   0.69680E-08   0.12759E-07 0.12940E+00 
c  r12          0.93859E-03      18   0.56914E-08   0.32158E-09 0.62046E+00 
c  r13          0.46675E-02      18   0.71099E-08   0.14933E-08 0.20020E+00 
c  r23          0.39975E-02      19   0.56862E-08   0.13326E-08 0.20438E+00 
c  epsilon      0.10969E+02      11   0.32563E-08   0.98292E-02 0.16939E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.84593E-02 0.43392E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -0.634         0.61358       0.0052564       0.0015073
v  Velocity[Y]            -0.57334         0.54445       0.0030807      0.00087334
v  Velocity[Z]              1.5651           5.438          4.3388          4.3625
v  ǁVelocityǁ               1.5789           5.438          4.3406          4.3632
v  Pressure                -36.423          359.98          87.622          169.81
v  r11                   0.0010599        0.081858        0.013073        0.018285
v  r22                   0.0011121        0.082652        0.013353        0.018645
v  r33                   0.0016365         0.17428        0.027249        0.037205
v  r12                   -0.010654          0.0136      -0.0002338      -0.0003093
v  r13                   -0.045548        0.052811      9.3145e-05       0.0010138
v  r23                   -0.046703        0.051218      3.0412e-05      0.00057457
v  epsilon                0.069015          271.19          7.2635          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099175      0.00092486       0.0017426
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017846           5.279         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.879          0.7135         0.85283


 TIME FOR THE TIME STEP            10506:        0.83434E+02

===============================================================


 INSTANT    0.105070000E-01   TIME STEP NUMBER           10507
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.750315816E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.215404982E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.513374306E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.144114506E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.144021970E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81217E-03   0.45346E-02 0.19936E+01 
c  Velocity[X]                                      0.13769E-03 
c  Velocity[Y]                                      0.12814E-03 
c  Velocity[Z]                                      0.42688E-02 
c  Pressure     0.36196E-04     133   0.92187E-02   0.25531E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53643E-08   0.16780E-08 0.10048E+00 
c  r22          0.10852E-01      13   0.53037E-08   0.18354E-08 0.10221E+00 
c  r33          0.21859E-01      15   0.57492E-08   0.12704E-07 0.12853E+00 
c  r12          0.93859E-03      18   0.57229E-08   0.30281E-09 0.60772E+00 
c  r13          0.46675E-02      19   0.54987E-08   0.14968E-08 0.20074E+00 
c  r23          0.39975E-02      19   0.66516E-08   0.13150E-08 0.20061E+00 
c  epsilon      0.10969E+02      11   0.32240E-08   0.99492E-02 0.16688E+00 
c  TempC        0.25716E+06      16   0.15096E-04   0.83562E-02 0.43112E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63401         0.61363       0.0052565       0.0015074
v  Velocity[Y]             -0.5735         0.54423       0.0030808       0.0008734
v  Velocity[Z]              1.5652           5.438          4.3388          4.3625
v  ǁVelocityǁ                1.579           5.438          4.3406          4.3632
v  Pressure                -36.441          360.02          87.633          169.84
v  r11                   0.0010599         0.08185        0.013073        0.018285
v  r22                   0.0011121        0.082652        0.013353        0.018645
v  r33                   0.0016366         0.17429        0.027249        0.037205
v  r12                   -0.010655        0.013597      -0.0002338      -0.0003093
v  r13                    -0.04555        0.052808      9.3145e-05       0.0010138
v  r23                   -0.046703        0.051211      3.0411e-05      0.00057456
v  epsilon                0.069016          271.22          7.2635          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099175      0.00092486       0.0017426
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2792         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8792          0.7135         0.85284


 TIME FOR THE TIME STEP            10507:        0.79063E+02

===============================================================


 INSTANT    0.105080000E-01   TIME STEP NUMBER           10508
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.166294031E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.240920916E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.128154360E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.865154582E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.474615587E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81208E-03   0.45499E-02 0.19958E+01 
c  Velocity[X]                                      0.13873E-03 
c  Velocity[Y]                                      0.12902E-03 
c  Velocity[Z]                                      0.42822E-02 
c  Pressure     0.36658E-04     132   0.93377E-02   0.25858E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52784E-08   0.16632E-08 0.10084E+00 
c  r22          0.10852E-01      13   0.54602E-08   0.18708E-08 0.10294E+00 
c  r33          0.21859E-01      14   0.65747E-08   0.12761E-07 0.12912E+00 
c  r12          0.93859E-03      18   0.49585E-08   0.30602E-09 0.61213E+00 
c  r13          0.46675E-02      18   0.63399E-08   0.15006E-08 0.20097E+00 
c  r23          0.39975E-02      19   0.59219E-08   0.12948E-08 0.20100E+00 
c  epsilon      0.10969E+02      11   0.32006E-08   0.98506E-02 0.16532E+00 
c  TempC        0.25716E+06      16   0.15165E-04   0.84133E-02 0.43262E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63408          0.6136       0.0052564       0.0015074
v  Velocity[Y]            -0.57337         0.54434       0.0030807      0.00087335
v  Velocity[Z]              1.5652           5.438          4.3388          4.3625
v  ǁVelocityǁ                1.579           5.438          4.3406          4.3632
v  Pressure                -36.446          359.99          87.626          169.82
v  r11                   0.0010599        0.081847        0.013073        0.018285
v  r22                   0.0011121        0.082651        0.013353        0.018645
v  r33                   0.0016366         0.17431        0.027249        0.037205
v  r12                   -0.010656        0.013595      -0.0002338      -0.0003093
v  r13                   -0.045548         0.05281      9.3145e-05       0.0010138
v  r23                   -0.046703        0.051197      3.0411e-05      0.00057456
v  epsilon                0.069017          271.22          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099174      0.00092486       0.0017426
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2797         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8797         0.71351         0.85284


 TIME FOR THE TIME STEP            10508:        0.80088E+02

===============================================================


 INSTANT    0.105090000E-01   TIME STEP NUMBER           10509
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.242327640E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.193646794E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.238657304E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.194101241E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.134311911E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81220E-03   0.45272E-02 0.19930E+01 
c  Velocity[X]                                      0.13906E-03 
c  Velocity[Y]                                      0.12907E-03 
c  Velocity[Z]                                      0.42590E-02 
c  Pressure     0.36114E-04     131   0.91863E-02   0.25474E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51921E-08   0.16313E-08 0.10013E+00 
c  r22          0.10852E-01      13   0.49512E-08   0.18521E-08 0.10257E+00 
c  r33          0.21859E-01      15   0.53169E-08   0.12486E-07 0.12809E+00 
c  r12          0.93860E-03      17   0.67358E-08   0.29892E-09 0.60653E+00 
c  r13          0.46675E-02      18   0.70045E-08   0.14919E-08 0.20029E+00 
c  r23          0.39975E-02      19   0.61204E-08   0.12657E-08 0.19964E+00 
c  epsilon      0.10969E+02      11   0.34336E-08   0.96072E-02 0.16438E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84491E-02 0.43341E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63407         0.61358       0.0052565       0.0015074
v  Velocity[Y]            -0.57354         0.54406       0.0030808      0.00087335
v  Velocity[Z]              1.5652           5.438          4.3388          4.3625
v  ǁVelocityǁ                1.579           5.438          4.3406          4.3632
v  Pressure                -36.415          360.04          87.654          169.87
v  r11                   0.0010599        0.081842        0.013073        0.018285
v  r22                   0.0011121        0.082652        0.013353        0.018645
v  r33                   0.0016366         0.17434        0.027249        0.037205
v  r12                   -0.010654        0.013596      -0.0002338      -0.0003093
v  r13                   -0.045549        0.052811      9.3147e-05       0.0010138
v  r23                   -0.046703        0.051217      3.0412e-05      0.00057457
v  epsilon                0.069018          271.24          7.2635          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9919e-05       0.0099176      0.00092486       0.0017426
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb             0.0017846           5.279         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.879         0.71351         0.85284


 TIME FOR THE TIME STEP            10509:        0.80011E+02

===============================================================


 INSTANT    0.105100000E-01   TIME STEP NUMBER           10510
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.954829428E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283460109E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.538293356E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.291649576E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.326731828E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81307E-03   0.45050E-02 0.19886E+01 
c  Velocity[X]                                      0.13827E-03 
c  Velocity[Y]                                      0.12902E-03 
c  Velocity[Z]                                      0.42377E-02 
c  Pressure     0.36312E-04     131   0.92442E-02   0.25613E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.48992E-08   0.16280E-08 0.99723E-01 
c  r22          0.10852E-01      13   0.47821E-08   0.18276E-08 0.10195E+00 
c  r33          0.21859E-01      15   0.53683E-08   0.12466E-07 0.12732E+00 
c  r12          0.93860E-03      17   0.63978E-08   0.30276E-09 0.60995E+00 
c  r13          0.46675E-02      19   0.56076E-08   0.14907E-08 0.19927E+00 
c  r23          0.39975E-02      19   0.57498E-08   0.12754E-08 0.19945E+00 
c  epsilon      0.10969E+02      11   0.33455E-08   0.97414E-02 0.16422E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.83690E-02 0.43135E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63405         0.61361       0.0052565       0.0015074
v  Velocity[Y]            -0.57349         0.54411       0.0030808      0.00087337
v  Velocity[Z]              1.5652           5.438          4.3388          4.3625
v  ǁVelocityǁ                1.579           5.438          4.3406          4.3632
v  Pressure                -36.479          359.99          87.623          169.83
v  r11                     0.00106        0.081851        0.013073        0.018285
v  r22                   0.0011121        0.082652        0.013353        0.018645
v  r33                   0.0016366         0.17432        0.027249        0.037205
v  r12                   -0.010655        0.013599      -0.0002338      -0.0003093
v  r13                   -0.045551        0.052813      9.3148e-05       0.0010138
v  r23                   -0.046703        0.051204      3.0412e-05      0.00057457
v  epsilon                0.069019          271.26          7.2635          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099177      0.00092487       0.0017426
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2788         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8788          0.7135         0.85283


 TIME FOR THE TIME STEP            10510:        0.81800E+02

===============================================================


 INSTANT    0.105110000E-01   TIME STEP NUMBER           10511
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.450764109E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.628760913E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934911E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.144411956E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.480941183E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.870107847E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81127E-03   0.45330E-02 0.19950E+01 
c  Velocity[X]                                      0.13858E-03 
c  Velocity[Y]                                      0.12893E-03 
c  Velocity[Z]                                      0.42655E-02 
c  Pressure     0.36288E-04     133   0.92343E-02   0.25596E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.47241E-08   0.16691E-08 0.10048E+00 
c  r22          0.10852E-01      13   0.46636E-08   0.18442E-08 0.10191E+00 
c  r33          0.21859E-01      15   0.58315E-08   0.12728E-07 0.12861E+00 
c  r12          0.93860E-03      17   0.66837E-08   0.30153E-09 0.60836E+00 
c  r13          0.46675E-02      18   0.64989E-08   0.14912E-08 0.19968E+00 
c  r23          0.39975E-02      19   0.62301E-08   0.13017E-08 0.20173E+00 
c  epsilon      0.10969E+02      11   0.35048E-08   0.10083E-01 0.16921E+00 
c  TempC        0.25716E+06      16   0.15114E-04   0.84015E-02 0.43282E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63408         0.61361       0.0052565       0.0015074
v  Velocity[Y]            -0.57362         0.54429       0.0030807      0.00087333
v  Velocity[Z]              1.5651           5.438          4.3388          4.3625
v  ǁVelocityǁ               1.5789           5.438          4.3406          4.3632
v  Pressure                -36.417          359.99          87.633          169.83
v  r11                     0.00106         0.08185        0.013073        0.018285
v  r22                   0.0011121        0.082646        0.013353        0.018645
v  r33                   0.0016366         0.17428        0.027249        0.037205
v  r12                   -0.010654        0.013592      -0.0002338      -0.0003093
v  r13                   -0.045548         0.05281       9.315e-05       0.0010138
v  r23                   -0.046704        0.051202      3.0413e-05      0.00057457
v  epsilon                 0.06902          271.23          7.2635          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099177      0.00092487       0.0017426
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2783         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8783          0.7135         0.85283


 TIME FOR THE TIME STEP            10511:        0.80958E+02

===============================================================


 INSTANT    0.105120000E-01   TIME STEP NUMBER           10512
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.552997664E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.440698599E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.484443134E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.253167399E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.101377972E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81297E-03   0.45289E-02 0.19925E+01 
c  Velocity[X]                                      0.13833E-03 
c  Velocity[Y]                                      0.12900E-03 
c  Velocity[Z]                                      0.42616E-02 
c  Pressure     0.36203E-04     133   0.92076E-02   0.25537E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50726E-08   0.16567E-08 0.10027E+00 
c  r22          0.10852E-01      13   0.47379E-08   0.18461E-08 0.10199E+00 
c  r33          0.21859E-01      15   0.66668E-08   0.12688E-07 0.12806E+00 
c  r12          0.93860E-03      17   0.67361E-08   0.30715E-09 0.60945E+00 
c  r13          0.46675E-02      19   0.57623E-08   0.15047E-08 0.20000E+00 
c  r23          0.39975E-02      19   0.57375E-08   0.13196E-08 0.20179E+00 
c  epsilon      0.10969E+02      11   0.35992E-08   0.10119E-01 0.16702E+00 
c  TempC        0.25716E+06      16   0.15164E-04   0.84423E-02 0.43372E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63414         0.61357       0.0052565       0.0015074
v  Velocity[Y]            -0.57348         0.54403       0.0030808      0.00087333
v  Velocity[Z]              1.5652           5.438          4.3388          4.3625
v  ǁVelocityǁ                1.579           5.438          4.3406          4.3632
v  Pressure                -36.481          360.03          87.658          169.86
v  r11                     0.00106         0.08185        0.013073        0.018285
v  r22                   0.0011121        0.082646        0.013353        0.018645
v  r33                   0.0016367          0.1743        0.027249        0.037205
v  r12                   -0.010653        0.013584      -0.0002338     -0.00030931
v  r13                   -0.045546         0.05281      9.3151e-05       0.0010138
v  r23                   -0.046703         0.05123      3.0414e-05      0.00057457
v  epsilon                0.069021          271.26          7.2635          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099177      0.00092487       0.0017426
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2789         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8789          0.7135         0.85283


 TIME FOR THE TIME STEP            10512:        0.79010E+02

===============================================================


 INSTANT    0.105130000E-01   TIME STEP NUMBER           10513
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.482556321E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.512886461E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.439494796E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.128914427E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.224755492E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81304E-03   0.45036E-02 0.19856E+01 
c  Velocity[X]                                      0.13826E-03 
c  Velocity[Y]                                      0.12775E-03 
c  Velocity[Z]                                      0.42376E-02 
c  Pressure     0.36464E-04     136   0.92759E-02   0.25721E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49193E-08   0.16586E-08 0.10066E+00 
c  r22          0.10852E-01      13   0.51542E-08   0.18851E-08 0.10346E+00 
c  r33          0.21859E-01      15   0.60139E-08   0.12640E-07 0.12854E+00 
c  r12          0.93860E-03      17   0.69090E-08   0.30828E-09 0.61341E+00 
c  r13          0.46675E-02      19   0.54100E-08   0.15089E-08 0.20076E+00 
c  r23          0.39976E-02      19   0.60476E-08   0.12958E-08 0.20106E+00 
c  epsilon      0.10969E+02      11   0.34114E-08   0.96795E-02 0.16336E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.83900E-02 0.43256E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161988


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63407         0.61362       0.0052565       0.0015074
v  Velocity[Y]            -0.57349         0.54401       0.0030807      0.00087331
v  Velocity[Z]              1.5653           5.438          4.3388          4.3625
v  ǁVelocityǁ               1.5791           5.438          4.3406          4.3632
v  Pressure                -36.447          360.06          87.665          169.89
v  r11                     0.00106        0.081851        0.013073        0.018285
v  r22                   0.0011122        0.082647        0.013353        0.018645
v  r33                   0.0016367         0.17433        0.027249        0.037205
v  r12                   -0.010652        0.013574      -0.0002338     -0.00030931
v  r13                    -0.04555        0.052808      9.3152e-05       0.0010138
v  r23                   -0.046703        0.051214      3.0414e-05      0.00057457
v  epsilon                0.069022          271.26          7.2635          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05       0.0099177      0.00092487       0.0017426
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2789         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8789          0.7135         0.85283


 TIME FOR THE TIME STEP            10513:        0.79798E+02

===============================================================


 INSTANT    0.105140000E-01   TIME STEP NUMBER           10514
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.101991658E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.824071403E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.343919819E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.475256578E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.957929983E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81215E-03   0.45175E-02 0.19941E+01 
c  Velocity[X]                                      0.13863E-03 
c  Velocity[Y]                                      0.12864E-03 
c  Velocity[Z]                                      0.42502E-02 
c  Pressure     0.36531E-04     131   0.93000E-02   0.25768E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53279E-08   0.16470E-08 0.10051E+00 
c  r22          0.10852E-01      13   0.53055E-08   0.18351E-08 0.10237E+00 
c  r33          0.21859E-01      15   0.63416E-08   0.12581E-07 0.12839E+00 
c  r12          0.93860E-03      18   0.50726E-08   0.29905E-09 0.60966E+00 
c  r13          0.46675E-02      19   0.57053E-08   0.14939E-08 0.20038E+00 
c  r23          0.39976E-02      19   0.68520E-08   0.12833E-08 0.19996E+00 
c  epsilon      0.10969E+02      11   0.32635E-08   0.97736E-02 0.16588E+00 
c  TempC        0.25716E+06      16   0.15166E-04   0.84326E-02 0.43289E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63403          0.6136       0.0052565       0.0015074
v  Velocity[Y]            -0.57351         0.54412       0.0030807      0.00087328
v  Velocity[Z]              1.5651          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4381          4.3406          4.3632
v  Pressure                -36.435          359.93          87.606          169.78
v  r11                     0.00106        0.081867        0.013073        0.018285
v  r22                   0.0011122        0.082647        0.013353        0.018645
v  r33                   0.0016367         0.17431        0.027249        0.037205
v  r12                   -0.010654        0.013578      -0.0002338     -0.00030931
v  r13                   -0.045547        0.052809      9.3153e-05       0.0010138
v  r23                   -0.046702        0.051198      3.0414e-05      0.00057457
v  epsilon                0.069024          271.28          7.2635          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099177      0.00092487       0.0017426
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2796         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8796          0.7135         0.85283


 TIME FOR THE TIME STEP            10514:        0.82129E+02

===============================================================


 INSTANT    0.105150000E-01   TIME STEP NUMBER           10515
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.450103382E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.244414781E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.165814147E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.251684050E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.289797625E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81197E-03   0.45463E-02 0.19947E+01 
c  Velocity[X]                                      0.13934E-03 
c  Velocity[Y]                                      0.12886E-03 
c  Velocity[Z]                                      0.42781E-02 
c  Pressure     0.36148E-04     133   0.91982E-02   0.25498E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52015E-08   0.16420E-08 0.10024E+00 
c  r22          0.10852E-01      13   0.54193E-08   0.18398E-08 0.10223E+00 
c  r33          0.21859E-01      15   0.62701E-08   0.12584E-07 0.12802E+00 
c  r12          0.93860E-03      18   0.55512E-08   0.29594E-09 0.60731E+00 
c  r13          0.46675E-02      19   0.53375E-08   0.14981E-08 0.20034E+00 
c  r23          0.39976E-02      19   0.58638E-08   0.12819E-08 0.19961E+00 
c  epsilon      0.10969E+02      11   0.35129E-08   0.99839E-02 0.16650E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.84500E-02 0.43342E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63407         0.61357       0.0052566       0.0015074
v  Velocity[Y]            -0.57372         0.54426       0.0030808      0.00087333
v  Velocity[Z]              1.5653          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4381          4.3406          4.3632
v  Pressure                -36.388             360          87.628          169.83
v  r11                     0.00106        0.081869        0.013073        0.018285
v  r22                   0.0011122        0.082648        0.013353        0.018645
v  r33                   0.0016367         0.17429        0.027249        0.037205
v  r12                   -0.010653        0.013577      -0.0002338     -0.00030931
v  r13                   -0.045546        0.052809      9.3154e-05       0.0010138
v  r23                   -0.046702        0.051187      3.0415e-05      0.00057457
v  epsilon                0.069025          271.21          7.2635          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9941e-05       0.0099178      0.00092487       0.0017426
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2797         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8797          0.7135         0.85283


 TIME FOR THE TIME STEP            10515:        0.79859E+02

===============================================================


 INSTANT    0.105160000E-01   TIME STEP NUMBER           10516
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.257542053E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69752E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.212006081E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69752E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108427751E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69752E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.243512344E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69752E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169747500E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69752E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81340E-03   0.44667E-02 0.19800E+01 
c  Velocity[X]                                      0.13806E-03 
c  Velocity[Y]                                      0.12833E-03 
c  Velocity[Z]                                      0.42004E-02 
c  Pressure     0.36384E-04     131   0.92629E-02   0.25664E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49822E-08   0.16436E-08 0.99865E-01 
c  r22          0.10852E-01      13   0.54554E-08   0.18127E-08 0.10140E+00 
c  r33          0.21859E-01      15   0.51246E-08   0.12537E-07 0.12738E+00 
c  r12          0.93860E-03      18   0.57461E-08   0.29350E-09 0.60329E+00 
c  r13          0.46675E-02      19   0.56470E-08   0.14991E-08 0.19924E+00 
c  r23          0.39976E-02      19   0.61657E-08   0.12993E-08 0.20037E+00 
c  epsilon      0.10969E+02      11   0.35537E-08   0.99082E-02 0.16478E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.83757E-02 0.43167E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6341         0.61361       0.0052566       0.0015074
v  Velocity[Y]            -0.57367         0.54436       0.0030807       0.0008733
v  Velocity[Z]              1.5654          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4381          4.3406          4.3632
v  Pressure                -36.471          360.05          87.641          169.86
v  r11                     0.00106        0.081864        0.013073        0.018285
v  r22                   0.0011122        0.082648        0.013353        0.018645
v  r33                   0.0016367          0.1743        0.027249        0.037206
v  r12                   -0.010653        0.013574      -0.0002338     -0.00030931
v  r13                   -0.045549        0.052808      9.3155e-05       0.0010138
v  r23                   -0.046701        0.051207      3.0415e-05      0.00057457
v  epsilon                0.069026          271.22          7.2635          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099175      0.00092487       0.0017426
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2797         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8797          0.7135         0.85283


 TIME FOR THE TIME STEP            10516:        0.80679E+02

===============================================================


 INSTANT    0.105170000E-01   TIME STEP NUMBER           10517
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141017540E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.398691759E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.693407285E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.758595786E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227347948E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81132E-03   0.45170E-02 0.19903E+01 
c  Velocity[X]                                      0.13771E-03 
c  Velocity[Y]                                      0.12859E-03 
c  Velocity[Z]                                      0.42507E-02 
c  Pressure     0.36150E-04     132   0.92018E-02   0.25499E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.48319E-08   0.16523E-08 0.10059E+00 
c  r22          0.10852E-01      13   0.56458E-08   0.18169E-08 0.10184E+00 
c  r33          0.21859E-01      15   0.61136E-08   0.12554E-07 0.12815E+00 
c  r12          0.93860E-03      18   0.58858E-08   0.30057E-09 0.60860E+00 
c  r13          0.46675E-02      20   0.59877E-08   0.14972E-08 0.19958E+00 
c  r23          0.39976E-02      20   0.59169E-08   0.12898E-08 0.20114E+00 
c  epsilon      0.10969E+02      11   0.35328E-08   0.10004E-01 0.16897E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.83979E-02 0.43308E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63414          0.6136       0.0052566       0.0015074
v  Velocity[Y]            -0.57365         0.54417       0.0030807      0.00087329
v  Velocity[Z]              1.5654          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4381          4.3406          4.3632
v  Pressure                -36.431          359.98          87.616          169.81
v  r11                     0.00106        0.081862        0.013073        0.018285
v  r22                   0.0011122        0.082643        0.013353        0.018645
v  r33                   0.0016368         0.17433        0.027249        0.037206
v  r12                   -0.010657        0.013581      -0.0002338     -0.00030931
v  r13                   -0.045548        0.052808      9.3156e-05       0.0010138
v  r23                     -0.0467          0.0512      3.0415e-05      0.00057457
v  epsilon                0.069027          271.24          7.2635          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9943e-05       0.0099176      0.00092487       0.0017426
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2797         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8797         0.71351         0.85283


 TIME FOR THE TIME STEP            10517:        0.82979E+02

===============================================================


 INSTANT    0.105180000E-01   TIME STEP NUMBER           10518
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.487312071E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.995185156E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173281173E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100888856E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.478797599E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81245E-03   0.45381E-02 0.19939E+01 
c  Velocity[X]                                      0.13880E-03 
c  Velocity[Y]                                      0.12962E-03 
c  Velocity[Z]                                      0.42697E-02 
c  Pressure     0.36216E-04     132   0.92236E-02   0.25545E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.48874E-08   0.16431E-08 0.99690E-01 
c  r22          0.10852E-01      13   0.58879E-08   0.18130E-08 0.10144E+00 
c  r33          0.21859E-01      15   0.55323E-08   0.12570E-07 0.12769E+00 
c  r12          0.93860E-03      18   0.64928E-08   0.29528E-09 0.60467E+00 
c  r13          0.46675E-02      19   0.65519E-08   0.14883E-08 0.19935E+00 
c  r23          0.39976E-02      19   0.63819E-08   0.13064E-08 0.20069E+00 
c  epsilon      0.10969E+02      11   0.35305E-08   0.98482E-02 0.16467E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84658E-02 0.43387E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63411         0.61358       0.0052565       0.0015074
v  Velocity[Y]            -0.57359         0.54428       0.0030807      0.00087327
v  Velocity[Z]              1.5653          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4381          4.3406          4.3632
v  Pressure                -36.483          359.96          87.602          169.79
v  r11                     0.00106        0.081859        0.013073        0.018285
v  r22                   0.0011122        0.082645        0.013353        0.018645
v  r33                   0.0016368         0.17436        0.027249        0.037206
v  r12                   -0.010657        0.013586      -0.0002338     -0.00030931
v  r13                   -0.045546         0.05281      9.3157e-05       0.0010138
v  r23                     -0.0467        0.051189      3.0415e-05      0.00057457
v  epsilon                0.069028          271.23          7.2635          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099176      0.00092487       0.0017426
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017846            5.28         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178            5.88         0.71351         0.85284


 TIME FOR THE TIME STEP            10518:        0.81536E+02

===============================================================


 INSTANT    0.105190000E-01   TIME STEP NUMBER           10519
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.251643947E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105311252E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.813941900E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.451598873E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100480830E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81372E-03   0.45252E-02 0.19911E+01 
c  Velocity[X]                                      0.13873E-03 
c  Velocity[Y]                                      0.12907E-03 
c  Velocity[Z]                                      0.42574E-02 
c  Pressure     0.36107E-04     133   0.91860E-02   0.25468E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49522E-08   0.16421E-08 0.99984E-01 
c  r22          0.10852E-01      13   0.52836E-08   0.18172E-08 0.10155E+00 
c  r33          0.21859E-01      15   0.51778E-08   0.12459E-07 0.12758E+00 
c  r12          0.93860E-03      18   0.62816E-08   0.29520E-09 0.60576E+00 
c  r13          0.46675E-02      19   0.56054E-08   0.14777E-08 0.19913E+00 
c  r23          0.39976E-02      19   0.65817E-08   0.12918E-08 0.20062E+00 
c  epsilon      0.10969E+02      11   0.34611E-08   0.96835E-02 0.16434E+00 
c  TempC        0.25716E+06      16   0.15104E-04   0.84392E-02 0.43300E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63407         0.61365       0.0052566       0.0015074
v  Velocity[Y]            -0.57373         0.54442       0.0030807      0.00087332
v  Velocity[Z]              1.5654          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4381          4.3406          4.3632
v  Pressure                -36.445          360.04          87.631          169.84
v  r11                     0.00106        0.081863        0.013073        0.018285
v  r22                   0.0011122        0.082646        0.013353        0.018645
v  r33                   0.0016368         0.17434        0.027249        0.037206
v  r12                   -0.010657        0.013584      -0.0002338     -0.00030931
v  r13                   -0.045548        0.052806      9.3158e-05       0.0010138
v  r23                   -0.046698        0.051213      3.0416e-05      0.00057457
v  epsilon                0.069029          271.22          7.2635          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099176      0.00092487       0.0017426
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017846            5.28         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178            5.88         0.71351         0.85283


 TIME FOR THE TIME STEP            10519:        0.75744E+02

===============================================================


 INSTANT    0.105200000E-01   TIME STEP NUMBER           10520
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120203041E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123296116E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934910E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.301857749E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.256589626E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151863991E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81231E-03   0.45127E-02 0.19916E+01 
c  Velocity[X]                                      0.13864E-03 
c  Velocity[Y]                                      0.12824E-03 
c  Velocity[Z]                                      0.42458E-02 
c  Pressure     0.36256E-04     132   0.92291E-02   0.25574E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.48581E-08   0.16680E-08 0.10096E+00 
c  r22          0.10852E-01      13   0.50458E-08   0.18420E-08 0.10203E+00 
c  r33          0.21859E-01      15   0.64834E-08   0.12700E-07 0.12863E+00 
c  r12          0.93860E-03      18   0.52854E-08   0.30033E-09 0.61001E+00 
c  r13          0.46675E-02      18   0.70057E-08   0.15259E-08 0.20095E+00 
c  r23          0.39976E-02      19   0.57067E-08   0.12986E-08 0.20129E+00 
c  epsilon      0.10969E+02      11   0.34413E-08   0.97820E-02 0.16595E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.83903E-02 0.43175E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63418         0.61361       0.0052565       0.0015073
v  Velocity[Y]            -0.57371         0.54423       0.0030806      0.00087327
v  Velocity[Z]              1.5655          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4381          4.3406          4.3632
v  Pressure                -36.479          360.07          87.674          169.88
v  r11                     0.00106        0.081869        0.013073        0.018285
v  r22                   0.0011122        0.082646        0.013353        0.018645
v  r33                   0.0016368          0.1743        0.027249        0.037206
v  r12                   -0.010656        0.013581      -0.0002338     -0.00030931
v  r13                   -0.045546        0.052805      9.3159e-05       0.0010138
v  r23                   -0.046696        0.051205      3.0417e-05      0.00057457
v  epsilon                 0.06903          271.17          7.2635          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05       0.0099176      0.00092488       0.0017427
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2796         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8796         0.71351         0.85284


 TIME FOR THE TIME STEP            10520:        0.78733E+02

===============================================================


 INSTANT    0.105210000E-01   TIME STEP NUMBER           10521
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.473107125E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267115597E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182997831E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.289510167E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285108309E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81219E-03   0.45321E-02 0.19926E+01 
c  Velocity[X]                                      0.13855E-03 
c  Velocity[Y]                                      0.12893E-03 
c  Velocity[Z]                                      0.42646E-02 
c  Pressure     0.36190E-04     133   0.92074E-02   0.25528E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51392E-08   0.17066E-08 0.10195E+00 
c  r22          0.10852E-01      13   0.50716E-08   0.18495E-08 0.10232E+00 
c  r33          0.21859E-01      15   0.64216E-08   0.12767E-07 0.12917E+00 
c  r12          0.93860E-03      18   0.54096E-08   0.30889E-09 0.61588E+00 
c  r13          0.46675E-02      18   0.69444E-08   0.14700E-08 0.19859E+00 
c  r23          0.39976E-02      19   0.56731E-08   0.13150E-08 0.20300E+00 
c  epsilon      0.10969E+02      11   0.35262E-08   0.96178E-02 0.16268E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.84178E-02 0.43336E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63417         0.61358       0.0052566       0.0015074
v  Velocity[Y]            -0.57377         0.54431       0.0030807      0.00087332
v  Velocity[Z]              1.5656          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4381          4.3406          4.3632
v  Pressure                -36.423          359.98          87.623          169.82
v  r11                     0.00106        0.081872        0.013073        0.018285
v  r22                   0.0011122        0.082646        0.013353        0.018645
v  r33                   0.0016368         0.17431        0.027249        0.037206
v  r12                   -0.010655        0.013581      -0.0002338     -0.00030931
v  r13                   -0.045547        0.052805       9.316e-05       0.0010138
v  r23                   -0.046694        0.051186      3.0419e-05      0.00057457
v  epsilon                0.069031          271.18          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9955e-05       0.0099176      0.00092488       0.0017427
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2793         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8793          0.7135         0.85283


 TIME FOR THE TIME STEP            10521:        0.77123E+02

===============================================================


 INSTANT    0.105220000E-01   TIME STEP NUMBER           10522
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237851717E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133983241E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.336650270E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141771522E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.815647416E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81299E-03   0.45241E-02 0.19922E+01 
c  Velocity[X]                                      0.13831E-03 
c  Velocity[Y]                                      0.12895E-03 
c  Velocity[Z]                                      0.42569E-02 
c  Pressure     0.36339E-04     133   0.92499E-02   0.25632E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54513E-08   0.16492E-08 0.10040E+00 
c  r22          0.10852E-01      13   0.49180E-08   0.18835E-08 0.10306E+00 
c  r33          0.21859E-01      15   0.62307E-08   0.12695E-07 0.12845E+00 
c  r12          0.93860E-03      18   0.62451E-08   0.30510E-09 0.61176E+00 
c  r13          0.46675E-02      18   0.70603E-08   0.15036E-08 0.20057E+00 
c  r23          0.39976E-02      19   0.60806E-08   0.12964E-08 0.20055E+00 
c  epsilon      0.10969E+02      11   0.35514E-08   0.99221E-02 0.16534E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.83983E-02 0.43244E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63412         0.61361       0.0052566       0.0015074
v  Velocity[Y]            -0.57373         0.54445       0.0030807       0.0008733
v  Velocity[Z]              1.5657          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4381          4.3406          4.3632
v  Pressure                -36.448             360          87.623          169.82
v  r11                     0.00106        0.081885        0.013073        0.018285
v  r22                   0.0011123        0.082647        0.013353        0.018646
v  r33                   0.0016369         0.17434        0.027249        0.037206
v  r12                    -0.01066        0.013584      -0.0002338     -0.00030931
v  r13                   -0.045549        0.052807      9.3159e-05       0.0010138
v  r23                   -0.046693         0.05121      3.0419e-05      0.00057457
v  epsilon                0.069032           271.2          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099177      0.00092488       0.0017427
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2788         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8788          0.7135         0.85283


 TIME FOR THE TIME STEP            10522:        0.77175E+02

===============================================================


 INSTANT    0.105230000E-01   TIME STEP NUMBER           10523
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.228172403E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.284261398E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.294338379E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201527284E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.243058390E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81206E-03   0.45039E-02 0.19869E+01 
c  Velocity[X]                                      0.13842E-03 
c  Velocity[Y]                                      0.12875E-03 
c  Velocity[Z]                                      0.42368E-02 
c  Pressure     0.36243E-04     132   0.92278E-02   0.25565E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55874E-08   0.17100E-08 0.10186E+00 
c  r22          0.10852E-01      13   0.48430E-08   0.18372E-08 0.10202E+00 
c  r33          0.21859E-01      15   0.71033E-08   0.12818E-07 0.12913E+00 
c  r12          0.93860E-03      18   0.59189E-08   0.30701E-09 0.61377E+00 
c  r13          0.46675E-02      18   0.71692E-08   0.14998E-08 0.19982E+00 
c  r23          0.39976E-02      19   0.61140E-08   0.13401E-08 0.20401E+00 
c  epsilon      0.10969E+02      11   0.36275E-08   0.10155E-01 0.17063E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.83933E-02 0.43218E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63419          0.6136       0.0052567       0.0015074
v  Velocity[Y]            -0.57376         0.54426       0.0030807      0.00087332
v  Velocity[Z]              1.5656          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4381          4.3406          4.3632
v  Pressure                -36.395          360.04          87.656          169.86
v  r11                     0.00106        0.081901        0.013073        0.018285
v  r22                   0.0011123        0.082643        0.013353        0.018646
v  r33                   0.0016369         0.17431        0.027249        0.037206
v  r12                   -0.010659        0.013586      -0.0002338     -0.00030931
v  r13                   -0.045546        0.052808       9.316e-05       0.0010138
v  r23                   -0.046691        0.051207      3.0419e-05      0.00057457
v  epsilon                0.069033          271.19          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9963e-05       0.0099179      0.00092488       0.0017427
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2784         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8784          0.7135         0.85283


 TIME FOR THE TIME STEP            10523:        0.81424E+02

===============================================================


 INSTANT    0.105240000E-01   TIME STEP NUMBER           10524
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.170633959E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.989319519E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160322415E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.234104955E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.311019518E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81310E-03   0.45188E-02 0.19898E+01 
c  Velocity[X]                                      0.13847E-03 
c  Velocity[Y]                                      0.12826E-03 
c  Velocity[Z]                                      0.42521E-02 
c  Pressure     0.36422E-04     132   0.92643E-02   0.25691E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60029E-08   0.16269E-08 0.10002E+00 
c  r22          0.10852E-01      13   0.48224E-08   0.17957E-08 0.10099E+00 
c  r33          0.21859E-01      15   0.58309E-08   0.12250E-07 0.12645E+00 
c  r12          0.93860E-03      18   0.53121E-08   0.29416E-09 0.60400E+00 
c  r13          0.46675E-02      19   0.59974E-08   0.14784E-08 0.19859E+00 
c  r23          0.39976E-02      19   0.57175E-08   0.12668E-08 0.19847E+00 
c  epsilon      0.10969E+02      11   0.33356E-08   0.95809E-02 0.16318E+00 
c  TempC        0.25716E+06      16   0.15169E-04   0.84720E-02 0.43456E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63414         0.61359       0.0052567       0.0015074
v  Velocity[Y]            -0.57375         0.54435       0.0030807      0.00087333
v  Velocity[Z]              1.5657          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4381          4.3406          4.3632
v  Pressure                 -36.47          360.04           87.66          169.87
v  r11                   0.0010601        0.081908        0.013073        0.018285
v  r22                   0.0011123        0.082644        0.013353        0.018646
v  r33                   0.0016369         0.17429        0.027249        0.037206
v  r12                    -0.01066        0.013586      -0.0002338     -0.00030931
v  r13                   -0.045546        0.052808      9.3161e-05       0.0010138
v  r23                    -0.04669        0.051199       3.042e-05      0.00057457
v  epsilon                0.069034          271.17          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9963e-05       0.0099179      0.00092488       0.0017427
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2777         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8777          0.7135         0.85283


 TIME FOR THE TIME STEP            10524:        0.78556E+02

===============================================================


 INSTANT    0.105250000E-01   TIME STEP NUMBER           10525
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.418114179E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130015666E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.570864879E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.257361118E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.312462565E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81261E-03   0.45247E-02 0.19915E+01 
c  Velocity[X]                                      0.13843E-03 
c  Velocity[Y]                                      0.12876E-03 
c  Velocity[Z]                                      0.42575E-02 
c  Pressure     0.36429E-04     132   0.92750E-02   0.25695E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58206E-08   0.16361E-08 0.10025E+00 
c  r22          0.10852E-01      13   0.49299E-08   0.18256E-08 0.10141E+00 
c  r33          0.21859E-01      15   0.57969E-08   0.12413E-07 0.12731E+00 
c  r12          0.93860E-03      18   0.53880E-08   0.29536E-09 0.60564E+00 
c  r13          0.46675E-02      19   0.58334E-08   0.14823E-08 0.19906E+00 
c  r23          0.39976E-02      19   0.55666E-08   0.12679E-08 0.19938E+00 
c  epsilon      0.10969E+02      11   0.31757E-08   0.96608E-02 0.16274E+00 
c  TempC        0.25716E+06      16   0.15102E-04   0.84155E-02 0.43237E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63413         0.61364       0.0052567       0.0015074
v  Velocity[Y]            -0.57392         0.54446       0.0030808      0.00087332
v  Velocity[Z]              1.5657          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4381          4.3406          4.3632
v  Pressure                -36.443          360.02          87.628          169.85
v  r11                   0.0010601         0.08192        0.013073        0.018285
v  r22                   0.0011123        0.082646        0.013353        0.018646
v  r33                   0.0016369         0.17431        0.027249        0.037206
v  r12                   -0.010659        0.013584      -0.0002338     -0.00030931
v  r13                    -0.04555        0.052805      9.3162e-05       0.0010138
v  r23                   -0.046689        0.051213      3.0421e-05      0.00057457
v  epsilon                0.069035          271.17          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9967e-05       0.0099179      0.00092488       0.0017427
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8783         0.71351         0.85284


 TIME FOR THE TIME STEP            10525:        0.76822E+02

===============================================================


 INSTANT    0.105260000E-01   TIME STEP NUMBER           10526
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.218886012E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.369567945E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115363329E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.105666528E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.435306569E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81297E-03   0.45323E-02 0.19950E+01 
c  Velocity[X]                                      0.13825E-03 
c  Velocity[Y]                                      0.12951E-03 
c  Velocity[Z]                                      0.42645E-02 
c  Pressure     0.36320E-04     133   0.92435E-02   0.25619E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52670E-08   0.16262E-08 0.99393E-01 
c  r22          0.10852E-01      13   0.47979E-08   0.18019E-08 0.10092E+00 
c  r33          0.21859E-01      15   0.67975E-08   0.12400E-07 0.12667E+00 
c  r12          0.93860E-03      18   0.53797E-08   0.29997E-09 0.60559E+00 
c  r13          0.46675E-02      19   0.55652E-08   0.14942E-08 0.19908E+00 
c  r23          0.39976E-02      19   0.56789E-08   0.12875E-08 0.19925E+00 
c  epsilon      0.10969E+02      11   0.33672E-08   0.98229E-02 0.16477E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.83873E-02 0.43156E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63418         0.61359       0.0052566       0.0015074
v  Velocity[Y]            -0.57371         0.54427       0.0030807      0.00087329
v  Velocity[Z]              1.5655          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4381          4.3406          4.3632
v  Pressure                -36.435             360          87.644          169.84
v  r11                   0.0010601        0.081927        0.013073        0.018285
v  r22                   0.0011123        0.082647        0.013353        0.018646
v  r33                   0.0016369         0.17432        0.027249        0.037206
v  r12                   -0.010659        0.013585      -0.0002338     -0.00030931
v  r13                   -0.045546        0.052806      9.3164e-05       0.0010138
v  r23                   -0.046689         0.05121      3.0423e-05      0.00057458
v  epsilon                0.069037          271.21          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9968e-05       0.0099177      0.00092488       0.0017427
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2775         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8775          0.7135         0.85283


 TIME FOR THE TIME STEP            10526:        0.75716E+02

===============================================================


 INSTANT    0.105270000E-01   TIME STEP NUMBER           10527
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.264292271E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221276549E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.978352008E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.444085537E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116230870E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81298E-03   0.45427E-02 0.19938E+01 
c  Velocity[X]                                      0.13869E-03 
c  Velocity[Y]                                      0.12854E-03 
c  Velocity[Z]                                      0.42755E-02 
c  Pressure     0.36599E-04     132   0.93115E-02   0.25815E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54171E-08   0.16104E-08 0.99183E-01 
c  r22          0.10852E-01      13   0.45783E-08   0.17895E-08 0.10093E+00 
c  r33          0.21859E-01      15   0.63649E-08   0.12249E-07 0.12646E+00 
c  r12          0.93860E-03      18   0.49801E-08   0.28442E-09 0.59797E+00 
c  r13          0.46675E-02      19   0.58225E-08   0.14632E-08 0.19844E+00 
c  r23          0.39976E-02      19   0.65862E-08   0.12700E-08 0.19822E+00 
c  epsilon      0.10969E+02      11   0.32970E-08   0.93279E-02 0.16096E+00 
c  TempC        0.25716E+06      16   0.15112E-04   0.84573E-02 0.43443E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63407         0.61359       0.0052567       0.0015074
v  Velocity[Y]            -0.57383         0.54431       0.0030808      0.00087333
v  Velocity[Z]              1.5656          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4381          4.3406          4.3632
v  Pressure                -36.421          359.95          87.597          169.79
v  r11                   0.0010601        0.081932        0.013073        0.018285
v  r22                   0.0011123        0.082647        0.013353        0.018646
v  r33                   0.0016369         0.17436        0.027249        0.037206
v  r12                   -0.010657        0.013585      -0.0002338     -0.00030931
v  r13                   -0.045546        0.052804      9.3165e-05       0.0010138
v  r23                   -0.046689          0.0512      3.0424e-05      0.00057458
v  epsilon                0.069038           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.997e-05       0.0099178      0.00092488       0.0017427
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017846           5.278         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.878          0.7135         0.85283


 TIME FOR THE TIME STEP            10527:        0.82970E+02

===============================================================


 INSTANT    0.105280000E-01   TIME STEP NUMBER           10528
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.228482294E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.176635011E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239782434E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.145578852E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.384081365E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81336E-03   0.44945E-02 0.19851E+01 
c  Velocity[X]                                      0.13824E-03 
c  Velocity[Y]                                      0.12844E-03 
c  Velocity[Z]                                      0.42278E-02 
c  Pressure     0.36547E-04     132   0.93064E-02   0.25778E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52883E-08   0.16628E-08 0.10023E+00 
c  r22          0.10852E-01      13   0.47792E-08   0.18474E-08 0.10180E+00 
c  r33          0.21859E-01      15   0.65403E-08   0.12686E-07 0.12804E+00 
c  r12          0.93860E-03      18   0.53654E-08   0.29921E-09 0.60512E+00 
c  r13          0.46675E-02      18   0.70302E-08   0.15010E-08 0.20021E+00 
c  r23          0.39976E-02      19   0.54642E-08   0.13078E-08 0.20128E+00 
c  epsilon      0.10969E+02      11   0.34560E-08   0.10183E-01 0.16719E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.83567E-02 0.43154E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6341         0.61364       0.0052566       0.0015074
v  Velocity[Y]            -0.57384         0.54442       0.0030808       0.0008733
v  Velocity[Z]              1.5655          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4381          4.3406          4.3632
v  Pressure                -36.471          360.03           87.64          169.85
v  r11                   0.0010601        0.081937        0.013073        0.018286
v  r22                   0.0011123        0.082646        0.013353        0.018646
v  r33                    0.001637         0.17434        0.027249        0.037206
v  r12                   -0.010658        0.013582      -0.0002338     -0.00030931
v  r13                   -0.045547        0.052805      9.3165e-05       0.0010138
v  r23                   -0.046689        0.051225      3.0424e-05      0.00057458
v  epsilon                0.069039          271.22          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9971e-05       0.0099177      0.00092488       0.0017427
v  CourantNb               0.44217             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8783         0.71351         0.85284


 TIME FOR THE TIME STEP            10528:        0.82001E+02

===============================================================


 INSTANT    0.105290000E-01   TIME STEP NUMBER           10529
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.934454351E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.148137153E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.496181766E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.110646027E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.627066119E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81137E-03   0.45358E-02 0.19956E+01 
c  Velocity[X]                                      0.13863E-03 
c  Velocity[Y]                                      0.12874E-03 
c  Velocity[Z]                                      0.42685E-02 
c  Pressure     0.36463E-04     133   0.92784E-02   0.25722E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54456E-08   0.16404E-08 0.99463E-01 
c  r22          0.10852E-01      13   0.52627E-08   0.18251E-08 0.10114E+00 
c  r33          0.21859E-01      14   0.70856E-08   0.12586E-07 0.12704E+00 
c  r12          0.93860E-03      18   0.60810E-08   0.29854E-09 0.60511E+00 
c  r13          0.46675E-02      19   0.60217E-08   0.15105E-08 0.19941E+00 
c  r23          0.39976E-02      19   0.56253E-08   0.12992E-08 0.19961E+00 
c  epsilon      0.10969E+02      11   0.33121E-08   0.10241E-01 0.16950E+00 
c  TempC        0.25716E+06      16   0.15142E-04   0.84241E-02 0.43266E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63411         0.61362       0.0052566       0.0015074
v  Velocity[Y]            -0.57389         0.54414       0.0030808       0.0008733
v  Velocity[Z]              1.5657          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4381          4.3406          4.3632
v  Pressure                -36.392          360.03           87.64          169.85
v  r11                   0.0010601        0.081941        0.013073        0.018286
v  r22                   0.0011123        0.082645        0.013353        0.018646
v  r33                    0.001637          0.1743        0.027249        0.037206
v  r12                    -0.01066        0.013581      -0.0002338     -0.00030931
v  r13                   -0.045546        0.052806      9.3165e-05       0.0010138
v  r23                   -0.046689        0.051207      3.0425e-05      0.00057458
v  epsilon                 0.06904          271.18          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9973e-05       0.0099176      0.00092489       0.0017427
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2783         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8783         0.71351         0.85284


 TIME FOR THE TIME STEP            10529:        0.82865E+02

===============================================================


 INSTANT    0.105300000E-01   TIME STEP NUMBER           10530
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.151912472E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.285092315E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.279549277E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.112205220E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127793725E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81273E-03   0.45287E-02 0.19930E+01 
c  Velocity[X]                                      0.13857E-03 
c  Velocity[Y]                                      0.12962E-03 
c  Velocity[Z]                                      0.42605E-02 
c  Pressure     0.35962E-04     131   0.91554E-02   0.25366E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56352E-08   0.16191E-08 0.99410E-01 
c  r22          0.10852E-01      13   0.50766E-08   0.18098E-08 0.10102E+00 
c  r33          0.21859E-01      15   0.58428E-08   0.12284E-07 0.12613E+00 
c  r12          0.93860E-03      18   0.51750E-08   0.29052E-09 0.59970E+00 
c  r13          0.46675E-02      19   0.55654E-08   0.14801E-08 0.19856E+00 
c  r23          0.39976E-02      19   0.56560E-08   0.12562E-08 0.19740E+00 
c  epsilon      0.10969E+02      10   0.53919E-08   0.96334E-02 0.16346E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.84658E-02 0.43389E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63414         0.61359       0.0052566       0.0015073
v  Velocity[Y]            -0.57385         0.54415       0.0030807      0.00087329
v  Velocity[Z]              1.5658          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4381          4.3406          4.3632
v  Pressure                -36.474          359.98          87.623          169.81
v  r11                   0.0010601        0.081936        0.013073        0.018286
v  r22                   0.0011124        0.082646        0.013353        0.018646
v  r33                    0.001637         0.17431        0.027249        0.037206
v  r12                   -0.010661        0.013578      -0.0002338     -0.00030931
v  r13                   -0.045545        0.052808      9.3167e-05       0.0010138
v  r23                   -0.046689        0.051189      3.0425e-05      0.00057458
v  epsilon                0.069041           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9975e-05       0.0099177      0.00092489       0.0017427
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017846           5.278         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.878          0.7135         0.85283


 TIME FOR THE TIME STEP            10530:        0.83328E+02

===============================================================


 INSTANT    0.105310000E-01   TIME STEP NUMBER           10531
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122091609E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136592644E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.772650728E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.118470299E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229642898E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81395E-03   0.44871E-02 0.19820E+01 
c  Velocity[X]                                      0.13778E-03 
c  Velocity[Y]                                      0.12748E-03 
c  Velocity[Z]                                      0.42218E-02 
c  Pressure     0.36308E-04     133   0.92423E-02   0.25611E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55008E-08   0.16204E-08 0.98666E-01 
c  r22          0.10852E-01      13   0.47482E-08   0.18486E-08 0.10153E+00 
c  r33          0.21859E-01      15   0.54611E-08   0.12523E-07 0.12643E+00 
c  r12          0.93860E-03      18   0.52661E-08   0.30092E-09 0.60760E+00 
c  r13          0.46675E-02      19   0.56810E-08   0.14963E-08 0.19938E+00 
c  r23          0.39976E-02      19   0.54621E-08   0.12628E-08 0.19677E+00 
c  epsilon      0.10969E+02      11   0.31872E-08   0.98887E-02 0.16375E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.83827E-02 0.43224E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63404         0.61365       0.0052567       0.0015074
v  Velocity[Y]            -0.57374         0.54423       0.0030808      0.00087332
v  Velocity[Z]              1.5655          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4381          4.3406          4.3632
v  Pressure                -36.436          360.07          87.667          169.88
v  r11                   0.0010601        0.081927        0.013073        0.018286
v  r22                   0.0011124        0.082641        0.013353        0.018646
v  r33                    0.001637         0.17434        0.027249        0.037206
v  r12                   -0.010658        0.013575      -0.0002338     -0.00030931
v  r13                   -0.045547        0.052808      9.3167e-05       0.0010138
v  r23                   -0.046689        0.051175      3.0426e-05      0.00057458
v  epsilon                0.069042          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9976e-05       0.0099177      0.00092489       0.0017427
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2775         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8775         0.71351         0.85284


 TIME FOR THE TIME STEP            10531:        0.85941E+02

===============================================================


 INSTANT    0.105320000E-01   TIME STEP NUMBER           10532
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.132217840E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.314005174E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.144346118E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.344338866E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.244830649E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81158E-03   0.45018E-02 0.19888E+01 
c  Velocity[X]                                      0.13845E-03 
c  Velocity[Y]                                      0.12863E-03 
c  Velocity[Z]                                      0.42348E-02 
c  Pressure     0.36264E-04     133   0.92315E-02   0.25579E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54494E-08   0.16190E-08 0.99056E-01 
c  r22          0.10852E-01      13   0.46913E-08   0.18115E-08 0.10104E+00 
c  r33          0.21860E-01      15   0.52938E-08   0.12417E-07 0.12696E+00 
c  r12          0.93860E-03      18   0.51323E-08   0.29143E-09 0.59920E+00 
c  r13          0.46675E-02      19   0.53679E-08   0.14959E-08 0.19970E+00 
c  r23          0.39976E-02      19   0.59584E-08   0.12730E-08 0.19815E+00 
c  epsilon      0.10969E+02      11   0.32685E-08   0.96426E-02 0.16378E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83922E-02 0.43233E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6341         0.61362       0.0052567       0.0015073
v  Velocity[Y]            -0.57361         0.54435       0.0030807      0.00087329
v  Velocity[Z]              1.5656          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4381          4.3406          4.3632
v  Pressure                -36.449          359.99           87.63          169.83
v  r11                   0.0010601        0.081919        0.013073        0.018286
v  r22                   0.0011124        0.082641        0.013353        0.018646
v  r33                    0.001637          0.1743        0.027249        0.037206
v  r12                   -0.010657        0.013575      -0.0002338     -0.00030931
v  r13                   -0.045544        0.052808      9.3168e-05       0.0010138
v  r23                   -0.046689        0.051211      3.0426e-05      0.00057458
v  epsilon                0.069043          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9973e-05       0.0099178      0.00092489       0.0017427
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017846           5.277         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.877         0.71351         0.85284


 TIME FOR THE TIME STEP            10532:        0.83743E+02

===============================================================


 INSTANT    0.105330000E-01   TIME STEP NUMBER           10533
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115728371E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.103892548E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.426719558E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.260280743E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.270844029E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81267E-03   0.45366E-02 0.19941E+01 
c  Velocity[X]                                      0.13868E-03 
c  Velocity[Y]                                      0.12920E-03 
c  Velocity[Z]                                      0.42687E-02 
c  Pressure     0.36690E-04     132   0.93398E-02   0.25880E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54459E-08   0.16408E-08 0.99168E-01 
c  r22          0.10852E-01      13   0.47598E-08   0.18351E-08 0.10119E+00 
c  r33          0.21859E-01      15   0.56450E-08   0.12640E-07 0.12698E+00 
c  r12          0.93860E-03      18   0.53574E-08   0.29898E-09 0.60262E+00 
c  r13          0.46675E-02      18   0.70500E-08   0.14993E-08 0.19934E+00 
c  r23          0.39976E-02      19   0.57098E-08   0.12967E-08 0.19842E+00 
c  epsilon      0.10969E+02      11   0.34017E-08   0.10175E-01 0.16604E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.84537E-02 0.43424E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63413         0.61359       0.0052566       0.0015074
v  Velocity[Y]            -0.57374         0.54409       0.0030808      0.00087333
v  Velocity[Z]              1.5656          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4381          4.3406          4.3632
v  Pressure                -36.396          360.04          87.662          169.87
v  r11                   0.0010601         0.08191        0.013073        0.018286
v  r22                   0.0011124        0.082641        0.013353        0.018646
v  r33                   0.0016371         0.17429        0.027249        0.037206
v  r12                   -0.010659        0.013574      -0.0002338     -0.00030931
v  r13                   -0.045545        0.052805      9.3168e-05       0.0010138
v  r23                   -0.046689        0.051199      3.0427e-05      0.00057458
v  epsilon                0.069044          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9973e-05       0.0099178      0.00092489       0.0017427
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2775         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8775         0.71351         0.85283


 TIME FOR THE TIME STEP            10533:        0.82372E+02

===============================================================


 INSTANT    0.105340000E-01   TIME STEP NUMBER           10534
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.838294031E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.102439872E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.380948580E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.189938761E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.542716236E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81329E-03   0.45214E-02 0.19930E+01 
c  Velocity[X]                                      0.13874E-03 
c  Velocity[Y]                                      0.12856E-03 
c  Velocity[Z]                                      0.42541E-02 
c  Pressure     0.36203E-04     133   0.92173E-02   0.25537E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52708E-08   0.16286E-08 0.99272E-01 
c  r22          0.10852E-01      12   0.63529E-08   0.17841E-08 0.10038E+00 
c  r33          0.21860E-01      15   0.51687E-08   0.12265E-07 0.12594E+00 
c  r12          0.93860E-03      17   0.70771E-08   0.28978E-09 0.59655E+00 
c  r13          0.46675E-02      18   0.63169E-08   0.14585E-08 0.19752E+00 
c  r23          0.39976E-02      19   0.53757E-08   0.12636E-08 0.19715E+00 
c  epsilon      0.10969E+02      11   0.32203E-08   0.95297E-02 0.16164E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.83724E-02 0.43116E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162021


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63407         0.61365       0.0052567       0.0015074
v  Velocity[Y]            -0.57366         0.54418       0.0030808      0.00087334
v  Velocity[Z]              1.5657          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4381          4.3406          4.3632
v  Pressure                -36.467          360.06          87.665          169.88
v  r11                   0.0010601          0.0819        0.013073        0.018286
v  r22                   0.0011124        0.082642        0.013353        0.018646
v  r33                   0.0016371         0.17431        0.027249        0.037206
v  r12                   -0.010659        0.013576      -0.0002338     -0.00030931
v  r13                   -0.045548        0.052806      9.3169e-05       0.0010138
v  r23                   -0.046689        0.051188      3.0428e-05      0.00057458
v  epsilon                0.069045          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.997e-05       0.0099179      0.00092489       0.0017427
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017846          5.2779         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8779          0.7135         0.85283


 TIME FOR THE TIME STEP            10534:        0.82366E+02

===============================================================


 INSTANT    0.105350000E-01   TIME STEP NUMBER           10535
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.135005809E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190515015E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.259748234E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.751991962E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.657029136E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81174E-03   0.45324E-02 0.19939E+01 
c  Velocity[X]                                      0.13843E-03 
c  Velocity[Y]                                      0.12867E-03 
c  Velocity[Z]                                      0.42653E-02 
c  Pressure     0.36345E-04     133   0.92585E-02   0.25636E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51524E-08   0.16671E-08 0.10028E+00 
c  r22          0.10852E-01      12   0.62175E-08   0.18516E-08 0.10189E+00 
c  r33          0.21860E-01      14   0.66168E-08   0.12765E-07 0.12778E+00 
c  r12          0.93860E-03      18   0.50080E-08   0.30007E-09 0.60549E+00 
c  r13          0.46675E-02      18   0.55946E-08   0.15088E-08 0.19959E+00 
c  r23          0.39976E-02      18   0.68490E-08   0.13060E-08 0.20023E+00 
c  epsilon      0.10969E+02      11   0.32029E-08   0.10398E-01 0.17189E+00 
c  TempC        0.25716E+06      16   0.15095E-04   0.84475E-02 0.43328E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63409         0.61364       0.0052567       0.0015074
v  Velocity[Y]            -0.57377         0.54434       0.0030808       0.0008733
v  Velocity[Z]              1.5659          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5797          5.4381          4.3406          4.3632
v  Pressure                -36.438             360           87.65          169.85
v  r11                   0.0010601        0.081906        0.013073        0.018286
v  r22                   0.0011124         0.08264        0.013353        0.018646
v  r33                   0.0016371         0.17433        0.027249        0.037206
v  r12                   -0.010657        0.013579      -0.0002338     -0.00030931
v  r13                   -0.045545        0.052804       9.317e-05       0.0010138
v  r23                   -0.046689        0.051205      3.0427e-05      0.00057458
v  epsilon                0.069046          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9969e-05       0.0099179      0.00092489       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2778         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8778         0.71351         0.85284


 TIME FOR THE TIME STEP            10535:        0.77441E+02

===============================================================


 INSTANT    0.105360000E-01   TIME STEP NUMBER           10536
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.713193470E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.788628304E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.225408753E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.331958579E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.408617064E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81299E-03   0.45271E-02 0.19889E+01 
c  Velocity[X]                                      0.13729E-03 
c  Velocity[Y]                                      0.12811E-03 
c  Velocity[Z]                                      0.42617E-02 
c  Pressure     0.36375E-04     131   0.92652E-02   0.25658E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50927E-08   0.16229E-08 0.99585E-01 
c  r22          0.10852E-01      12   0.64486E-08   0.18135E-08 0.10128E+00 
c  r33          0.21860E-01      14   0.71417E-08   0.12456E-07 0.12697E+00 
c  r12          0.93861E-03      18   0.55375E-08   0.30135E-09 0.60856E+00 
c  r13          0.46675E-02      18   0.68597E-08   0.14929E-08 0.19945E+00 
c  r23          0.39976E-02      18   0.70109E-08   0.12790E-08 0.19925E+00 
c  epsilon      0.10969E+02      11   0.33494E-08   0.95973E-02 0.16275E+00 
c  TempC        0.25716E+06      16   0.15181E-04   0.84057E-02 0.43308E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63408         0.61357       0.0052568       0.0015074
v  Velocity[Y]             -0.5737         0.54408       0.0030808      0.00087332
v  Velocity[Z]              1.5657          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4381          4.3406          4.3632
v  Pressure                -36.459          359.98          87.633          169.83
v  r11                   0.0010601        0.081916        0.013073        0.018286
v  r22                   0.0011124         0.08264        0.013353        0.018646
v  r33                   0.0016371         0.17436        0.027249        0.037206
v  r12                   -0.010658        0.013581      -0.0002338     -0.00030931
v  r13                   -0.045544        0.052804       9.317e-05       0.0010138
v  r23                   -0.046689        0.051195      3.0428e-05      0.00057458
v  epsilon                0.069047          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9968e-05       0.0099178      0.00092489       0.0017427
v  CourantNb               0.44217             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2773         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8773         0.71351         0.85283


 TIME FOR THE TIME STEP            10536:        0.75925E+02

===============================================================


 INSTANT    0.105370000E-01   TIME STEP NUMBER           10537
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.245163440E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.627930807E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.641928908E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.189035597E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.379972385E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81261E-03   0.45110E-02 0.19863E+01 
c  Velocity[X]                                      0.13777E-03 
c  Velocity[Y]                                      0.12778E-03 
c  Velocity[Z]                                      0.42455E-02 
c  Pressure     0.36298E-04     132   0.92344E-02   0.25603E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.48613E-08   0.16311E-08 0.99619E-01 
c  r22          0.10852E-01      13   0.45930E-08   0.18223E-08 0.10143E+00 
c  r33          0.21860E-01      14   0.64418E-08   0.12444E-07 0.12731E+00 
c  r12          0.93861E-03      18   0.53039E-08   0.29647E-09 0.60355E+00 
c  r13          0.46675E-02      18   0.63175E-08   0.14774E-08 0.19951E+00 
c  r23          0.39976E-02      18   0.65524E-08   0.12547E-08 0.19804E+00 
c  epsilon      0.10969E+02      11   0.32861E-08   0.96977E-02 0.16427E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.83180E-02 0.43007E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61365       0.0052567       0.0015074
v  Velocity[Y]            -0.57372         0.54404       0.0030808      0.00087333
v  Velocity[Z]              1.5658          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4381          4.3406          4.3632
v  Pressure                -36.404          359.98          87.627          169.82
v  r11                   0.0010602        0.081922        0.013073        0.018286
v  r22                   0.0011124        0.082635        0.013353        0.018646
v  r33                   0.0016371         0.17434        0.027249        0.037206
v  r12                   -0.010658        0.013584      -0.0002338     -0.00030931
v  r13                   -0.045548        0.052805       9.317e-05       0.0010138
v  r23                   -0.046689        0.051184      3.0428e-05      0.00057458
v  epsilon                0.069048          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9969e-05       0.0099177      0.00092489       0.0017427
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2777         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8777          0.7135         0.85283


 TIME FOR THE TIME STEP            10537:        0.76802E+02

===============================================================


 INSTANT    0.105380000E-01   TIME STEP NUMBER           10538
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.151367252E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.172686411E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.349050667E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.236874365E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.271977230E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81238E-03   0.45252E-02 0.19929E+01 
c  Velocity[X]                                      0.13857E-03 
c  Velocity[Y]                                      0.12855E-03 
c  Velocity[Z]                                      0.42581E-02 
c  Pressure     0.36387E-04     131   0.92566E-02   0.25666E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.47766E-08   0.16460E-08 0.10008E+00 
c  r22          0.10852E-01      12   0.65680E-08   0.18603E-08 0.10202E+00 
c  r33          0.21860E-01      14   0.64828E-08   0.12705E-07 0.12816E+00 
c  r12          0.93861E-03      17   0.68118E-08   0.29394E-09 0.60389E+00 
c  r13          0.46675E-02      18   0.66677E-08   0.15293E-08 0.20164E+00 
c  r23          0.39976E-02      19   0.55365E-08   0.12938E-08 0.20009E+00 
c  epsilon      0.10969E+02      11   0.32908E-08   0.10181E-01 0.16893E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.84205E-02 0.43327E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63408         0.61361       0.0052568       0.0015074
v  Velocity[Y]            -0.57363         0.54418       0.0030807      0.00087329
v  Velocity[Z]              1.5656          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4381          4.3406          4.3632
v  Pressure                -36.418          359.94          87.605          169.79
v  r11                   0.0010602        0.081922        0.013073        0.018286
v  r22                   0.0011124        0.082636        0.013353        0.018646
v  r33                   0.0016372          0.1743        0.027249        0.037206
v  r12                   -0.010657         0.01358      -0.0002338     -0.00030931
v  r13                   -0.045545        0.052805       9.317e-05       0.0010138
v  r23                   -0.046689        0.051183      3.0428e-05      0.00057458
v  epsilon                0.069049          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9969e-05       0.0099177      0.00092489       0.0017427
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2784         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8784         0.71351         0.85283


 TIME FOR THE TIME STEP            10538:        0.79445E+02

===============================================================


 INSTANT    0.105390000E-01   TIME STEP NUMBER           10539
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.991488347E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.265691508E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.170122409E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.324133122E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.194519293E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81254E-03   0.45542E-02 0.19982E+01 
c  Velocity[X]                                      0.13859E-03 
c  Velocity[Y]                                      0.12848E-03 
c  Velocity[Z]                                      0.42871E-02 
c  Pressure     0.36318E-04     133   0.92474E-02   0.25618E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.48208E-08   0.16155E-08 0.99433E-01 
c  r22          0.10852E-01      13   0.45621E-08   0.18107E-08 0.10076E+00 
c  r33          0.21860E-01      15   0.63291E-08   0.12304E-07 0.12643E+00 
c  r12          0.93861E-03      18   0.54682E-08   0.29005E-09 0.60205E+00 
c  r13          0.46675E-02      19   0.56767E-08   0.14879E-08 0.19876E+00 
c  r23          0.39976E-02      19   0.60976E-08   0.12429E-08 0.19685E+00 
c  epsilon      0.10969E+02      11   0.34544E-08   0.96483E-02 0.16351E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.85204E-02 0.43508E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63402         0.61358       0.0052568       0.0015074
v  Velocity[Y]            -0.57364         0.54429       0.0030808      0.00087336
v  Velocity[Z]              1.5658          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4381          4.3406          4.3632
v  Pressure                -36.432          360.05          87.655          169.86
v  r11                   0.0010602        0.081931        0.013073        0.018286
v  r22                   0.0011125        0.082636        0.013353        0.018646
v  r33                   0.0016372         0.17431        0.027249        0.037206
v  r12                   -0.010657        0.013578      -0.0002338      -0.0003093
v  r13                   -0.045544        0.052802       9.317e-05       0.0010138
v  r23                   -0.046689        0.051207      3.0429e-05      0.00057458
v  epsilon                 0.06905          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9969e-05       0.0099176       0.0009249       0.0017427
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2783         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8783         0.71351         0.85283


 TIME FOR THE TIME STEP            10539:        0.80021E+02

===============================================================


 INSTANT    0.105400000E-01   TIME STEP NUMBER           10540
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.425315194E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.996723876E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.264571823E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.549062594E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138015386E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81302E-03   0.44869E-02 0.19828E+01 
c  Velocity[X]                                      0.13747E-03 
c  Velocity[Y]                                      0.12721E-03 
c  Velocity[Z]                                      0.42222E-02 
c  Pressure     0.36073E-04     133   0.91851E-02   0.25445E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52376E-08   0.16411E-08 0.99617E-01 
c  r22          0.10852E-01      13   0.46051E-08   0.18185E-08 0.10118E+00 
c  r33          0.21860E-01      15   0.55890E-08   0.12492E-07 0.12728E+00 
c  r12          0.93861E-03      18   0.53792E-08   0.29464E-09 0.60230E+00 
c  r13          0.46675E-02      18   0.73016E-08   0.14839E-08 0.19939E+00 
c  r23          0.39976E-02      19   0.65718E-08   0.12810E-08 0.19906E+00 
c  epsilon      0.10969E+02      11   0.32316E-08   0.97833E-02 0.16439E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.83674E-02 0.43183E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63403         0.61363       0.0052568       0.0015074
v  Velocity[Y]            -0.57362         0.54409       0.0030808      0.00087334
v  Velocity[Z]              1.5656          5.4381          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4381          4.3406          4.3632
v  Pressure                -36.427          360.15          87.723          169.95
v  r11                   0.0010602         0.08193        0.013073        0.018286
v  r22                   0.0011125        0.082636        0.013353        0.018646
v  r33                   0.0016372         0.17433        0.027249        0.037206
v  r12                   -0.010658        0.013578      -0.0002338     -0.00030931
v  r13                   -0.045547        0.052801       9.317e-05       0.0010138
v  r23                   -0.046689        0.051202      3.0429e-05      0.00057457
v  epsilon                0.069051          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9966e-05       0.0099175       0.0009249       0.0017427
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2784         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8784          0.7135         0.85283


 TIME FOR THE TIME STEP            10540:        0.80667E+02

===============================================================


 INSTANT    0.105410000E-01   TIME STEP NUMBER           10541
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.841801132E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.228115846E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.121964443E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.202784034E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150185400E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81204E-03   0.45342E-02 0.19948E+01 
c  Velocity[X]                                      0.13828E-03 
c  Velocity[Y]                                      0.12922E-03 
c  Velocity[Z]                                      0.42667E-02 
c  Pressure     0.36717E-04     133   0.93470E-02   0.25899E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53490E-08   0.16662E-08 0.10044E+00 
c  r22          0.10852E-01      13   0.47722E-08   0.18549E-08 0.10191E+00 
c  r33          0.21860E-01      14   0.70130E-08   0.12862E-07 0.12863E+00 
c  r12          0.93861E-03      18   0.53944E-08   0.29743E-09 0.60755E+00 
c  r13          0.46675E-02      18   0.63317E-08   0.15203E-08 0.20043E+00 
c  r23          0.39976E-02      19   0.52404E-08   0.13148E-08 0.20136E+00 
c  epsilon      0.10969E+02      11   0.31080E-08   0.10463E-01 0.17262E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84330E-02 0.43348E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61359       0.0052568       0.0015074
v  Velocity[Y]            -0.57369         0.54418       0.0030808      0.00087331
v  Velocity[Z]              1.5657          5.4382          4.3388          4.3625
v  ǁVelocityǁ               1.5795          5.4382          4.3406          4.3632
v  Pressure                -36.419          360.04          87.663          169.87
v  r11                   0.0010602        0.081934        0.013073        0.018286
v  r22                   0.0011125        0.082635        0.013353        0.018646
v  r33                   0.0016372         0.17431        0.027249        0.037206
v  r12                   -0.010661        0.013578      -0.0002338      -0.0003093
v  r13                   -0.045546        0.052802      9.3171e-05       0.0010138
v  r23                    -0.04669        0.051185      3.0429e-05      0.00057457
v  epsilon                0.069052          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9965e-05       0.0099174       0.0009249       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2778         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8778         0.71351         0.85283


 TIME FOR THE TIME STEP            10541:        0.83423E+02

===============================================================


 INSTANT    0.105420000E-01   TIME STEP NUMBER           10542
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.349855795E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.304016475E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.372519822E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.971773671E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.274553724E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81217E-03   0.45335E-02 0.19946E+01 
c  Velocity[X]                                      0.13885E-03 
c  Velocity[Y]                                      0.12952E-03 
c  Velocity[Z]                                      0.42651E-02 
c  Pressure     0.36420E-04     133   0.92734E-02   0.25689E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53101E-08   0.16471E-08 0.99846E-01 
c  r22          0.10852E-01      13   0.49391E-08   0.18500E-08 0.10152E+00 
c  r33          0.21860E-01      15   0.56211E-08   0.12611E-07 0.12749E+00 
c  r12          0.93861E-03      18   0.60444E-08   0.30162E-09 0.60652E+00 
c  r13          0.46675E-02      18   0.69857E-08   0.14933E-08 0.19933E+00 
c  r23          0.39976E-02      19   0.56567E-08   0.12835E-08 0.19940E+00 
c  epsilon      0.10969E+02      11   0.32090E-08   0.98120E-02 0.16438E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84467E-02 0.43326E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61355       0.0052567       0.0015074
v  Velocity[Y]            -0.57363         0.54419       0.0030808      0.00087332
v  Velocity[Z]              1.5658          5.4382          4.3388          4.3625
v  ǁVelocityǁ               1.5796          5.4382          4.3406          4.3632
v  Pressure                -36.473          359.96          87.613           169.8
v  r11                   0.0010602        0.081936        0.013073        0.018286
v  r22                   0.0011125        0.082637        0.013353        0.018646
v  r33                   0.0016372         0.17429        0.027249        0.037206
v  r12                    -0.01066        0.013584      -0.0002338      -0.0003093
v  r13                   -0.045544        0.052805      9.3171e-05       0.0010138
v  r23                   -0.046691         0.05121       3.043e-05      0.00057457
v  epsilon                0.069053          271.18          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9962e-05       0.0099175       0.0009249       0.0017427
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2772         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8772          0.7135         0.85283


 TIME FOR THE TIME STEP            10542:        0.77714E+02

===============================================================


 INSTANT    0.105430000E-01   TIME STEP NUMBER           10543
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168868391E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.393499339E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.977134377E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.109685343E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110373409E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81301E-03   0.45175E-02 0.19902E+01 
c  Velocity[X]                                      0.13866E-03 
c  Velocity[Y]                                      0.12778E-03 
c  Velocity[Z]                                      0.42510E-02 
c  Pressure     0.36140E-04     132   0.92018E-02   0.25491E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50417E-08   0.16533E-08 0.99902E-01 
c  r22          0.10852E-01      13   0.50756E-08   0.18582E-08 0.10188E+00 
c  r33          0.21860E-01      14   0.71281E-08   0.12635E-07 0.12773E+00 
c  r12          0.93861E-03      18   0.53946E-08   0.30522E-09 0.61117E+00 
c  r13          0.46675E-02      18   0.71565E-08   0.14991E-08 0.20024E+00 
c  r23          0.39976E-02      19   0.59347E-08   0.12899E-08 0.19976E+00 
c  epsilon      0.10969E+02      11   0.31748E-08   0.97081E-02 0.16402E+00 
c  TempC        0.25716E+06      16   0.15103E-04   0.83593E-02 0.43127E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61359       0.0052567       0.0015074
v  Velocity[Y]            -0.57367         0.54424       0.0030807      0.00087333
v  Velocity[Z]              1.5654          5.4382          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4382          4.3406          4.3632
v  Pressure                -36.397          359.99          87.612          169.82
v  r11                   0.0010602        0.081944        0.013073        0.018286
v  r22                   0.0011125        0.082632        0.013353        0.018646
v  r33                   0.0016373          0.1743         0.02725        0.037206
v  r12                   -0.010662        0.013581      -0.0002338      -0.0003093
v  r13                   -0.045546        0.052804      9.3171e-05       0.0010138
v  r23                   -0.046691        0.051203       3.043e-05      0.00057457
v  epsilon                0.069054          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099175       0.0009249       0.0017427
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2774         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8774         0.71351         0.85283


 TIME FOR THE TIME STEP            10543:        0.74507E+02

===============================================================


 INSTANT    0.105440000E-01   TIME STEP NUMBER           10544
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.433530146E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.464724008E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.920995832E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.246732863E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.114257615E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81244E-03   0.45256E-02 0.19929E+01 
c  Velocity[X]                                      0.13802E-03 
c  Velocity[Y]                                      0.12829E-03 
c  Velocity[Z]                                      0.42593E-02 
c  Pressure     0.36560E-04     133   0.93026E-02   0.25788E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55701E-08   0.16701E-08 0.10042E+00 
c  r22          0.10852E-01      13   0.51225E-08   0.18562E-08 0.10189E+00 
c  r33          0.21860E-01      15   0.57080E-08   0.12801E-07 0.12853E+00 
c  r12          0.93861E-03      18   0.53082E-08   0.30028E-09 0.60911E+00 
c  r13          0.46675E-02      19   0.56515E-08   0.15163E-08 0.20075E+00 
c  r23          0.39976E-02      19   0.58155E-08   0.13063E-08 0.20067E+00 
c  epsilon      0.10969E+02      11   0.33536E-08   0.99138E-02 0.16566E+00 
c  TempC        0.25716E+06      16   0.15187E-04   0.84468E-02 0.43347E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61357       0.0052568       0.0015074
v  Velocity[Y]            -0.57345         0.54434       0.0030807      0.00087334
v  Velocity[Z]              1.5655          5.4382          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4382          4.3406          4.3632
v  Pressure                -36.455          359.98          87.633          169.82
v  r11                   0.0010602        0.081941        0.013073        0.018286
v  r22                   0.0011125        0.082632        0.013353        0.018646
v  r33                   0.0016373         0.17432         0.02725        0.037206
v  r12                   -0.010663        0.013582      -0.0002338      -0.0003093
v  r13                   -0.045544        0.052804      9.3171e-05       0.0010138
v  r23                   -0.046691        0.051199      3.0432e-05      0.00057457
v  epsilon                0.069055          271.21          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9956e-05       0.0099174       0.0009249       0.0017427
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2777         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8777          0.7135         0.85283


 TIME FOR THE TIME STEP            10544:        0.77315E+02

===============================================================


 INSTANT    0.105450000E-01   TIME STEP NUMBER           10545
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.134570096E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.649840749E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.738865943E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.475706280E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.214372673E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81177E-03   0.45287E-02 0.19922E+01 
c  Velocity[X]                                      0.13873E-03 
c  Velocity[Y]                                      0.12862E-03 
c  Velocity[Z]                                      0.42613E-02 
c  Pressure     0.36246E-04     133   0.92267E-02   0.25567E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57714E-08   0.16339E-08 0.99752E-01 
c  r22          0.10852E-01      13   0.57130E-08   0.18344E-08 0.10165E+00 
c  r33          0.21860E-01      15   0.53164E-08   0.12447E-07 0.12708E+00 
c  r12          0.93861E-03      18   0.61336E-08   0.29690E-09 0.60472E+00 
c  r13          0.46675E-02      18   0.72667E-08   0.14778E-08 0.19942E+00 
c  r23          0.39976E-02      19   0.55046E-08   0.12479E-08 0.19697E+00 
c  epsilon      0.10969E+02      11   0.33879E-08   0.97909E-02 0.16541E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.83981E-02 0.43262E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63395         0.61355       0.0052568       0.0015074
v  Velocity[Y]            -0.57366          0.5441       0.0030808      0.00087339
v  Velocity[Z]              1.5654          5.4382          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4382          4.3406          4.3632
v  Pressure                -36.442          360.06          87.667          169.88
v  r11                   0.0010602        0.081941        0.013073        0.018286
v  r22                   0.0011125        0.082634        0.013353        0.018646
v  r33                   0.0016373         0.17435         0.02725        0.037206
v  r12                   -0.010663        0.013589      -0.0002338      -0.0003093
v  r13                   -0.045545        0.052803      9.3171e-05       0.0010138
v  r23                   -0.046691        0.051212      3.0432e-05      0.00057458
v  epsilon                0.069056          271.23          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9954e-05       0.0099173       0.0009249       0.0017427
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017847           5.278         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.878         0.71351         0.85284


 TIME FOR THE TIME STEP            10545:        0.76607E+02

===============================================================


 INSTANT    0.105460000E-01   TIME STEP NUMBER           10546
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178272529E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.366559415E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.374013623E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.937421647E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.876739322E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81392E-03   0.45049E-02 0.19875E+01 
c  Velocity[X]                                      0.13805E-03 
c  Velocity[Y]                                      0.12926E-03 
c  Velocity[Z]                                      0.42376E-02 
c  Pressure     0.36059E-04     133   0.91781E-02   0.25434E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49628E-08   0.16756E-08 0.10039E+00 
c  r22          0.10852E-01      13   0.54994E-08   0.18138E-08 0.10136E+00 
c  r33          0.21860E-01      14   0.67196E-08   0.12707E-07 0.12824E+00 
c  r12          0.93861E-03      18   0.66184E-08   0.29741E-09 0.60555E+00 
c  r13          0.46675E-02      19   0.53936E-08   0.14754E-08 0.19939E+00 
c  r23          0.39976E-02      19   0.56999E-08   0.13302E-08 0.20277E+00 
c  epsilon      0.10969E+02      11   0.32685E-08   0.10099E-01 0.17036E+00 
c  TempC        0.25716E+06      16   0.15191E-04   0.83879E-02 0.43232E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63396         0.61357       0.0052568       0.0015074
v  Velocity[Y]            -0.57362         0.54418       0.0030807      0.00087331
v  Velocity[Z]              1.5654          5.4382          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4382          4.3406          4.3632
v  Pressure                -36.461             360          87.638          169.84
v  r11                   0.0010602        0.081937        0.013073        0.018286
v  r22                   0.0011125        0.082635        0.013353        0.018646
v  r33                   0.0016373         0.17433         0.02725        0.037206
v  r12                   -0.010664        0.013591      -0.0002338      -0.0003093
v  r13                   -0.045547        0.052804      9.3171e-05       0.0010138
v  r23                   -0.046691        0.051198      3.0432e-05      0.00057457
v  epsilon                0.069057          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9954e-05       0.0099173       0.0009249       0.0017427
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2778         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8778         0.71351         0.85284


 TIME FOR THE TIME STEP            10546:        0.75183E+02

===============================================================


 INSTANT    0.105470000E-01   TIME STEP NUMBER           10547
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.549581094E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.124510687E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199807064E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.268899477E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.583335312E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81118E-03   0.45128E-02 0.19919E+01 
c  Velocity[X]                                      0.13792E-03 
c  Velocity[Y]                                      0.12795E-03 
c  Velocity[Z]                                      0.42469E-02 
c  Pressure     0.36264E-04     133   0.92350E-02   0.25578E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52982E-08   0.16500E-08 0.99391E-01 
c  r22          0.10852E-01      13   0.51525E-08   0.18630E-08 0.10153E+00 
c  r33          0.21860E-01      15   0.54546E-08   0.12800E-07 0.12757E+00 
c  r12          0.93861E-03      18   0.52076E-08   0.29986E-09 0.60429E+00 
c  r13          0.46675E-02      19   0.58510E-08   0.15360E-08 0.20110E+00 
c  r23          0.39976E-02      19   0.59048E-08   0.13033E-08 0.19940E+00 
c  epsilon      0.10969E+02      11   0.32025E-08   0.10377E-01 0.16752E+00 
c  TempC        0.25716E+06      16   0.15104E-04   0.84319E-02 0.43317E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63399         0.61353       0.0052568       0.0015074
v  Velocity[Y]            -0.57367         0.54434       0.0030808      0.00087334
v  Velocity[Z]              1.5654          5.4382          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4382          4.3406          4.3632
v  Pressure                -36.408          360.01          87.639          169.84
v  r11                   0.0010602         0.08192        0.013073        0.018286
v  r22                   0.0011125        0.082635        0.013353        0.018646
v  r33                   0.0016373         0.17429         0.02725        0.037206
v  r12                   -0.010668        0.013594      -0.0002338      -0.0003093
v  r13                   -0.045544        0.052802      9.3171e-05       0.0010138
v  r23                   -0.046691        0.051185      3.0432e-05      0.00057457
v  epsilon                0.069058          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9954e-05       0.0099175       0.0009249       0.0017427
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2777         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8777          0.7135         0.85283


 TIME FOR THE TIME STEP            10547:        0.78061E+02

===============================================================


 INSTANT    0.105480000E-01   TIME STEP NUMBER           10548
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.487973854E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.958457974E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.380079258E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.128387567E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.102730799E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81265E-03   0.45147E-02 0.19880E+01 
c  Velocity[X]                                      0.13865E-03 
c  Velocity[Y]                                      0.12741E-03 
c  Velocity[Z]                                      0.42486E-02 
c  Pressure     0.36547E-04     131   0.93057E-02   0.25779E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58432E-08   0.16408E-08 0.99509E-01 
c  r22          0.10852E-01      13   0.52582E-08   0.18406E-08 0.10149E+00 
c  r33          0.21860E-01      14   0.70226E-08   0.12637E-07 0.12760E+00 
c  r12          0.93861E-03      18   0.50875E-08   0.29525E-09 0.60231E+00 
c  r13          0.46675E-02      19   0.57188E-08   0.15148E-08 0.20078E+00 
c  r23          0.39976E-02      19   0.63926E-08   0.12893E-08 0.19914E+00 
c  epsilon      0.10969E+02      11   0.32064E-08   0.10191E-01 0.16736E+00 
c  TempC        0.25716E+06      16   0.15173E-04   0.84866E-02 0.43455E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398          0.6135       0.0052568       0.0015074
v  Velocity[Y]            -0.57363         0.54414       0.0030808      0.00087334
v  Velocity[Z]              1.5652          5.4382          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4382          4.3406          4.3632
v  Pressure                -36.453          360.02          87.646          169.85
v  r11                   0.0010602        0.081909        0.013073        0.018286
v  r22                   0.0011126        0.082637        0.013353        0.018646
v  r33                   0.0016373         0.17431         0.02725        0.037206
v  r12                   -0.010669        0.013594      -0.0002338      -0.0003093
v  r13                   -0.045543        0.052803      9.3172e-05       0.0010138
v  r23                   -0.046691        0.051204      3.0433e-05      0.00057457
v  epsilon                0.069059          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9954e-05       0.0099175       0.0009249       0.0017427
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2776         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8776          0.7135         0.85283


 TIME FOR THE TIME STEP            10548:        0.77139E+02

===============================================================


 INSTANT    0.105490000E-01   TIME STEP NUMBER           10549
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.585630186E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105045819E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.167318882E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.135426029E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140857418E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81258E-03   0.44944E-02 0.19855E+01 
c  Velocity[X]                                      0.13817E-03 
c  Velocity[Y]                                      0.12771E-03 
c  Velocity[Z]                                      0.42285E-02 
c  Pressure     0.36599E-04     133   0.93069E-02   0.25815E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61793E-08   0.16522E-08 0.10014E+00 
c  r22          0.10852E-01      13   0.51449E-08   0.18754E-08 0.10210E+00 
c  r33          0.21860E-01      15   0.57180E-08   0.12707E-07 0.12790E+00 
c  r12          0.93861E-03      18   0.49247E-08   0.30473E-09 0.61050E+00 
c  r13          0.46675E-02      19   0.63412E-08   0.15115E-08 0.20064E+00 
c  r23          0.39976E-02      19   0.62704E-08   0.12735E-08 0.19909E+00 
c  epsilon      0.10969E+02      11   0.33667E-08   0.10145E-01 0.16665E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.84073E-02 0.43285E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61354       0.0052568       0.0015075
v  Velocity[Y]            -0.57386         0.54423       0.0030808      0.00087335
v  Velocity[Z]              1.5653          5.4382          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4382          4.3406          4.3632
v  Pressure                -36.413             360          87.633          169.84
v  r11                   0.0010602        0.081899        0.013073        0.018286
v  r22                   0.0011126        0.082634        0.013353        0.018646
v  r33                   0.0016374         0.17433         0.02725        0.037206
v  r12                    -0.01067        0.013595      -0.0002338      -0.0003093
v  r13                   -0.045547        0.052805      9.3171e-05       0.0010138
v  r23                   -0.046691        0.051199      3.0433e-05      0.00057457
v  epsilon                 0.06906          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9955e-05       0.0099174      0.00092491       0.0017427
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2773         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8773          0.7135         0.85283


 TIME FOR THE TIME STEP            10549:        0.72060E+02

===============================================================


 INSTANT    0.105500000E-01   TIME STEP NUMBER           10550
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183663922E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.336592610E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182645072E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935012E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.534268532E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.126355343E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81133E-03   0.45407E-02 0.19968E+01 
c  Velocity[X]                                      0.13878E-03 
c  Velocity[Y]                                      0.12938E-03 
c  Velocity[Z]                                      0.42725E-02 
c  Pressure     0.36420E-04     133   0.92745E-02   0.25690E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.65249E-08   0.16400E-08 0.99665E-01 
c  r22          0.10852E-01      13   0.51255E-08   0.18264E-08 0.10141E+00 
c  r33          0.21860E-01      15   0.67108E-08   0.12516E-07 0.12731E+00 
c  r12          0.93861E-03      18   0.49015E-08   0.29412E-09 0.60347E+00 
c  r13          0.46675E-02      19   0.66673E-08   0.14864E-08 0.19953E+00 
c  r23          0.39976E-02      19   0.59248E-08   0.12765E-08 0.19869E+00 
c  epsilon      0.10969E+02      11   0.34943E-08   0.98533E-02 0.16472E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83571E-02 0.43149E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61354       0.0052568       0.0015074
v  Velocity[Y]            -0.57383          0.5444       0.0030807      0.00087332
v  Velocity[Z]              1.5652          5.4382          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4382          4.3406          4.3632
v  Pressure                -36.448          359.96          87.625           169.8
v  r11                   0.0010602        0.081899        0.013073        0.018286
v  r22                   0.0011126        0.082637        0.013353        0.018646
v  r33                   0.0016374         0.17431         0.02725        0.037206
v  r12                   -0.010669        0.013592      -0.0002338      -0.0003093
v  r13                   -0.045544        0.052807      9.3172e-05       0.0010138
v  r23                   -0.046691        0.051186      3.0435e-05      0.00057458
v  epsilon                0.069061          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9955e-05       0.0099175      0.00092491       0.0017427
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2774         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8774         0.71351         0.85283


 TIME FOR THE TIME STEP            10550:        0.76208E+02

===============================================================


 INSTANT    0.105510000E-01   TIME STEP NUMBER           10551
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.644611416E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249257349E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.281423849E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.718463552E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117740620E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81353E-03   0.45435E-02 0.19956E+01 
c  Velocity[X]                                      0.13933E-03 
c  Velocity[Y]                                      0.12799E-03 
c  Velocity[Z]                                      0.42762E-02 
c  Pressure     0.36404E-04     132   0.92740E-02   0.25679E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.64044E-08   0.16294E-08 0.99365E-01 
c  r22          0.10852E-01      13   0.51418E-08   0.18172E-08 0.10141E+00 
c  r33          0.21860E-01      15   0.52932E-08   0.12400E-07 0.12715E+00 
c  r12          0.93861E-03      17   0.68523E-08   0.29565E-09 0.60339E+00 
c  r13          0.46675E-02      19   0.69040E-08   0.14804E-08 0.19925E+00 
c  r23          0.39976E-02      19   0.56248E-08   0.12703E-08 0.19912E+00 
c  epsilon      0.10969E+02      11   0.32157E-08   0.93641E-02 0.16059E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.84252E-02 0.43296E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379         0.61354       0.0052569       0.0015074
v  Velocity[Y]            -0.57389         0.54413       0.0030808      0.00087336
v  Velocity[Z]              1.5653          5.4382          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4382          4.3406          4.3632
v  Pressure                -36.406          360.07          87.661          169.88
v  r11                   0.0010602        0.081891        0.013073        0.018286
v  r22                   0.0011126        0.082639        0.013353        0.018646
v  r33                   0.0016374         0.17428         0.02725        0.037206
v  r12                   -0.010664        0.013589      -0.0002338      -0.0003093
v  r13                   -0.045543        0.052804      9.3172e-05       0.0010138
v  r23                   -0.046691         0.05118      3.0435e-05      0.00057458
v  epsilon                0.069062          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9957e-05       0.0099176      0.00092491       0.0017427
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2785         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8785         0.71351         0.85284


 TIME FOR THE TIME STEP            10551:        0.77494E+02

===============================================================


 INSTANT    0.105520000E-01   TIME STEP NUMBER           10552
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.482521912E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.259764490E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.252732163E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.194594499E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.572703855E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81303E-03   0.45057E-02 0.19884E+01 
c  Velocity[X]                                      0.13742E-03 
c  Velocity[Y]                                      0.12821E-03 
c  Velocity[Z]                                      0.42401E-02 
c  Pressure     0.36478E-04     133   0.92922E-02   0.25730E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58466E-08   0.16530E-08 0.99759E-01 
c  r22          0.10852E-01      13   0.54026E-08   0.18383E-08 0.10147E+00 
c  r33          0.21860E-01      15   0.61608E-08   0.12692E-07 0.12791E+00 
c  r12          0.93861E-03      18   0.53540E-08   0.29554E-09 0.60424E+00 
c  r13          0.46675E-02      19   0.70776E-08   0.15141E-08 0.20074E+00 
c  r23          0.39976E-02      19   0.59814E-08   0.13024E-08 0.20069E+00 
c  epsilon      0.10969E+02      11   0.32278E-08   0.10407E-01 0.17204E+00 
c  TempC        0.25716E+06      16   0.15175E-04   0.84126E-02 0.43259E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61357       0.0052568       0.0015075
v  Velocity[Y]            -0.57393         0.54411       0.0030808      0.00087333
v  Velocity[Z]              1.5654          5.4382          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4382          4.3406          4.3632
v  Pressure                -36.467          360.01          87.632          169.84
v  r11                   0.0010602        0.081888        0.013073        0.018286
v  r22                   0.0011126        0.082641        0.013353        0.018646
v  r33                   0.0016374         0.17429         0.02725        0.037206
v  r12                   -0.010664        0.013591      -0.0002338      -0.0003093
v  r13                   -0.045545        0.052803      9.3172e-05       0.0010138
v  r23                   -0.046692        0.051213      3.0436e-05      0.00057458
v  epsilon                0.069063          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9958e-05       0.0099176      0.00092491       0.0017427
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2785         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8785         0.71351         0.85284


 TIME FOR THE TIME STEP            10552:        0.75047E+02

===============================================================


 INSTANT    0.105530000E-01   TIME STEP NUMBER           10553
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.838351047E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.277107110E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934912E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.114445913E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.810871074E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.270035741E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81151E-03   0.45143E-02 0.19901E+01 
c  Velocity[X]                                      0.13826E-03 
c  Velocity[Y]                                      0.12923E-03 
c  Velocity[Z]                                      0.42468E-02 
c  Pressure     0.36386E-04     132   0.92609E-02   0.25665E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55700E-08   0.16616E-08 0.99910E-01 
c  r22          0.10852E-01      13   0.50105E-08   0.18367E-08 0.10163E+00 
c  r33          0.21860E-01      15   0.71378E-08   0.12608E-07 0.12755E+00 
c  r12          0.93861E-03      18   0.49266E-08   0.30242E-09 0.60927E+00 
c  r13          0.46675E-02      20   0.59854E-08   0.15080E-08 0.20044E+00 
c  r23          0.39976E-02      19   0.62166E-08   0.12971E-08 0.19974E+00 
c  epsilon      0.10969E+02      11   0.33430E-08   0.99463E-02 0.16529E+00 
c  TempC        0.25716E+06      16   0.15122E-04   0.84273E-02 0.43309E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63395         0.61358       0.0052568       0.0015074
v  Velocity[Y]            -0.57408          0.5442       0.0030808      0.00087331
v  Velocity[Z]              1.5652          5.4382          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4382          4.3406          4.3632
v  Pressure                -36.418          360.06          87.667          169.88
v  r11                   0.0010603        0.081881        0.013073        0.018286
v  r22                   0.0011126        0.082641        0.013353        0.018646
v  r33                   0.0016374         0.17432         0.02725        0.037206
v  r12                   -0.010661        0.013588      -0.0002338      -0.0003093
v  r13                   -0.045544        0.052803      9.3173e-05       0.0010138
v  r23                   -0.046691        0.051211      3.0437e-05      0.00057458
v  epsilon                0.069064          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.996e-05       0.0099176      0.00092491       0.0017427
v  CourantNb               0.44218             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2781         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781         0.71351         0.85284


 TIME FOR THE TIME STEP            10553:        0.76726E+02

===============================================================


 INSTANT    0.105540000E-01   TIME STEP NUMBER           10554
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.279809030E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.280596254E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.142268994E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.124837772E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.279606467E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69753E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81274E-03   0.45286E-02 0.19921E+01 
c  Velocity[X]                                      0.13841E-03 
c  Velocity[Y]                                      0.12914E-03 
c  Velocity[Z]                                      0.42610E-02 
c  Pressure     0.36094E-04     131   0.91866E-02   0.25459E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53591E-08   0.16274E-08 0.99087E-01 
c  r22          0.10852E-01      13   0.49174E-08   0.18000E-08 0.10070E+00 
c  r33          0.21860E-01      15   0.59955E-08   0.12355E-07 0.12654E+00 
c  r12          0.93861E-03      18   0.54260E-08   0.29043E-09 0.60167E+00 
c  r13          0.46675E-02      19   0.71123E-08   0.14810E-08 0.19936E+00 
c  r23          0.39976E-02      19   0.66559E-08   0.12700E-08 0.19786E+00 
c  epsilon      0.10969E+02      11   0.34170E-08   0.95148E-02 0.16064E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.84608E-02 0.43370E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61354       0.0052569       0.0015074
v  Velocity[Y]            -0.57397         0.54434       0.0030807      0.00087327
v  Velocity[Z]              1.5652          5.4382          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4382          4.3406          4.3632
v  Pressure                -36.422          360.02          87.651          169.85
v  r11                   0.0010603        0.081869        0.013073        0.018286
v  r22                   0.0011126        0.082644        0.013353        0.018646
v  r33                   0.0016375         0.17435         0.02725        0.037206
v  r12                    -0.01066        0.013583      -0.0002338      -0.0003093
v  r13                   -0.045542        0.052807      9.3173e-05       0.0010138
v  r23                   -0.046691        0.051203      3.0438e-05      0.00057458
v  epsilon                0.069065          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9961e-05       0.0099176      0.00092491       0.0017427
v  CourantNb               0.44217             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2783         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8783          0.7135         0.85283


 TIME FOR THE TIME STEP            10554:        0.76350E+02

===============================================================


 INSTANT    0.105550000E-01   TIME STEP NUMBER           10555
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.266992416E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.202353027E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.398023835E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935012E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.167766919E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.299066306E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81232E-03   0.45335E-02 0.19904E+01 
c  Velocity[X]                                      0.13847E-03 
c  Velocity[Y]                                      0.12770E-03 
c  Velocity[Z]                                      0.42674E-02 
c  Pressure     0.36224E-04     132   0.92265E-02   0.25551E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54020E-08   0.16292E-08 0.99440E-01 
c  r22          0.10852E-01      13   0.47044E-08   0.18213E-08 0.10100E+00 
c  r33          0.21860E-01      15   0.64285E-08   0.12550E-07 0.12708E+00 
c  r12          0.93861E-03      18   0.55950E-08   0.30052E-09 0.60836E+00 
c  r13          0.46675E-02      19   0.71585E-08   0.15000E-08 0.19922E+00 
c  r23          0.39976E-02      19   0.71844E-08   0.12869E-08 0.19923E+00 
c  epsilon      0.10969E+02      11   0.34892E-08   0.99948E-02 0.16561E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.84097E-02 0.43241E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61362       0.0052568       0.0015074
v  Velocity[Y]            -0.57401         0.54401       0.0030808      0.00087332
v  Velocity[Z]              1.5655          5.4382          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4382          4.3406          4.3632
v  Pressure                -36.398          359.99          87.626          169.82
v  r11                   0.0010603        0.081865        0.013073        0.018286
v  r22                   0.0011126         0.08264        0.013353        0.018646
v  r33                   0.0016375         0.17434         0.02725        0.037206
v  r12                   -0.010665        0.013581      -0.0002338      -0.0003093
v  r13                   -0.045545        0.052806      9.3173e-05       0.0010138
v  r23                   -0.046691         0.05123      3.0439e-05      0.00057458
v  epsilon                0.069066          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9963e-05       0.0099176      0.00092491       0.0017427
v  CourantNb               0.44219             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2786         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8786         0.71351         0.85283


 TIME FOR THE TIME STEP            10555:        0.75221E+02

===============================================================


 INSTANT    0.105560000E-01   TIME STEP NUMBER           10556
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.271257415E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.904772376E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.215982470E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181493001E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.211768148E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81271E-03   0.45084E-02 0.19915E+01 
c  Velocity[X]                                      0.13741E-03 
c  Velocity[Y]                                      0.12796E-03 
c  Velocity[Z]                                      0.42430E-02 
c  Pressure     0.36662E-04     133   0.93337E-02   0.25859E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52863E-08   0.16347E-08 0.99525E-01 
c  r22          0.10852E-01      13   0.48975E-08   0.18190E-08 0.10126E+00 
c  r33          0.21860E-01      15   0.56838E-08   0.12495E-07 0.12725E+00 
c  r12          0.93861E-03      18   0.54408E-08   0.28980E-09 0.60136E+00 
c  r13          0.46675E-02      19   0.61585E-08   0.15051E-08 0.20033E+00 
c  r23          0.39976E-02      19   0.64714E-08   0.12860E-08 0.19885E+00 
c  epsilon      0.10969E+02      11   0.33329E-08   0.99842E-02 0.16728E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.83706E-02 0.43210E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383         0.61357       0.0052568       0.0015074
v  Velocity[Y]            -0.57388         0.54391       0.0030806      0.00087326
v  Velocity[Z]              1.5653          5.4382          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4382          4.3406          4.3632
v  Pressure                 -36.44          360.06           87.69          169.89
v  r11                   0.0010603        0.081884        0.013073        0.018286
v  r22                   0.0011126         0.08264        0.013353        0.018646
v  r33                   0.0016375          0.1743         0.02725        0.037206
v  r12                   -0.010664         0.01358      -0.0002338      -0.0003093
v  r13                   -0.045542        0.052807      9.3173e-05       0.0010138
v  r23                   -0.046691        0.051212      3.0439e-05      0.00057458
v  epsilon                0.069067          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.996e-05       0.0099176      0.00092491       0.0017427
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2784         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8784          0.7135         0.85283


 TIME FOR THE TIME STEP            10556:        0.76517E+02

===============================================================


 INSTANT    0.105570000E-01   TIME STEP NUMBER           10557
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.258039473E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239390866E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.265284539E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.759224675E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.210629195E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81232E-03   0.45358E-02 0.19959E+01 
c  Velocity[X]                                      0.13876E-03 
c  Velocity[Y]                                      0.12885E-03 
c  Velocity[Z]                                      0.42682E-02 
c  Pressure     0.36457E-04     132   0.92826E-02   0.25715E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51062E-08   0.16497E-08 0.99759E-01 
c  r22          0.10852E-01      13   0.47612E-08   0.18052E-08 0.10055E+00 
c  r33          0.21860E-01      14   0.70798E-08   0.12490E-07 0.12697E+00 
c  r12          0.93861E-03      18   0.56432E-08   0.28936E-09 0.60210E+00 
c  r13          0.46675E-02      19   0.67652E-08   0.14971E-08 0.19894E+00 
c  r23          0.39976E-02      19   0.71098E-08   0.12858E-08 0.19917E+00 
c  epsilon      0.10969E+02      11   0.33393E-08   0.10153E-01 0.16980E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.84517E-02 0.43388E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61357       0.0052568       0.0015074
v  Velocity[Y]            -0.57397         0.54396       0.0030808      0.00087332
v  Velocity[Z]              1.5655          5.4382          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4382          4.3406          4.3632
v  Pressure                -36.412          360.02          87.649          169.85
v  r11                   0.0010603        0.081897        0.013073        0.018286
v  r22                   0.0011126        0.082641        0.013353        0.018646
v  r33                   0.0016375         0.17431         0.02725        0.037206
v  r12                   -0.010664         0.01359      -0.0002338      -0.0003093
v  r13                   -0.045543        0.052804      9.3173e-05       0.0010138
v  r23                   -0.046691        0.051194       3.044e-05      0.00057458
v  epsilon                0.069068          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099175      0.00092491       0.0017427
v  CourantNb               0.44211             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2787         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8787         0.71351         0.85284


 TIME FOR THE TIME STEP            10557:        0.76327E+02

===============================================================


 INSTANT    0.105580000E-01   TIME STEP NUMBER           10558
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.202993322E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.115152702E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203179521E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138696879E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.174369553E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81266E-03   0.45169E-02 0.19893E+01 
c  Velocity[X]                                      0.13814E-03 
c  Velocity[Y]                                      0.12864E-03 
c  Velocity[Z]                                      0.42502E-02 
c  Pressure     0.36310E-04     132   0.92440E-02   0.25611E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53812E-08   0.16546E-08 0.99888E-01 
c  r22          0.10852E-01      13   0.51037E-08   0.18279E-08 0.10149E+00 
c  r33          0.21860E-01      15   0.58644E-08   0.12579E-07 0.12785E+00 
c  r12          0.93861E-03      18   0.52396E-08   0.30679E-09 0.61101E+00 
c  r13          0.46675E-02      19   0.58376E-08   0.15006E-08 0.20012E+00 
c  r23          0.39976E-02      19   0.70478E-08   0.13072E-08 0.20062E+00 
c  epsilon      0.10969E+02      11   0.34097E-08   0.98743E-02 0.16536E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.83512E-02 0.43103E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61359       0.0052568       0.0015074
v  Velocity[Y]            -0.57397          0.5441       0.0030807      0.00087326
v  Velocity[Z]              1.5651          5.4382          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4382          4.3406          4.3632
v  Pressure                -36.461          360.01          87.623          169.83
v  r11                   0.0010603          0.0819        0.013073        0.018286
v  r22                   0.0011127        0.082643        0.013353        0.018646
v  r33                   0.0016375         0.17433         0.02725        0.037206
v  r12                   -0.010663         0.01359      -0.0002338      -0.0003093
v  r13                   -0.045545        0.052806      9.3174e-05       0.0010138
v  r23                   -0.046692        0.051223      3.0441e-05      0.00057458
v  epsilon                0.069069          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9956e-05       0.0099175      0.00092491       0.0017427
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2782         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8782         0.71351         0.85284


 TIME FOR THE TIME STEP            10558:        0.77561E+02

===============================================================


 INSTANT    0.105590000E-01   TIME STEP NUMBER           10559
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.392080625E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.173094313E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.150230777E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.384577177E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.136286805E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81168E-03   0.44965E-02 0.19872E+01 
c  Velocity[X]                                      0.13759E-03 
c  Velocity[Y]                                      0.12760E-03 
c  Velocity[Z]                                      0.42313E-02 
c  Pressure     0.35974E-04     132   0.91582E-02   0.25375E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56555E-08   0.16423E-08 0.99538E-01 
c  r22          0.10852E-01      13   0.53290E-08   0.18375E-08 0.10118E+00 
c  r33          0.21860E-01      15   0.62725E-08   0.12642E-07 0.12719E+00 
c  r12          0.93861E-03      18   0.57651E-08   0.30030E-09 0.60990E+00 
c  r13          0.46675E-02      19   0.58107E-08   0.15330E-08 0.20105E+00 
c  r23          0.39976E-02      19   0.70641E-08   0.12991E-08 0.19950E+00 
c  epsilon      0.10969E+02      11   0.33321E-08   0.10095E-01 0.16501E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84651E-02 0.43373E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61357       0.0052569       0.0015075
v  Velocity[Y]            -0.57401         0.54424       0.0030807      0.00087327
v  Velocity[Z]              1.5653          5.4382          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4382          4.3406          4.3632
v  Pressure                -36.411             360           87.64          169.84
v  r11                   0.0010603        0.081899        0.013073        0.018286
v  r22                   0.0011127        0.082643        0.013353        0.018646
v  r33                   0.0016376         0.17431         0.02725        0.037206
v  r12                    -0.01066        0.013589      -0.0002338      -0.0003093
v  r13                   -0.045542        0.052804      9.3173e-05       0.0010138
v  r23                   -0.046692        0.051209      3.0441e-05      0.00057458
v  epsilon                 0.06907           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9953e-05       0.0099175      0.00092492       0.0017427
v  CourantNb               0.44218             0.6         0.59908         0.59839
v  FourierNb             0.0017847           5.278         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.878         0.71351         0.85284


 TIME FOR THE TIME STEP            10559:        0.74737E+02

===============================================================


 INSTANT    0.105600000E-01   TIME STEP NUMBER           10560
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.791637809E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.296198214E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205864514E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.188958201E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.101538023E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81278E-03   0.45272E-02 0.19905E+01 
c  Velocity[X]                                      0.13804E-03 
c  Velocity[Y]                                      0.12846E-03 
c  Velocity[Z]                                      0.42607E-02 
c  Pressure     0.36312E-04     131   0.92457E-02   0.25612E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53516E-08   0.16148E-08 0.99131E-01 
c  r22          0.10852E-01      13   0.47829E-08   0.17806E-08 0.10037E+00 
c  r33          0.21860E-01      15   0.58718E-08   0.12289E-07 0.12651E+00 
c  r12          0.93861E-03      17   0.68455E-08   0.29299E-09 0.60600E+00 
c  r13          0.46675E-02      19   0.60298E-08   0.14796E-08 0.19875E+00 
c  r23          0.39976E-02      19   0.67264E-08   0.12675E-08 0.19789E+00 
c  epsilon      0.10969E+02      11   0.34136E-08   0.96067E-02 0.16256E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.84320E-02 0.43379E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61356       0.0052568       0.0015074
v  Velocity[Y]            -0.57398         0.54437       0.0030806      0.00087326
v  Velocity[Z]              1.5654          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4383          4.3406          4.3632
v  Pressure                -36.426          360.07          87.688           169.9
v  r11                   0.0010603          0.0819        0.013073        0.018286
v  r22                   0.0011127        0.082643        0.013353        0.018646
v  r33                   0.0016376         0.17429         0.02725        0.037206
v  r12                   -0.010657         0.01359      -0.0002338      -0.0003093
v  r13                    -0.04554        0.052806      9.3174e-05       0.0010138
v  r23                   -0.046693        0.051199      3.0442e-05      0.00057458
v  epsilon                0.069071          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099176      0.00092492       0.0017427
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2781         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781         0.71351         0.85283


 TIME FOR THE TIME STEP            10560:        0.74133E+02

===============================================================


 INSTANT    0.105610000E-01   TIME STEP NUMBER           10561
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205874183E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.233877589E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.174489357E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.488511655E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.258331992E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81351E-03   0.45069E-02 0.19863E+01 
c  Velocity[X]                                      0.13755E-03 
c  Velocity[Y]                                      0.12853E-03 
c  Velocity[Z]                                      0.42408E-02 
c  Pressure     0.36551E-04     132   0.93030E-02   0.25781E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50455E-08   0.16259E-08 0.99214E-01 
c  r22          0.10852E-01      13   0.48094E-08   0.17919E-08 0.10054E+00 
c  r33          0.21860E-01      15   0.56539E-08   0.12341E-07 0.12641E+00 
c  r12          0.93861E-03      17   0.68297E-08   0.29534E-09 0.60539E+00 
c  r13          0.46675E-02      19   0.58817E-08   0.14764E-08 0.19856E+00 
c  r23          0.39976E-02      19   0.69064E-08   0.12803E-08 0.19834E+00 
c  epsilon      0.10969E+02      11   0.35068E-08   0.98118E-02 0.16380E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.83517E-02 0.43118E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61361       0.0052568       0.0015074
v  Velocity[Y]            -0.57402         0.54416       0.0030806      0.00087325
v  Velocity[Z]              1.5652          5.4383          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4383          4.3406          4.3632
v  Pressure                -36.412          360.02          87.633          169.84
v  r11                   0.0010603        0.081916        0.013073        0.018286
v  r22                   0.0011127        0.082643        0.013353        0.018646
v  r33                   0.0016376          0.1743         0.02725        0.037206
v  r12                   -0.010655         0.01359      -0.0002338      -0.0003093
v  r13                   -0.045545        0.052805      9.3174e-05       0.0010138
v  r23                   -0.046693        0.051214      3.0442e-05      0.00057458
v  epsilon                0.069072          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9948e-05       0.0099176      0.00092492       0.0017427
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2784         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8784          0.7135         0.85283


 TIME FOR THE TIME STEP            10561:        0.72920E+02

===============================================================


 INSTANT    0.105620000E-01   TIME STEP NUMBER           10562
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.558931103E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.284573692E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.333441812E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.134744798E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.118915446E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      45   0.81231E-03   0.45236E-02 0.19926E+01 
c  Velocity[X]                                      0.13869E-03 
c  Velocity[Y]                                      0.12812E-03 
c  Velocity[Z]                                      0.42568E-02 
c  Pressure     0.36249E-04     133   0.92263E-02   0.25569E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51064E-08   0.16327E-08 0.99613E-01 
c  r22          0.10852E-01      13   0.51268E-08   0.18128E-08 0.10123E+00 
c  r33          0.21860E-01      14   0.71046E-08   0.12493E-07 0.12738E+00 
c  r12          0.93861E-03      18   0.57627E-08   0.29214E-09 0.60560E+00 
c  r13          0.46675E-02      19   0.54315E-08   0.15069E-08 0.20070E+00 
c  r23          0.39976E-02      19   0.69406E-08   0.12911E-08 0.19959E+00 
c  epsilon      0.10969E+02      11   0.35251E-08   0.98333E-02 0.16521E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.84598E-02 0.43370E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63406         0.61358       0.0052568       0.0015074
v  Velocity[Y]            -0.57392         0.54424       0.0030805      0.00087321
v  Velocity[Z]              1.5654          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4383          4.3406          4.3632
v  Pressure                -36.438          359.95          87.615          169.79
v  r11                   0.0010603        0.081918        0.013073        0.018286
v  r22                   0.0011127        0.082643        0.013353        0.018646
v  r33                   0.0016376         0.17431         0.02725        0.037206
v  r12                   -0.010659        0.013597      -0.0002338      -0.0003093
v  r13                   -0.045542        0.052805      9.3174e-05       0.0010138
v  r23                   -0.046693        0.051203      3.0443e-05      0.00057458
v  epsilon                0.069073          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099177      0.00092492       0.0017427
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2779         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8779         0.71351         0.85283


 TIME FOR THE TIME STEP            10562:        0.76948E+02

===============================================================


 INSTANT    0.105630000E-01   TIME STEP NUMBER           10563
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186919670E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.201509561E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.111644392E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.591435347E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.108622735E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81212E-03   0.45204E-02 0.19912E+01 
c  Velocity[X]                                      0.13900E-03 
c  Velocity[Y]                                      0.12844E-03 
c  Velocity[Z]                                      0.42529E-02 
c  Pressure     0.36543E-04     132   0.93079E-02   0.25776E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51139E-08   0.16495E-08 0.10030E+00 
c  r22          0.10852E-01      13   0.49380E-08   0.18510E-08 0.10244E+00 
c  r33          0.21860E-01      15   0.58323E-08   0.12676E-07 0.12866E+00 
c  r12          0.93861E-03      18   0.64896E-08   0.30058E-09 0.61080E+00 
c  r13          0.46675E-02      19   0.58773E-08   0.15130E-08 0.20222E+00 
c  r23          0.39976E-02      20   0.57938E-08   0.12876E-08 0.20045E+00 
c  epsilon      0.10969E+02      11   0.34305E-08   0.10097E-01 0.17096E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.84428E-02 0.43326E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162021


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63406         0.61356       0.0052568       0.0015074
v  Velocity[Y]            -0.57394         0.54439       0.0030808      0.00087331
v  Velocity[Z]              1.5651          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4383          4.3406          4.3632
v  Pressure                -36.396          360.05          87.657          169.87
v  r11                   0.0010603        0.081907        0.013073        0.018286
v  r22                   0.0011127        0.082638        0.013353        0.018646
v  r33                   0.0016376         0.17435         0.02725        0.037206
v  r12                   -0.010664        0.013598      -0.0002338      -0.0003093
v  r13                   -0.045541        0.052804      9.3175e-05       0.0010138
v  r23                   -0.046693        0.051192      3.0444e-05      0.00057458
v  epsilon                0.069074           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9945e-05       0.0099179      0.00092492       0.0017427
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2773         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8773         0.71351         0.85283


 TIME FOR THE TIME STEP            10563:        0.75446E+02

===============================================================


 INSTANT    0.105640000E-01   TIME STEP NUMBER           10564
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.533711832E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.445456004E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.430231929E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.320767085E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.127871674E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81344E-03   0.45413E-02 0.19944E+01 
c  Velocity[X]                                      0.13820E-03 
c  Velocity[Y]                                      0.12838E-03 
c  Velocity[Z]                                      0.42747E-02 
c  Pressure     0.36296E-04     133   0.92318E-02   0.25602E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53363E-08   0.16732E-08 0.10023E+00 
c  r22          0.10852E-01      13   0.58120E-08   0.18873E-08 0.10265E+00 
c  r33          0.21860E-01      15   0.64348E-08   0.12904E-07 0.12868E+00 
c  r12          0.93861E-03      18   0.72470E-08   0.30209E-09 0.61138E+00 
c  r13          0.46675E-02      19   0.65328E-08   0.15355E-08 0.20169E+00 
c  r23          0.39976E-02      19   0.68733E-08   0.13088E-08 0.20076E+00 
c  epsilon      0.10969E+02      11   0.33469E-08   0.10268E-01 0.16809E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.83792E-02 0.43229E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63383          0.6136       0.0052568       0.0015074
v  Velocity[Y]            -0.57396         0.54421       0.0030807      0.00087328
v  Velocity[Z]              1.5654          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4383          4.3406          4.3632
v  Pressure                 -36.45          360.04           87.63          169.85
v  r11                   0.0010603        0.081908        0.013073        0.018286
v  r22                   0.0011127        0.082637        0.013353        0.018646
v  r33                   0.0016377         0.17432         0.02725        0.037206
v  r12                   -0.010665        0.013596      -0.0002338      -0.0003093
v  r13                   -0.045544        0.052803      9.3174e-05       0.0010138
v  r23                   -0.046693        0.051186      3.0445e-05      0.00057458
v  epsilon                0.069075          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05        0.009918      0.00092492       0.0017427
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2775         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8775         0.71351         0.85284


 TIME FOR THE TIME STEP            10564:        0.72580E+02

===============================================================


 INSTANT    0.105650000E-01   TIME STEP NUMBER           10565
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.403028483E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.217938738E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934909E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.240684884E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.133268271E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.126920299E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81154E-03   0.45244E-02 0.19908E+01 
c  Velocity[X]                                      0.13771E-03 
c  Velocity[Y]                                      0.12885E-03 
c  Velocity[Z]                                      0.42579E-02 
c  Pressure     0.36043E-04     133   0.91725E-02   0.25424E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55567E-08   0.16393E-08 0.99875E-01 
c  r22          0.10852E-01      13   0.52225E-08   0.18283E-08 0.10192E+00 
c  r33          0.21860E-01      15   0.55868E-08   0.12464E-07 0.12766E+00 
c  r12          0.93861E-03      18   0.73257E-08   0.30043E-09 0.61098E+00 
c  r13          0.46675E-02      19   0.59585E-08   0.14966E-08 0.20025E+00 
c  r23          0.39976E-02      19   0.65380E-08   0.12763E-08 0.19925E+00 
c  epsilon      0.10969E+02      11   0.33160E-08   0.94168E-02 0.16120E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.83864E-02 0.43208E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6339         0.61357       0.0052569       0.0015075
v  Velocity[Y]            -0.57397         0.54411       0.0030807      0.00087325
v  Velocity[Z]              1.5652          5.4383          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4383          4.3406          4.3632
v  Pressure                 -36.43          360.04          87.669          169.87
v  r11                   0.0010603        0.081898        0.013073        0.018286
v  r22                   0.0011127        0.082636        0.013353        0.018646
v  r33                   0.0016377         0.17428         0.02725        0.037206
v  r12                   -0.010664        0.013594      -0.0002338      -0.0003093
v  r13                   -0.045544        0.052801      9.3175e-05       0.0010138
v  r23                   -0.046694        0.051219      3.0447e-05      0.00057458
v  epsilon                0.069076          271.15          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9939e-05        0.009918      0.00092492       0.0017427
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2774         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8774         0.71351         0.85284


 TIME FOR THE TIME STEP            10565:        0.73334E+02

===============================================================


 INSTANT    0.105660000E-01   TIME STEP NUMBER           10566
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.261192720E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.330327253E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.163237450E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.864416296E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115251471E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81292E-03   0.45226E-02 0.19919E+01 
c  Velocity[X]                                      0.13800E-03 
c  Velocity[Y]                                      0.12826E-03 
c  Velocity[Z]                                      0.42564E-02 
c  Pressure     0.36583E-04     133   0.93115E-02   0.25805E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58005E-08   0.16550E-08 0.10065E+00 
c  r22          0.10852E-01      13   0.53779E-08   0.18449E-08 0.10219E+00 
c  r33          0.21860E-01      15   0.57589E-08   0.12626E-07 0.12851E+00 
c  r12          0.93861E-03      19   0.59073E-08   0.30102E-09 0.61320E+00 
c  r13          0.46675E-02      19   0.61723E-08   0.15062E-08 0.20077E+00 
c  r23          0.39976E-02      19   0.58614E-08   0.12850E-08 0.20049E+00 
c  epsilon      0.10969E+02      11   0.34628E-08   0.97717E-02 0.16433E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.84194E-02 0.43316E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63395         0.61353        0.005257       0.0015075
v  Velocity[Y]            -0.57392         0.54398       0.0030806      0.00087324
v  Velocity[Z]              1.5652          5.4383          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4383          4.3406          4.3632
v  Pressure                -36.453          359.96          87.613           169.8
v  r11                   0.0010604        0.081891        0.013073        0.018286
v  r22                   0.0011127        0.082637        0.013354        0.018646
v  r33                   0.0016377         0.17429         0.02725        0.037206
v  r12                   -0.010666        0.013591      -0.0002338      -0.0003093
v  r13                   -0.045542        0.052802      9.3175e-05       0.0010138
v  r23                   -0.046695        0.051212      3.0448e-05      0.00057458
v  epsilon                0.069077          271.17          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05        0.009918      0.00092492       0.0017427
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2776         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8776         0.71351         0.85284


 TIME FOR THE TIME STEP            10566:        0.74645E+02

===============================================================


 INSTANT    0.105670000E-01   TIME STEP NUMBER           10567
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.212812878E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.550651096E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.819754383E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.327211453E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.257062637E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81174E-03   0.45304E-02 0.19934E+01 
c  Velocity[X]                                      0.13895E-03 
c  Velocity[Y]                                      0.12814E-03 
c  Velocity[Z]                                      0.42633E-02 
c  Pressure     0.36426E-04     134   0.92773E-02   0.25693E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57993E-08   0.16655E-08 0.10032E+00 
c  r22          0.10852E-01      13   0.59713E-08   0.18452E-08 0.10198E+00 
c  r33          0.21860E-01      15   0.70840E-08   0.12715E-07 0.12828E+00 
c  r12          0.93861E-03      19   0.60208E-08   0.29571E-09 0.60555E+00 
c  r13          0.46675E-02      19   0.65075E-08   0.15018E-08 0.20010E+00 
c  r23          0.39976E-02      19   0.63427E-08   0.12998E-08 0.19965E+00 
c  epsilon      0.10969E+02      11   0.35386E-08   0.10072E-01 0.16606E+00 
c  TempC        0.25716E+06      16   0.15079E-04   0.84059E-02 0.43238E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389          0.6136       0.0052568       0.0015075
v  Velocity[Y]            -0.57403         0.54395       0.0030806      0.00087323
v  Velocity[Z]              1.5655          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4383          4.3406          4.3632
v  Pressure                -36.439          359.98          87.614          169.81
v  r11                   0.0010604        0.081886        0.013073        0.018286
v  r22                   0.0011127        0.082635        0.013354        0.018646
v  r33                   0.0016377         0.17433         0.02725        0.037206
v  r12                   -0.010671        0.013591      -0.0002338      -0.0003093
v  r13                   -0.045544        0.052796      9.3175e-05       0.0010138
v  r23                   -0.046696        0.051201      3.0449e-05      0.00057458
v  epsilon                0.069078          271.18          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9933e-05       0.0099178      0.00092492       0.0017427
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2781         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781          0.7135         0.85283


 TIME FOR THE TIME STEP            10567:        0.72677E+02

===============================================================


 INSTANT    0.105680000E-01   TIME STEP NUMBER           10568
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.269058499E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199046007E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934912E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.428792435E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.233871677E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.151312146E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81252E-03   0.44867E-02 0.19827E+01 
c  Velocity[X]                                      0.13824E-03 
c  Velocity[Y]                                      0.12798E-03 
c  Velocity[Z]                                      0.42205E-02 
c  Pressure     0.35814E-04     133   0.91174E-02   0.25261E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57800E-08   0.16393E-08 0.10020E+00 
c  r22          0.10852E-01      13   0.59196E-08   0.18008E-08 0.10164E+00 
c  r33          0.21860E-01      15   0.62745E-08   0.12401E-07 0.12754E+00 
c  r12          0.93861E-03      18   0.72633E-08   0.30234E-09 0.61101E+00 
c  r13          0.46675E-02      19   0.63740E-08   0.14792E-08 0.19961E+00 
c  r23          0.39976E-02      19   0.52094E-08   0.12840E-08 0.19956E+00 
c  epsilon      0.10969E+02      11   0.32615E-08   0.96179E-02 0.16404E+00 
c  TempC        0.25716E+06      16   0.15166E-04   0.84201E-02 0.43291E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63399         0.61355       0.0052568       0.0015074
v  Velocity[Y]            -0.57393          0.5438       0.0030805       0.0008732
v  Velocity[Z]              1.5652          5.4383          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4383          4.3406          4.3632
v  Pressure                -36.455          359.98          87.637          169.83
v  r11                   0.0010604        0.081886        0.013073        0.018286
v  r22                   0.0011127        0.082633        0.013354        0.018646
v  r33                   0.0016377          0.1743         0.02725        0.037206
v  r12                    -0.01067        0.013591      -0.0002338      -0.0003093
v  r13                   -0.045541        0.052796      9.3175e-05       0.0010138
v  r23                   -0.046697         0.05123       3.045e-05      0.00057458
v  epsilon                0.069079          271.21          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05       0.0099177      0.00092492       0.0017427
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2787         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8787         0.71351         0.85283


 TIME FOR THE TIME STEP            10568:        0.75128E+02

===============================================================


 INSTANT    0.105690000E-01   TIME STEP NUMBER           10569
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.786675502E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.365156455E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.514383524E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168996739E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.378004531E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81184E-03   0.45374E-02 0.19934E+01 
c  Velocity[X]                                      0.13849E-03 
c  Velocity[Y]                                      0.12878E-03 
c  Velocity[Z]                                      0.42701E-02 
c  Pressure     0.36550E-04     134   0.93090E-02   0.25781E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57928E-08   0.16842E-08 0.10095E+00 
c  r22          0.10852E-01      13   0.54577E-08   0.18352E-08 0.10130E+00 
c  r33          0.21860E-01      15   0.64007E-08   0.12846E-07 0.12854E+00 
c  r12          0.93861E-03      18   0.64350E-08   0.30105E-09 0.60986E+00 
c  r13          0.46675E-02      19   0.65398E-08   0.15059E-08 0.19978E+00 
c  r23          0.39976E-02      19   0.52420E-08   0.13223E-08 0.20217E+00 
c  epsilon      0.10969E+02      11   0.33593E-08   0.10548E-01 0.17217E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.85082E-02 0.43550E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61354       0.0052568       0.0015075
v  Velocity[Y]            -0.57403         0.54375       0.0030806       0.0008732
v  Velocity[Z]              1.5653          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4383          4.3406          4.3632
v  Pressure                -36.416          360.04           87.66          169.88
v  r11                   0.0010604        0.081883        0.013073        0.018286
v  r22                   0.0011128        0.082632        0.013354        0.018646
v  r33                   0.0016377         0.17428         0.02725        0.037206
v  r12                   -0.010667        0.013596      -0.0002338      -0.0003093
v  r13                   -0.045542        0.052795      9.3175e-05       0.0010138
v  r23                   -0.046699        0.051223       3.045e-05      0.00057458
v  epsilon                0.069079          271.14          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05       0.0099177      0.00092493       0.0017427
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2781         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781         0.71351         0.85283


 TIME FOR THE TIME STEP            10569:        0.78255E+02

===============================================================


 INSTANT    0.105700000E-01   TIME STEP NUMBER           10570
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.629154243E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.114585588E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.189889431E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.367915593E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.691751928E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81303E-03   0.45271E-02 0.19919E+01 
c  Velocity[X]                                      0.13879E-03 
c  Velocity[Y]                                      0.12860E-03 
c  Velocity[Z]                                      0.42598E-02 
c  Pressure     0.36428E-04     133   0.92708E-02   0.25695E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54278E-08   0.16493E-08 0.10023E+00 
c  r22          0.10852E-01      13   0.51483E-08   0.18340E-08 0.10184E+00 
c  r33          0.21860E-01      15   0.64156E-08   0.12567E-07 0.12776E+00 
c  r12          0.93862E-03      18   0.66303E-08   0.29960E-09 0.60819E+00 
c  r13          0.46675E-02      19   0.64878E-08   0.15023E-08 0.20028E+00 
c  r23          0.39976E-02      19   0.58853E-08   0.12777E-08 0.19884E+00 
c  epsilon      0.10969E+02      11   0.36086E-08   0.98028E-02 0.16461E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83764E-02 0.43154E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61357       0.0052569       0.0015075
v  Velocity[Y]            -0.57385         0.54379       0.0030806      0.00087323
v  Velocity[Z]              1.5652          5.4383          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4383          4.3406          4.3632
v  Pressure                -36.455          360.01           87.65          169.85
v  r11                   0.0010604        0.081875        0.013073        0.018286
v  r22                   0.0011128        0.082631        0.013354        0.018646
v  r33                   0.0016377         0.17429         0.02725        0.037206
v  r12                   -0.010664        0.013593      -0.0002338      -0.0003093
v  r13                   -0.045543        0.052796      9.3176e-05       0.0010138
v  r23                     -0.0467        0.051212       3.045e-05      0.00057458
v  epsilon                 0.06908          271.17          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05       0.0099178      0.00092493       0.0017427
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017847          5.2785         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8785         0.71351         0.85283


 TIME FOR THE TIME STEP            10570:        0.80401E+02

===============================================================


 INSTANT    0.105710000E-01   TIME STEP NUMBER           10571
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.248107806E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.273672856E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.368611312E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.225474463E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.954853857E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81271E-03   0.45428E-02 0.19949E+01 
c  Velocity[X]                                      0.13812E-03 
c  Velocity[Y]                                      0.12858E-03 
c  Velocity[Z]                                      0.42761E-02 
c  Pressure     0.36433E-04     132   0.92765E-02   0.25699E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50896E-08   0.16510E-08 0.10013E+00 
c  r22          0.10852E-01      13   0.56848E-08   0.18157E-08 0.10139E+00 
c  r33          0.21860E-01      15   0.57396E-08   0.12513E-07 0.12726E+00 
c  r12          0.93862E-03      19   0.55194E-08   0.29763E-09 0.60802E+00 
c  r13          0.46675E-02      19   0.64644E-08   0.14805E-08 0.19937E+00 
c  r23          0.39976E-02      19   0.64330E-08   0.12812E-08 0.19837E+00 
c  epsilon      0.10969E+02      11   0.35573E-08   0.99455E-02 0.16539E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.84001E-02 0.43257E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61354       0.0052569       0.0015075
v  Velocity[Y]             -0.5739         0.54386       0.0030806      0.00087326
v  Velocity[Z]              1.5651          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4383          4.3406          4.3632
v  Pressure                -36.431          359.98          87.618          169.82
v  r11                   0.0010604        0.081876        0.013073        0.018286
v  r22                   0.0011128        0.082624        0.013354        0.018646
v  r33                   0.0016378         0.17432         0.02725        0.037206
v  r12                   -0.010663        0.013597      -0.0002338      -0.0003093
v  r13                   -0.045541        0.052795      9.3176e-05       0.0010138
v  r23                   -0.046701         0.05123      3.0451e-05      0.00057458
v  epsilon                0.069081          271.18          7.2635          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099178      0.00092493       0.0017427
v  CourantNb               0.44216             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2785         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8785         0.71351         0.85284


 TIME FOR THE TIME STEP            10571:        0.74481E+02

===============================================================


 INSTANT    0.105720000E-01   TIME STEP NUMBER           10572
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267648741E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.317752856E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.187546233E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.112113749E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.226893863E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81294E-03   0.45140E-02 0.19899E+01 
c  Velocity[X]                                      0.13837E-03 
c  Velocity[Y]                                      0.12838E-03 
c  Velocity[Z]                                      0.42472E-02 
c  Pressure     0.36237E-04     133   0.92279E-02   0.25560E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53936E-08   0.16527E-08 0.10035E+00 
c  r22          0.10852E-01      13   0.57509E-08   0.18222E-08 0.10147E+00 
c  r33          0.21860E-01      15   0.62271E-08   0.12553E-07 0.12795E+00 
c  r12          0.93862E-03      19   0.57486E-08   0.30021E-09 0.60754E+00 
c  r13          0.46675E-02      19   0.68567E-08   0.14924E-08 0.19965E+00 
c  r23          0.39976E-02      19   0.59874E-08   0.12964E-08 0.20074E+00 
c  epsilon      0.10969E+02      11   0.34932E-08   0.99975E-02 0.16678E+00 
c  TempC        0.25716E+06      16   0.15178E-04   0.84036E-02 0.43237E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63395         0.61353       0.0052569       0.0015075
v  Velocity[Y]            -0.57388         0.54382       0.0030806       0.0008733
v  Velocity[Z]              1.5651          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4383          4.3406          4.3632
v  Pressure                -36.468          359.95           87.61           169.8
v  r11                   0.0010604         0.08189        0.013073        0.018286
v  r22                   0.0011128        0.082624        0.013354        0.018646
v  r33                   0.0016378         0.17435         0.02725        0.037206
v  r12                   -0.010664        0.013597      -0.0002338      -0.0003093
v  r13                   -0.045541        0.052794      9.3176e-05       0.0010138
v  r23                   -0.046701        0.051211      3.0452e-05      0.00057458
v  epsilon                0.069082          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099178      0.00092493       0.0017427
v  CourantNb               0.44217             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2788         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8788          0.7135         0.85283


 TIME FOR THE TIME STEP            10572:        0.73884E+02

===============================================================


 INSTANT    0.105730000E-01   TIME STEP NUMBER           10573
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.209893150E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.159994421E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229982804E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.305659942E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.960165808E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81282E-03   0.44754E-02 0.19813E+01 
c  Velocity[X]                                      0.13856E-03 
c  Velocity[Y]                                      0.12784E-03 
c  Velocity[Z]                                      0.42090E-02 
c  Pressure     0.35945E-04     132   0.91467E-02   0.25353E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59185E-08   0.16428E-08 0.10035E+00 
c  r22          0.10852E-01      13   0.61002E-08   0.18087E-08 0.10119E+00 
c  r33          0.21860E-01      15   0.66490E-08   0.12323E-07 0.12716E+00 
c  r12          0.93862E-03      19   0.58816E-08   0.30281E-09 0.61037E+00 
c  r13          0.46675E-02      19   0.69875E-08   0.14717E-08 0.19858E+00 
c  r23          0.39976E-02      19   0.69001E-08   0.12786E-08 0.19895E+00 
c  epsilon      0.10969E+02      11   0.33294E-08   0.97329E-02 0.16506E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.83865E-02 0.43189E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63399         0.61359       0.0052568       0.0015074
v  Velocity[Y]            -0.57396         0.54381       0.0030807      0.00087332
v  Velocity[Z]              1.5652          5.4383          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4383          4.3406          4.3632
v  Pressure                  -36.4          360.06          87.665          169.88
v  r11                   0.0010604        0.081895        0.013073        0.018286
v  r22                   0.0011128        0.082625        0.013354        0.018646
v  r33                   0.0016378         0.17433         0.02725        0.037206
v  r12                   -0.010664        0.013595      -0.0002338      -0.0003093
v  r13                   -0.045545        0.052792      9.3176e-05       0.0010138
v  r23                   -0.046701        0.051205      3.0453e-05      0.00057458
v  epsilon                0.069083          271.22          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099178      0.00092493       0.0017427
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2787         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8787         0.71351         0.85283


 TIME FOR THE TIME STEP            10573:        0.74886E+02

===============================================================


 INSTANT    0.105740000E-01   TIME STEP NUMBER           10574
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.223894526E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.492594059E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.394123062E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.431787523E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.445181601E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81188E-03   0.45179E-02 0.19919E+01 
c  Velocity[X]                                      0.13819E-03 
c  Velocity[Y]                                      0.12865E-03 
c  Velocity[Z]                                      0.42511E-02 
c  Pressure     0.36580E-04     131   0.93150E-02   0.25802E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60634E-08   0.16169E-08 0.99627E-01 
c  r22          0.10852E-01      13   0.62202E-08   0.17810E-08 0.10102E+00 
c  r33          0.21860E-01      15   0.72673E-08   0.12212E-07 0.12676E+00 
c  r12          0.93862E-03      19   0.61870E-08   0.29513E-09 0.60546E+00 
c  r13          0.46675E-02      20   0.57755E-08   0.14626E-08 0.19862E+00 
c  r23          0.39976E-02      19   0.67903E-08   0.12686E-08 0.19856E+00 
c  epsilon      0.10969E+02      11   0.32668E-08   0.93709E-02 0.16137E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.84843E-02 0.43390E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63396         0.61354       0.0052568       0.0015074
v  Velocity[Y]            -0.57388         0.54371       0.0030806       0.0008733
v  Velocity[Z]              1.5654          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4383          4.3406          4.3632
v  Pressure                -36.422          359.97          87.618          169.82
v  r11                   0.0010604        0.081899        0.013073        0.018286
v  r22                   0.0011128        0.082626        0.013354        0.018646
v  r33                   0.0016378          0.1743         0.02725        0.037206
v  r12                   -0.010673        0.013596      -0.0002338      -0.0003093
v  r13                   -0.045541        0.052793      9.3177e-05       0.0010138
v  r23                   -0.046701        0.051201      3.0453e-05      0.00057458
v  epsilon                0.069084          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099178      0.00092493       0.0017427
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2786         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8786         0.71351         0.85283


 TIME FOR THE TIME STEP            10574:        0.79174E+02

===============================================================


 INSTANT    0.105750000E-01   TIME STEP NUMBER           10575
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.728850192E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.271831890E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.396189449E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.348706406E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.744991387E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81179E-03   0.45185E-02 0.19908E+01 
c  Velocity[X]                                      0.13911E-03 
c  Velocity[Y]                                      0.12831E-03 
c  Velocity[Z]                                      0.42511E-02 
c  Pressure     0.36245E-04     133   0.92315E-02   0.25565E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55958E-08   0.16495E-08 0.10049E+00 
c  r22          0.10852E-01      13   0.63247E-08   0.18046E-08 0.10121E+00 
c  r33          0.21860E-01      15   0.66631E-08   0.12485E-07 0.12784E+00 
c  r12          0.93862E-03      19   0.58130E-08   0.30186E-09 0.60876E+00 
c  r13          0.46675E-02      19   0.70041E-08   0.14745E-08 0.19867E+00 
c  r23          0.39976E-02      19   0.72784E-08   0.12963E-08 0.20131E+00 
c  epsilon      0.10969E+02      11   0.33112E-08   0.10060E-01 0.17080E+00 
c  TempC        0.25716E+06      16   0.15100E-04   0.84717E-02 0.43389E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63396         0.61354       0.0052568       0.0015074
v  Velocity[Y]            -0.57396         0.54373       0.0030807      0.00087333
v  Velocity[Z]              1.5651          5.4383          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4383          4.3406          4.3632
v  Pressure                -36.417          360.04          87.658          169.87
v  r11                   0.0010604        0.081911        0.013074        0.018286
v  r22                   0.0011128        0.082626        0.013354        0.018646
v  r33                   0.0016378         0.17431         0.02725        0.037206
v  r12                   -0.010669        0.013594      -0.0002338      -0.0003093
v  r13                   -0.045541         0.05279      9.3177e-05       0.0010138
v  r23                   -0.046702        0.051229      3.0454e-05      0.00057458
v  epsilon                0.069085          271.17          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099178      0.00092493       0.0017427
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2781         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781          0.7135         0.85283


 TIME FOR THE TIME STEP            10575:        0.80338E+02

===============================================================


 INSTANT    0.105760000E-01   TIME STEP NUMBER           10576
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.900446919E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.359233425E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.439031969E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.256066288E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.780307235E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81366E-03   0.44843E-02 0.19832E+01 
c  Velocity[X]                                      0.13809E-03 
c  Velocity[Y]                                      0.12799E-03 
c  Velocity[Z]                                      0.42182E-02 
c  Pressure     0.36319E-04     131   0.92444E-02   0.25618E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61586E-08   0.16326E-08 0.99575E-01 
c  r22          0.10852E-01      13   0.65887E-08   0.18211E-08 0.10148E+00 
c  r33          0.21860E-01      15   0.67715E-08   0.12503E-07 0.12751E+00 
c  r12          0.93862E-03      19   0.58397E-08   0.29542E-09 0.60497E+00 
c  r13          0.46675E-02      20   0.71931E-08   0.15040E-08 0.20048E+00 
c  r23          0.39976E-02      20   0.56106E-08   0.12768E-08 0.19881E+00 
c  epsilon      0.10969E+02      11   0.33794E-08   0.99430E-02 0.16626E+00 
c  TempC        0.25716E+06      16   0.15171E-04   0.83718E-02 0.43253E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63392         0.61357       0.0052569       0.0015074
v  Velocity[Y]            -0.57388         0.54383       0.0030806      0.00087329
v  Velocity[Z]               1.565          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4383          4.3406          4.3632
v  Pressure                -36.488          360.06          87.665          169.88
v  r11                   0.0010604        0.081911        0.013074        0.018286
v  r22                   0.0011128        0.082626        0.013354        0.018646
v  r33                   0.0016379         0.17433         0.02725        0.037206
v  r12                    -0.01067         0.01359      -0.0002338      -0.0003093
v  r13                   -0.045544        0.052791      9.3178e-05       0.0010138
v  r23                   -0.046702        0.051219      3.0456e-05      0.00057458
v  epsilon                0.069086          271.19          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099177      0.00092493       0.0017427
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2764         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8764         0.71351         0.85284


 TIME FOR THE TIME STEP            10576:        0.76509E+02

===============================================================


 INSTANT    0.105770000E-01   TIME STEP NUMBER           10577
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190793122E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105034811E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.610152641E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.384959450E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.707979380E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81212E-03   0.45297E-02 0.19939E+01 
c  Velocity[X]                                      0.13865E-03 
c  Velocity[Y]                                      0.12796E-03 
c  Velocity[Z]                                      0.42631E-02 
c  Pressure     0.36939E-04     133   0.93947E-02   0.26056E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.63397E-08   0.16178E-08 0.99394E-01 
c  r22          0.10852E-01      13   0.67903E-08   0.18095E-08 0.10116E+00 
c  r33          0.21860E-01      15   0.63389E-08   0.12388E-07 0.12701E+00 
c  r12          0.93862E-03      19   0.57078E-08   0.30032E-09 0.60687E+00 
c  r13          0.46675E-02      20   0.57939E-08   0.14848E-08 0.19940E+00 
c  r23          0.39976E-02      19   0.71170E-08   0.12738E-08 0.19877E+00 
c  epsilon      0.10969E+02      11   0.34574E-08   0.95996E-02 0.16212E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.83661E-02 0.43177E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63387         0.61356       0.0052569       0.0015075
v  Velocity[Y]            -0.57391         0.54398       0.0030806       0.0008733
v  Velocity[Z]               1.565          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4383          4.3406          4.3632
v  Pressure                -36.435          360.04          87.664          169.87
v  r11                   0.0010604         0.08192        0.013074        0.018286
v  r22                   0.0011129        0.082626        0.013354        0.018646
v  r33                   0.0016379         0.17431         0.02725        0.037206
v  r12                   -0.010671        0.013588      -0.0002338      -0.0003093
v  r13                   -0.045543        0.052791      9.3178e-05       0.0010138
v  r23                   -0.046702        0.051202      3.0456e-05      0.00057458
v  epsilon                0.069087          271.22          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9941e-05       0.0099176      0.00092493       0.0017427
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2758         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8758         0.71351         0.85284


 TIME FOR THE TIME STEP            10577:        0.74713E+02

===============================================================


 INSTANT    0.105780000E-01   TIME STEP NUMBER           10578
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.408878177E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129754134E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.609626892E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191615266E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.253999193E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81313E-03   0.45540E-02 0.19978E+01 
c  Velocity[X]                                      0.13820E-03 
c  Velocity[Y]                                      0.12842E-03 
c  Velocity[Z]                                      0.42873E-02 
c  Pressure     0.36176E-04     132   0.92185E-02   0.25518E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58779E-08   0.16020E-08 0.99264E-01 
c  r22          0.10852E-01      13   0.64237E-08   0.17894E-08 0.10100E+00 
c  r33          0.21860E-01      15   0.55373E-08   0.12254E-07 0.12712E+00 
c  r12          0.93862E-03      18   0.70117E-08   0.29619E-09 0.60480E+00 
c  r13          0.46675E-02      19   0.66397E-08   0.14721E-08 0.19939E+00 
c  r23          0.39976E-02      19   0.66470E-08   0.12610E-08 0.19848E+00 
c  epsilon      0.10969E+02      11   0.33941E-08   0.96783E-02 0.16503E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.84470E-02 0.43286E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61352       0.0052569       0.0015075
v  Velocity[Y]            -0.57383         0.54415       0.0030807      0.00087334
v  Velocity[Z]              1.5651          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4383          4.3406          4.3632
v  Pressure                -36.478          359.94          87.592          169.78
v  r11                   0.0010604        0.081925        0.013074        0.018286
v  r22                   0.0011129        0.082627        0.013354        0.018646
v  r33                   0.0016379         0.17429         0.02725        0.037206
v  r12                   -0.010673         0.01359      -0.0002338      -0.0003093
v  r13                   -0.045542        0.052795      9.3178e-05       0.0010138
v  r23                   -0.046703        0.051229      3.0457e-05      0.00057458
v  epsilon                0.069088          271.18          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099175      0.00092493       0.0017427
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2762         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8762         0.71351         0.85283


 TIME FOR THE TIME STEP            10578:        0.72859E+02

===============================================================


 INSTANT    0.105790000E-01   TIME STEP NUMBER           10579
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.260288089E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106707863E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200389550E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.573803147E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.135771219E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81266E-03   0.45032E-02 0.19891E+01 
c  Velocity[X]                                      0.13773E-03 
c  Velocity[Y]                                      0.12693E-03 
c  Velocity[Z]                                      0.42386E-02 
c  Pressure     0.36424E-04     131   0.92685E-02   0.25692E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52913E-08   0.16315E-08 0.99434E-01 
c  r22          0.10852E-01      13   0.61533E-08   0.17923E-08 0.10038E+00 
c  r33          0.21860E-01      15   0.69148E-08   0.12437E-07 0.12678E+00 
c  r12          0.93862E-03      18   0.60296E-08   0.29383E-09 0.60346E+00 
c  r13          0.46675E-02      20   0.62555E-08   0.14753E-08 0.19862E+00 
c  r23          0.39976E-02      20   0.55235E-08   0.12712E-08 0.19800E+00 
c  epsilon      0.10969E+02      11   0.34621E-08   0.10098E-01 0.16711E+00 
c  TempC        0.25716E+06      16   0.15112E-04   0.83981E-02 0.43207E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6338         0.61359        0.005257       0.0015075
v  Velocity[Y]            -0.57394         0.54404       0.0030807      0.00087333
v  Velocity[Z]              1.5651          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4383          4.3406          4.3632
v  Pressure                  -36.4          359.98           87.61          169.81
v  r11                   0.0010604        0.081927        0.013074        0.018286
v  r22                   0.0011129        0.082621        0.013354        0.018646
v  r33                   0.0016379          0.1743         0.02725        0.037206
v  r12                    -0.01067        0.013594      -0.0002338      -0.0003093
v  r13                   -0.045544        0.052792      9.3178e-05       0.0010138
v  r23                   -0.046703        0.051226      3.0458e-05      0.00057458
v  epsilon                0.069089          271.18          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9944e-05       0.0099175      0.00092494       0.0017427
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2765         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8765          0.7135         0.85282


 TIME FOR THE TIME STEP            10579:        0.74662E+02

===============================================================


 INSTANT    0.105800000E-01   TIME STEP NUMBER           10580
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.449220005E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136481662E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.491452097E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.315562014E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.344992195E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81241E-03   0.45236E-02 0.19908E+01 
c  Velocity[X]                                      0.13867E-03 
c  Velocity[Y]                                      0.12797E-03 
c  Velocity[Z]                                      0.42569E-02 
c  Pressure     0.36476E-04     133   0.92904E-02   0.25729E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59775E-08   0.16215E-08 0.98916E-01 
c  r22          0.10852E-01      13   0.58635E-08   0.18061E-08 0.10095E+00 
c  r33          0.21860E-01      15   0.63277E-08   0.12450E-07 0.12682E+00 
c  r12          0.93862E-03      18   0.59442E-08   0.29817E-09 0.60557E+00 
c  r13          0.46675E-02      19   0.68024E-08   0.14692E-08 0.19856E+00 
c  r23          0.39976E-02      19   0.67686E-08   0.12797E-08 0.19828E+00 
c  epsilon      0.10969E+02      11   0.34301E-08   0.10360E-01 0.17169E+00 
c  TempC        0.25716E+06      16   0.15165E-04   0.84193E-02 0.43330E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61354        0.005257       0.0015075
v  Velocity[Y]            -0.57378         0.54402       0.0030806      0.00087333
v  Velocity[Z]               1.565          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4383          4.3406          4.3632
v  Pressure                -36.459          360.02          87.647          169.85
v  r11                   0.0010605        0.081933        0.013074        0.018286
v  r22                   0.0011129        0.082621        0.013354        0.018646
v  r33                   0.0016379         0.17431         0.02725        0.037206
v  r12                   -0.010667        0.013593      -0.0002338      -0.0003093
v  r13                   -0.045542        0.052793      9.3178e-05       0.0010138
v  r23                   -0.046703        0.051216      3.0458e-05      0.00057458
v  epsilon                 0.06909          271.21          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9944e-05       0.0099175      0.00092494       0.0017427
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017848           5.277         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.877          0.7135         0.85283


 TIME FOR THE TIME STEP            10580:        0.75056E+02

===============================================================


 INSTANT    0.105810000E-01   TIME STEP NUMBER           10581
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.684604889E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.215939181E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.143033666E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.313617640E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.335338312E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81201E-03   0.45395E-02 0.19935E+01 
c  Velocity[X]                                      0.13845E-03 
c  Velocity[Y]                                      0.12916E-03 
c  Velocity[Z]                                      0.42718E-02 
c  Pressure     0.36578E-04     131   0.93065E-02   0.25801E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59677E-08   0.16203E-08 0.99353E-01 
c  r22          0.10852E-01      13   0.68754E-08   0.18034E-08 0.10078E+00 
c  r33          0.21860E-01      15   0.60582E-08   0.12333E-07 0.12675E+00 
c  r12          0.93862E-03      18   0.66231E-08   0.29262E-09 0.60167E+00 
c  r13          0.46675E-02      19   0.67543E-08   0.14915E-08 0.19889E+00 
c  r23          0.39976E-02      20   0.55132E-08   0.12584E-08 0.19751E+00 
c  epsilon      0.10969E+02      11   0.34095E-08   0.97671E-02 0.16321E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84119E-02 0.43322E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393         0.61354        0.005257       0.0015075
v  Velocity[Y]            -0.57383         0.54413       0.0030808      0.00087337
v  Velocity[Z]              1.5651          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4383          4.3406          4.3632
v  Pressure                -36.409          360.05          87.658          169.87
v  r11                   0.0010605        0.081931        0.013074        0.018286
v  r22                   0.0011129        0.082624        0.013354        0.018646
v  r33                    0.001638         0.17435         0.02725        0.037206
v  r12                   -0.010665        0.013594      -0.0002338      -0.0003093
v  r13                   -0.045543        0.052793      9.3179e-05       0.0010138
v  r23                   -0.046705        0.051232      3.0459e-05      0.00057458
v  epsilon                0.069091          271.21          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9944e-05       0.0099175      0.00092494       0.0017427
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2781         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781          0.7135         0.85283


 TIME FOR THE TIME STEP            10581:        0.77505E+02

===============================================================


 INSTANT    0.105820000E-01   TIME STEP NUMBER           10582
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.243233059E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.946893609E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.349321526E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.996626325E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.295304109E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81261E-03   0.44821E-02 0.19822E+01 
c  Velocity[X]                                      0.13718E-03 
c  Velocity[Y]                                      0.12838E-03 
c  Velocity[Z]                                      0.42166E-02 
c  Pressure     0.36332E-04     132   0.92503E-02   0.25626E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57751E-08   0.15998E-08 0.98770E-01 
c  r22          0.10852E-01      13   0.64615E-08   0.17711E-08 0.10046E+00 
c  r33          0.21860E-01      15   0.61534E-08   0.12190E-07 0.12648E+00 
c  r12          0.93862E-03      18   0.54659E-08   0.29523E-09 0.60447E+00 
c  r13          0.46675E-02      19   0.54753E-08   0.14668E-08 0.19868E+00 
c  r23          0.39976E-02      19   0.63833E-08   0.12709E-08 0.19827E+00 
c  epsilon      0.10969E+02      11   0.35278E-08   0.93143E-02 0.16070E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.83957E-02 0.43195E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61358        0.005257       0.0015075
v  Velocity[Y]            -0.57369          0.5443       0.0030807      0.00087332
v  Velocity[Z]               1.565          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4383          4.3406          4.3632
v  Pressure                -36.484          359.94          87.601          169.79
v  r11                   0.0010605        0.081931        0.013074        0.018286
v  r22                   0.0011129        0.082626        0.013354        0.018646
v  r33                    0.001638         0.17433         0.02725        0.037206
v  r12                   -0.010664        0.013599      -0.0002338      -0.0003093
v  r13                   -0.045545        0.052792      9.3179e-05       0.0010138
v  r23                   -0.046706        0.051219      3.0459e-05      0.00057458
v  epsilon                0.069092          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9944e-05       0.0099177      0.00092494       0.0017427
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2784         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8784          0.7135         0.85283


 TIME FOR THE TIME STEP            10582:        0.77447E+02

===============================================================


 INSTANT    0.105830000E-01   TIME STEP NUMBER           10583
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.501321636E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.418342408E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.180139473E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110172643E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130434464E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81243E-03   0.45200E-02 0.19909E+01 
c  Velocity[X]                                      0.13785E-03 
c  Velocity[Y]                                      0.12743E-03 
c  Velocity[Z]                                      0.42547E-02 
c  Pressure     0.36602E-04     132   0.93091E-02   0.25817E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58882E-08   0.16182E-08 0.98967E-01 
c  r22          0.10852E-01      13   0.59884E-08   0.18041E-08 0.10083E+00 
c  r33          0.21860E-01      15   0.60625E-08   0.12416E-07 0.12668E+00 
c  r12          0.93862E-03      18   0.49400E-08   0.29657E-09 0.60393E+00 
c  r13          0.46675E-02      19   0.63333E-08   0.14900E-08 0.19936E+00 
c  r23          0.39976E-02      19   0.74639E-08   0.12605E-08 0.19660E+00 
c  epsilon      0.10969E+02      11   0.34730E-08   0.10146E-01 0.16772E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.84106E-02 0.43244E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379         0.61356       0.0052571       0.0015075
v  Velocity[Y]            -0.57377         0.54413       0.0030807      0.00087337
v  Velocity[Z]              1.5649          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5787          5.4383          4.3406          4.3632
v  Pressure                -36.409          360.03          87.652          169.86
v  r11                   0.0010605        0.081931        0.013074        0.018286
v  r22                   0.0011129        0.082626        0.013354        0.018646
v  r33                    0.001638          0.1743         0.02725        0.037206
v  r12                   -0.010664        0.013598      -0.0002338      -0.0003093
v  r13                   -0.045543        0.052792       9.318e-05       0.0010138
v  r23                   -0.046707        0.051205       3.046e-05      0.00057458
v  epsilon                0.069093          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099178      0.00092494       0.0017427
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8783         0.71351         0.85284


 TIME FOR THE TIME STEP            10583:        0.75723E+02

===============================================================


 INSTANT    0.105840000E-01   TIME STEP NUMBER           10584
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.280346188E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.155512470E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.277672418E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935014E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226211625E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.369614207E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81245E-03   0.45292E-02 0.19924E+01 
c  Velocity[X]                                      0.13881E-03 
c  Velocity[Y]                                      0.12842E-03 
c  Velocity[Z]                                      0.42619E-02 
c  Pressure     0.36170E-04     133   0.92093E-02   0.25514E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52246E-08   0.16296E-08 0.99359E-01 
c  r22          0.10852E-01      13   0.55191E-08   0.18065E-08 0.10089E+00 
c  r33          0.21860E-01      15   0.61937E-08   0.12436E-07 0.12700E+00 
c  r12          0.93862E-03      18   0.49485E-08   0.30589E-09 0.60846E+00 
c  r13          0.46675E-02      19   0.54095E-08   0.15123E-08 0.20009E+00 
c  r23          0.39976E-02      19   0.60560E-08   0.12860E-08 0.19872E+00 
c  epsilon      0.10969E+02      11   0.34270E-08   0.98969E-02 0.16547E+00 
c  TempC        0.25716E+06      16   0.15167E-04   0.84910E-02 0.43486E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61354        0.005257       0.0015075
v  Velocity[Y]            -0.57373         0.54419       0.0030807      0.00087337
v  Velocity[Z]              1.5653          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4383          4.3406          4.3632
v  Pressure                -36.451          359.98          87.616          169.81
v  r11                   0.0010605        0.081934        0.013074        0.018286
v  r22                   0.0011129        0.082627        0.013354        0.018646
v  r33                    0.001638         0.17431         0.02725        0.037206
v  r12                   -0.010668        0.013597      -0.0002338      -0.0003093
v  r13                   -0.045541        0.052794       9.318e-05       0.0010138
v  r23                   -0.046709         0.05123      3.0462e-05      0.00057458
v  epsilon                0.069094          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9948e-05       0.0099179      0.00092494       0.0017427
v  CourantNb               0.44219             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2775         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8775         0.71351         0.85284


 TIME FOR THE TIME STEP            10584:        0.78724E+02

===============================================================


 INSTANT    0.105850000E-01   TIME STEP NUMBER           10585
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.274725101E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.305922889E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141006870E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.507950336E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115507613E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81263E-03   0.44846E-02 0.19837E+01 
c  Velocity[X]                                      0.13740E-03 
c  Velocity[Y]                                      0.12821E-03 
c  Velocity[Z]                                      0.42190E-02 
c  Pressure     0.36295E-04     131   0.92434E-02   0.25601E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49925E-08   0.16692E-08 0.10045E+00 
c  r22          0.10852E-01      13   0.49144E-08   0.17975E-08 0.10098E+00 
c  r33          0.21860E-01      14   0.71586E-08   0.12462E-07 0.12740E+00 
c  r12          0.93862E-03      17   0.65681E-08   0.30256E-09 0.61099E+00 
c  r13          0.46675E-02      18   0.65317E-08   0.14800E-08 0.19870E+00 
c  r23          0.39976E-02      19   0.61808E-08   0.12925E-08 0.20007E+00 
c  epsilon      0.10969E+02      11   0.32523E-08   0.96094E-02 0.16274E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.83936E-02 0.43200E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61356        0.005257       0.0015075
v  Velocity[Y]            -0.57375         0.54436       0.0030807      0.00087334
v  Velocity[Z]              1.5652          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4383          4.3406          4.3632
v  Pressure                -36.428          360.01          87.635          169.84
v  r11                   0.0010605        0.081933        0.013074        0.018286
v  r22                   0.0011129        0.082628        0.013354        0.018646
v  r33                    0.001638         0.17433         0.02725        0.037206
v  r12                   -0.010667        0.013592      -0.0002338      -0.0003093
v  r13                   -0.045544        0.052796       9.318e-05       0.0010138
v  r23                    -0.04671        0.051222      3.0462e-05      0.00057458
v  epsilon                0.069095          271.21          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05       0.0099181      0.00092494       0.0017427
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2767         0.11442         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8767          0.7135         0.85283


 TIME FOR THE TIME STEP            10585:        0.79915E+02

===============================================================


 INSTANT    0.105860000E-01   TIME STEP NUMBER           10586
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108939842E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.276041380E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.201767098E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.119087458E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.177221827E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81208E-03   0.44831E-02 0.19823E+01 
c  Velocity[X]                                      0.13726E-03 
c  Velocity[Y]                                      0.12757E-03 
c  Velocity[Z]                                      0.42183E-02 
c  Pressure     0.35837E-04     133   0.91169E-02   0.25278E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51744E-08   0.17184E-08 0.10169E+00 
c  r22          0.10852E-01      13   0.49868E-08   0.18048E-08 0.10116E+00 
c  r33          0.21860E-01      15   0.56466E-08   0.12859E-07 0.12925E+00 
c  r12          0.93862E-03      17   0.65592E-08   0.30795E-09 0.61423E+00 
c  r13          0.46675E-02      18   0.63793E-08   0.14746E-08 0.19883E+00 
c  r23          0.39976E-02      19   0.59450E-08   0.13478E-08 0.20486E+00 
c  epsilon      0.10969E+02      11   0.32684E-08   0.10221E-01 0.17099E+00 
c  TempC        0.25716E+06      16   0.15169E-04   0.83806E-02 0.43191E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61354        0.005257       0.0015075
v  Velocity[Y]             -0.5735          0.5441       0.0030807      0.00087331
v  Velocity[Z]              1.5652          5.4383          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4383          4.3406          4.3632
v  Pressure                -36.467          360.04          87.655          169.86
v  r11                   0.0010605        0.081933        0.013074        0.018286
v  r22                    0.001113        0.082629        0.013354        0.018646
v  r33                   0.0016381          0.1743         0.02725        0.037206
v  r12                   -0.010663        0.013586      -0.0002338      -0.0003093
v  r13                   -0.045542        0.052801       9.318e-05       0.0010138
v  r23                   -0.046711        0.051208      3.0462e-05      0.00057458
v  epsilon                0.069095          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9957e-05        0.009918      0.00092494       0.0017427
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2765         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8765         0.71351         0.85283


 TIME FOR THE TIME STEP            10586:        0.82604E+02

===============================================================


 INSTANT    0.105870000E-01   TIME STEP NUMBER           10587
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.256074499E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.437073418E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.513290279E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.906203045E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.339371912E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration      10587, Physical time    0.10587E-01


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint/main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary
 End writing


 Time for restart files:    0.13367E+02



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81203E-03   0.45456E-02 0.19970E+01 
c  Velocity[X]                                      0.13866E-03 
c  Velocity[Y]                                      0.12816E-03 
c  Velocity[Z]                                      0.42788E-02 
c  Pressure     0.36452E-04     131   0.92828E-02   0.25711E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52568E-08   0.17111E-08 0.10222E+00 
c  r22          0.10852E-01      13   0.49659E-08   0.18562E-08 0.10221E+00 
c  r33          0.21860E-01      15   0.65925E-08   0.12936E-07 0.13000E+00 
c  r12          0.93862E-03      18   0.56661E-08   0.30830E-09 0.61609E+00 
c  r13          0.46675E-02      18   0.68679E-08   0.15065E-08 0.20022E+00 
c  r23          0.39976E-02      19   0.53713E-08   0.13137E-08 0.20345E+00 
c  epsilon      0.10969E+02      11   0.34455E-08   0.98831E-02 0.16375E+00 
c  TempC        0.25716E+06      16   0.15120E-04   0.84206E-02 0.43290E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63398         0.61353       0.0052571       0.0015075
v  Velocity[Y]            -0.57358         0.54412       0.0030808      0.00087335
v  Velocity[Z]              1.5651          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4383          4.3406          4.3632
v  Pressure                -36.405          360.02          87.629          169.84
v  r11                   0.0010605        0.081927        0.013074        0.018286
v  r22                    0.001113         0.08263        0.013354        0.018646
v  r33                   0.0016381         0.17428         0.02725        0.037206
v  r12                    -0.01066         0.01358      -0.0002338      -0.0003093
v  r13                   -0.045541        0.052796       9.318e-05       0.0010138
v  r23                   -0.046711        0.051201      3.0462e-05      0.00057458
v  epsilon                0.069096          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9962e-05        0.009918      0.00092494       0.0017427
v  CourantNb               0.44219             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2775         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8775         0.71351         0.85284


 TIME FOR THE TIME STEP            10587:        0.92716E+02

===============================================================


 INSTANT    0.105880000E-01   TIME STEP NUMBER           10588
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129904753E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.148730896E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.539627444E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.259717730E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110529947E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81371E-03   0.44909E-02 0.19832E+01 
c  Velocity[X]                                      0.13799E-03 
c  Velocity[Y]                                      0.12864E-03 
c  Velocity[Z]                                      0.42243E-02 
c  Pressure     0.36090E-04     133   0.91859E-02   0.25456E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53665E-08   0.16367E-08 0.99774E-01 
c  r22          0.10852E-01      13   0.48725E-08   0.17916E-08 0.10099E+00 
c  r33          0.21860E-01      15   0.62316E-08   0.12337E-07 0.12711E+00 
c  r12          0.93862E-03      18   0.54874E-08   0.29676E-09 0.60603E+00 
c  r13          0.46675E-02      18   0.68506E-08   0.14582E-08 0.19798E+00 
c  r23          0.39976E-02      19   0.54821E-08   0.12547E-08 0.19783E+00 
c  epsilon      0.10969E+02      11   0.34077E-08   0.95845E-02 0.16232E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.83799E-02 0.43204E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63377         0.61356        0.005257       0.0015075
v  Velocity[Y]            -0.57348         0.54427       0.0030807      0.00087333
v  Velocity[Z]               1.565          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4383          4.3406          4.3632
v  Pressure                -36.499          360.01          87.636          169.84
v  r11                   0.0010605        0.081928        0.013074        0.018286
v  r22                    0.001113        0.082625        0.013354        0.018646
v  r33                   0.0016381          0.1743         0.02725        0.037206
v  r12                    -0.01066        0.013577      -0.0002338      -0.0003093
v  r13                   -0.045544        0.052797       9.318e-05       0.0010138
v  r23                   -0.046711        0.051221      3.0463e-05      0.00057458
v  epsilon                0.069097           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9965e-05       0.0099179      0.00092494       0.0017427
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2775         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8775         0.71351         0.85284


 TIME FOR THE TIME STEP            10588:        0.73321E+02

===============================================================


 INSTANT    0.105890000E-01   TIME STEP NUMBER           10589
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.172711297E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106790748E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.277752478E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172671066E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.263786445E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81167E-03   0.45278E-02 0.19958E+01 
c  Velocity[X]                                      0.13856E-03 
c  Velocity[Y]                                      0.12866E-03 
c  Velocity[Z]                                      0.42605E-02 
c  Pressure     0.36720E-04     132   0.93495E-02   0.25902E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59766E-08   0.16339E-08 0.99823E-01 
c  r22          0.10852E-01      13   0.45651E-08   0.18173E-08 0.10160E+00 
c  r33          0.21860E-01      15   0.69430E-08   0.12391E-07 0.12727E+00 
c  r12          0.93862E-03      18   0.54059E-08   0.29401E-09 0.60428E+00 
c  r13          0.46675E-02      18   0.68862E-08   0.14624E-08 0.19848E+00 
c  r23          0.39976E-02      19   0.51730E-08   0.12680E-08 0.19806E+00 
c  epsilon      0.10969E+02      11   0.35180E-08   0.96556E-02 0.16364E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84753E-02 0.43374E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379         0.61353       0.0052571       0.0015075
v  Velocity[Y]            -0.57366          0.5441       0.0030807      0.00087334
v  Velocity[Z]              1.5648          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5786          5.4384          4.3406          4.3632
v  Pressure                -36.404          359.99          87.629          169.83
v  r11                   0.0010605        0.081923        0.013074        0.018286
v  r22                    0.001113        0.082626        0.013354        0.018646
v  r33                   0.0016381         0.17432         0.02725        0.037206
v  r12                    -0.01066        0.013573      -0.0002338      -0.0003093
v  r13                   -0.045543        0.052799       9.318e-05       0.0010138
v  r23                   -0.046711        0.051216      3.0464e-05      0.00057458
v  epsilon                0.069098          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9966e-05       0.0099178      0.00092495       0.0017427
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2781         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781         0.71351         0.85284


 TIME FOR THE TIME STEP            10589:        0.77857E+02

===============================================================


 INSTANT    0.105900000E-01   TIME STEP NUMBER           10590
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.569270634E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.174270612E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.165983188E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.231088730E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.286907765E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81293E-03   0.45612E-02 0.19989E+01 
c  Velocity[X]                                      0.13828E-03 
c  Velocity[Y]                                      0.12865E-03 
c  Velocity[Z]                                      0.42943E-02 
c  Pressure     0.36362E-04     131   0.92641E-02   0.25649E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55112E-08   0.16344E-08 0.10026E+00 
c  r22          0.10852E-01      13   0.45867E-08   0.18181E-08 0.10168E+00 
c  r33          0.21860E-01      15   0.68065E-08   0.12403E-07 0.12768E+00 
c  r12          0.93862E-03      18   0.53651E-08   0.29775E-09 0.60730E+00 
c  r13          0.46675E-02      19   0.72721E-08   0.14823E-08 0.19918E+00 
c  r23          0.39976E-02      19   0.56405E-08   0.12726E-08 0.19913E+00 
c  epsilon      0.10969E+02      11   0.33591E-08   0.93753E-02 0.16179E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.84298E-02 0.43304E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389          0.6135       0.0052572       0.0015076
v  Velocity[Y]            -0.57376         0.54422       0.0030807      0.00087335
v  Velocity[Z]               1.565          5.4383          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4383          4.3406          4.3632
v  Pressure                -36.446          359.99          87.631          169.83
v  r11                   0.0010605        0.081922        0.013074        0.018286
v  r22                    0.001113        0.082628        0.013354        0.018646
v  r33                   0.0016381         0.17435         0.02725        0.037206
v  r12                    -0.01066        0.013576      -0.0002338      -0.0003093
v  r13                   -0.045541          0.0528      9.3181e-05       0.0010138
v  r23                    -0.04671        0.051211      3.0465e-05      0.00057458
v  epsilon                0.069099          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9964e-05       0.0099176      0.00092495       0.0017427
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8786         0.71351         0.85284


 TIME FOR THE TIME STEP            10590:        0.84133E+02

===============================================================


 INSTANT    0.105910000E-01   TIME STEP NUMBER           10591
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.213951607E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276549995E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161077971E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122852235E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.135454360E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81353E-03   0.45149E-02 0.19917E+01 
c  Velocity[X]                                      0.13876E-03 
c  Velocity[Y]                                      0.12844E-03 
c  Velocity[Z]                                      0.42477E-02 
c  Pressure     0.36615E-04     133   0.93198E-02   0.25827E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54234E-08   0.16579E-08 0.10037E+00 
c  r22          0.10852E-01      13   0.44914E-08   0.18186E-08 0.10142E+00 
c  r33          0.21860E-01      15   0.59666E-08   0.12629E-07 0.12796E+00 
c  r12          0.93862E-03      18   0.51931E-08   0.30043E-09 0.60657E+00 
c  r13          0.46675E-02      19   0.61990E-08   0.15015E-08 0.19949E+00 
c  r23          0.39976E-02      19   0.54041E-08   0.13034E-08 0.20023E+00 
c  epsilon      0.10969E+02      11   0.32221E-08   0.10225E-01 0.17082E+00 
c  TempC        0.25716E+06      16   0.15103E-04   0.83833E-02 0.43208E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61359       0.0052571       0.0015075
v  Velocity[Y]            -0.57368         0.54438       0.0030807      0.00087335
v  Velocity[Z]               1.565          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4384          4.3406          4.3632
v  Pressure                -36.424          359.97          87.613          169.81
v  r11                   0.0010605        0.081925        0.013074        0.018286
v  r22                    0.001113        0.082629        0.013354        0.018646
v  r33                   0.0016382         0.17433         0.02725        0.037206
v  r12                   -0.010656        0.013578      -0.0002338      -0.0003093
v  r13                   -0.045543        0.052796      9.3182e-05       0.0010138
v  r23                    -0.04671        0.051241      3.0465e-05      0.00057458
v  epsilon                  0.0691          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9962e-05       0.0099177      0.00092495       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2785         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8785         0.71351         0.85283


 TIME FOR THE TIME STEP            10591:        0.81001E+02

===============================================================


 INSTANT    0.105920000E-01   TIME STEP NUMBER           10592
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.148204441E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.297476985E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.885387392E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.869596926E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.258539948E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81233E-03   0.44927E-02 0.19856E+01 
c  Velocity[X]                                      0.13749E-03 
c  Velocity[Y]                                      0.12796E-03 
c  Velocity[Z]                                      0.42272E-02 
c  Pressure     0.36021E-04     133   0.91699E-02   0.25408E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50949E-08   0.16255E-08 0.99769E-01 
c  r22          0.10852E-01      13   0.51432E-08   0.17972E-08 0.10154E+00 
c  r33          0.21860E-01      15   0.55610E-08   0.12315E-07 0.12721E+00 
c  r12          0.93862E-03      18   0.62090E-08   0.29803E-09 0.60384E+00 
c  r13          0.46675E-02      18   0.69932E-08   0.14782E-08 0.19924E+00 
c  r23          0.39976E-02      19   0.54243E-08   0.12728E-08 0.19859E+00 
c  epsilon      0.10969E+02      11   0.33398E-08   0.94033E-02 0.16239E+00 
c  TempC        0.25716E+06      16   0.15165E-04   0.84202E-02 0.43322E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162018


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61356       0.0052571       0.0015075
v  Velocity[Y]            -0.57367         0.54427       0.0030807      0.00087336
v  Velocity[Z]               1.565          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4384          4.3406          4.3632
v  Pressure                -36.459          359.95          87.611           169.8
v  r11                   0.0010605        0.081923        0.013074        0.018286
v  r22                    0.001113        0.082629        0.013354        0.018646
v  r33                   0.0016382         0.17429         0.02725        0.037206
v  r12                   -0.010656        0.013583      -0.0002338      -0.0003093
v  r13                   -0.045541        0.052798      9.3181e-05       0.0010138
v  r23                   -0.046709        0.051222      3.0465e-05      0.00057458
v  epsilon                0.069101          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9958e-05       0.0099176      0.00092495       0.0017427
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8783         0.71351         0.85284


 TIME FOR THE TIME STEP            10592:        0.83533E+02

===============================================================


 INSTANT    0.105930000E-01   TIME STEP NUMBER           10593
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.657226994E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.539870542E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.469857014E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.146305489E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.231315703E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81181E-03   0.45209E-02 0.19902E+01 
c  Velocity[X]                                      0.13802E-03 
c  Velocity[Y]                                      0.12775E-03 
c  Velocity[Z]                                      0.42551E-02 
c  Pressure     0.36273E-04     132   0.92356E-02   0.25586E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49631E-08   0.16411E-08 0.10038E+00 
c  r22          0.10852E-01      13   0.45511E-08   0.18040E-08 0.10085E+00 
c  r33          0.21860E-01      15   0.51792E-08   0.12343E-07 0.12669E+00 
c  r12          0.93862E-03      17   0.67476E-08   0.29186E-09 0.60143E+00 
c  r13          0.46675E-02      18   0.71674E-08   0.14815E-08 0.19834E+00 
c  r23          0.39976E-02      18   0.66375E-08   0.12631E-08 0.19826E+00 
c  epsilon      0.10969E+02      11   0.33356E-08   0.95381E-02 0.16151E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84330E-02 0.43320E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393         0.61352       0.0052571       0.0015076
v  Velocity[Y]            -0.57363          0.5442       0.0030808      0.00087338
v  Velocity[Z]               1.565          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4384          4.3406          4.3632
v  Pressure                -36.445          359.98          87.613          169.82
v  r11                   0.0010606         0.08192        0.013074        0.018286
v  r22                    0.001113         0.08263        0.013354        0.018646
v  r33                   0.0016382         0.17431         0.02725        0.037206
v  r12                   -0.010658        0.013581      -0.0002338      -0.0003093
v  r13                   -0.045542        0.052799      9.3182e-05       0.0010138
v  r23                   -0.046708        0.051206      3.0466e-05      0.00057458
v  epsilon                0.069102           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9953e-05       0.0099176      0.00092495       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017848           5.278         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.878         0.71351         0.85283


 TIME FOR THE TIME STEP            10593:        0.80996E+02

===============================================================


 INSTANT    0.105940000E-01   TIME STEP NUMBER           10594
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.318557629E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119270128E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.612732206E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.250987871E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.112596992E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81370E-03   0.45146E-02 0.19909E+01 
c  Velocity[X]                                      0.13823E-03 
c  Velocity[Y]                                      0.12800E-03 
c  Velocity[Z]                                      0.42483E-02 
c  Pressure     0.36251E-04     133   0.92226E-02   0.25570E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55679E-08   0.16201E-08 0.99664E-01 
c  r22          0.10852E-01      12   0.64184E-08   0.17848E-08 0.10115E+00 
c  r33          0.21860E-01      15   0.57306E-08   0.12272E-07 0.12696E+00 
c  r12          0.93862E-03      17   0.69243E-08   0.29834E-09 0.60663E+00 
c  r13          0.46675E-02      19   0.53779E-08   0.14744E-08 0.19950E+00 
c  r23          0.39976E-02      19   0.52724E-08   0.12633E-08 0.19814E+00 
c  epsilon      0.10969E+02      11   0.33847E-08   0.94900E-02 0.16248E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.84107E-02 0.43190E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63391         0.61357       0.0052571       0.0015076
v  Velocity[Y]            -0.57355         0.54427       0.0030808      0.00087338
v  Velocity[Z]              1.5653          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4384          4.3406          4.3632
v  Pressure                -36.455          360.03          87.656          169.87
v  r11                   0.0010606        0.081921        0.013074        0.018286
v  r22                    0.001113        0.082631        0.013354        0.018646
v  r33                   0.0016382         0.17433         0.02725        0.037206
v  r12                   -0.010659        0.013582      -0.0002338      -0.0003093
v  r13                   -0.045544        0.052801      9.3182e-05       0.0010138
v  r23                   -0.046707        0.051227      3.0468e-05      0.00057459
v  epsilon                0.069103          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099177      0.00092495       0.0017427
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2778         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8778         0.71351         0.85284


 TIME FOR THE TIME STEP            10594:        0.82633E+02

===============================================================


 INSTANT    0.105950000E-01   TIME STEP NUMBER           10595
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.500625758E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.548058639E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934901E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.523710133E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.417942679E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.163194672E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81203E-03   0.45016E-02 0.19887E+01 
c  Velocity[X]                                      0.13876E-03 
c  Velocity[Y]                                      0.12830E-03 
c  Velocity[Z]                                      0.42346E-02 
c  Pressure     0.36462E-04     133   0.92801E-02   0.25719E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50830E-08   0.16481E-08 0.99986E-01 
c  r22          0.10852E-01      13   0.47724E-08   0.18267E-08 0.10135E+00 
c  r33          0.21860E-01      15   0.61501E-08   0.12547E-07 0.12729E+00 
c  r12          0.93862E-03      18   0.50774E-08   0.29829E-09 0.60609E+00 
c  r13          0.46675E-02      19   0.63305E-08   0.14929E-08 0.19904E+00 
c  r23          0.39976E-02      18   0.66072E-08   0.12681E-08 0.19792E+00 
c  epsilon      0.10969E+02      11   0.34605E-08   0.99273E-02 0.16423E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.83989E-02 0.43229E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61356       0.0052571       0.0015075
v  Velocity[Y]            -0.57367         0.54438       0.0030807      0.00087338
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4384          4.3406          4.3632
v  Pressure                -36.401          360.08           87.69           169.9
v  r11                   0.0010606        0.081923        0.013074        0.018286
v  r22                    0.001113        0.082627        0.013354        0.018646
v  r33                   0.0016382         0.17431         0.02725        0.037206
v  r12                    -0.01066        0.013587      -0.0002338      -0.0003093
v  r13                   -0.045541        0.052801      9.3183e-05       0.0010138
v  r23                   -0.046705        0.051217      3.0468e-05      0.00057459
v  epsilon                0.069103          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099176      0.00092495       0.0017427
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2779         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8779         0.71351         0.85284


 TIME FOR THE TIME STEP            10595:        0.80237E+02

===============================================================


 INSTANT    0.105960000E-01   TIME STEP NUMBER           10596
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.958012237E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.416141082E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.373986001E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.194086946E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.146859941E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81361E-03   0.45321E-02 0.19919E+01 
c  Velocity[X]                                      0.13832E-03 
c  Velocity[Y]                                      0.12825E-03 
c  Velocity[Z]                                      0.42655E-02 
c  Pressure     0.36152E-04     132   0.92079E-02   0.25500E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54583E-08   0.16796E-08 0.10074E+00 
c  r22          0.10852E-01      13   0.45902E-08   0.18126E-08 0.10126E+00 
c  r33          0.21860E-01      15   0.53396E-08   0.12644E-07 0.12798E+00 
c  r12          0.93862E-03      18   0.55343E-08   0.29379E-09 0.60246E+00 
c  r13          0.46675E-02      19   0.57339E-08   0.14936E-08 0.19938E+00 
c  r23          0.39976E-02      18   0.69069E-08   0.13037E-08 0.20050E+00 
c  epsilon      0.10969E+02      11   0.32560E-08   0.10159E-01 0.16763E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.84179E-02 0.43341E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63377         0.61356       0.0052571       0.0015075
v  Velocity[Y]            -0.57373         0.54418       0.0030807      0.00087337
v  Velocity[Z]              1.5654          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4384          4.3406          4.3632
v  Pressure                -36.458             360           87.64          169.84
v  r11                   0.0010606        0.081924        0.013074        0.018286
v  r22                   0.0011131        0.082628        0.013354        0.018646
v  r33                   0.0016383         0.17428         0.02725        0.037206
v  r12                   -0.010662        0.013594     -0.00023381      -0.0003093
v  r13                    -0.04554        0.052801      9.3183e-05       0.0010138
v  r23                   -0.046704        0.051199      3.0468e-05      0.00057459
v  epsilon                0.069104          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099177      0.00092495       0.0017427
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2779         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8779         0.71351         0.85283


 TIME FOR THE TIME STEP            10596:        0.77475E+02

===============================================================


 INSTANT    0.105970000E-01   TIME STEP NUMBER           10597
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.112695575E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.157585427E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.408581132E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.111289503E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.701069733E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81220E-03   0.45330E-02 0.19921E+01 
c  Velocity[X]                                      0.13746E-03 
c  Velocity[Y]                                      0.12808E-03 
c  Velocity[Z]                                      0.42675E-02 
c  Pressure     0.36889E-04     132   0.93946E-02   0.26021E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57023E-08   0.16888E-08 0.10146E+00 
c  r22          0.10852E-01      13   0.46166E-08   0.18014E-08 0.10177E+00 
c  r33          0.21860E-01      14   0.68988E-08   0.12483E-07 0.12849E+00 
c  r12          0.93862E-03      17   0.70027E-08   0.30021E-09 0.61164E+00 
c  r13          0.46675E-02      19   0.66100E-08   0.14550E-08 0.19860E+00 
c  r23          0.39976E-02      19   0.59406E-08   0.12961E-08 0.20155E+00 
c  epsilon      0.10969E+02      11   0.32005E-08   0.96280E-02 0.16686E+00 
c  TempC        0.25716E+06      16   0.15127E-04   0.84340E-02 0.43388E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61358       0.0052572       0.0015075
v  Velocity[Y]            -0.57374         0.54424       0.0030808      0.00087334
v  Velocity[Z]              1.5653          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4384          4.3406          4.3632
v  Pressure                -36.444          360.05          87.649          169.87
v  r11                   0.0010606        0.081916        0.013074        0.018286
v  r22                   0.0011131        0.082629        0.013354        0.018646
v  r33                   0.0016383          0.1743         0.02725        0.037206
v  r12                   -0.010661        0.013587     -0.00023381      -0.0003093
v  r13                   -0.045544          0.0528      9.3183e-05       0.0010138
v  r23                   -0.046703        0.051191      3.0469e-05      0.00057459
v  epsilon                0.069105          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099177      0.00092495       0.0017427
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017848          5.2765         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8765         0.71351         0.85283


 TIME FOR THE TIME STEP            10597:        0.78636E+02

===============================================================


 INSTANT    0.105980000E-01   TIME STEP NUMBER           10598
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141144649E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.117642175E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.159330717E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.942264555E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.752598481E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81213E-03   0.45124E-02 0.19898E+01 
c  Velocity[X]                                      0.13761E-03 
c  Velocity[Y]                                      0.12818E-03 
c  Velocity[Z]                                      0.42466E-02 
c  Pressure     0.35849E-04     132   0.91282E-02   0.25287E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58701E-08   0.16381E-08 0.99597E-01 
c  r22          0.10852E-01      13   0.48688E-08   0.18110E-08 0.10119E+00 
c  r33          0.21860E-01      14   0.68649E-08   0.12486E-07 0.12726E+00 
c  r12          0.93862E-03      18   0.51111E-08   0.29515E-09 0.60489E+00 
c  r13          0.46675E-02      19   0.53182E-08   0.14847E-08 0.19865E+00 
c  r23          0.39976E-02      19   0.57807E-08   0.12830E-08 0.19918E+00 
c  epsilon      0.10969E+02      11   0.33355E-08   0.98458E-02 0.16529E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.84191E-02 0.43276E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61357       0.0052572       0.0015076
v  Velocity[Y]            -0.57373         0.54438       0.0030807      0.00087332
v  Velocity[Z]              1.5653          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4384          4.3406          4.3632
v  Pressure                -36.433          359.96          87.613           169.8
v  r11                   0.0010606        0.081913        0.013074        0.018286
v  r22                   0.0011131         0.08263        0.013354        0.018646
v  r33                   0.0016383         0.17431         0.02725        0.037206
v  r12                   -0.010667         0.01359     -0.00023381      -0.0003093
v  r13                   -0.045542        0.052801      9.3184e-05       0.0010138
v  r23                   -0.046702        0.051217      3.0469e-05      0.00057459
v  epsilon                0.069106          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099177      0.00092495       0.0017427
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2766         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8766         0.71351         0.85283


 TIME FOR THE TIME STEP            10598:        0.75734E+02

===============================================================


 INSTANT    0.105990000E-01   TIME STEP NUMBER           10599
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195842370E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.334940543E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227118237E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.349682432E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182106042E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81225E-03   0.45229E-02 0.19903E+01 
c  Velocity[X]                                      0.13884E-03 
c  Velocity[Y]                                      0.12845E-03 
c  Velocity[Z]                                      0.42556E-02 
c  Pressure     0.36339E-04     132   0.92519E-02   0.25632E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.62500E-08   0.16298E-08 0.99829E-01 
c  r22          0.10852E-01      13   0.49581E-08   0.17803E-08 0.10082E+00 
c  r33          0.21860E-01      14   0.65359E-08   0.12171E-07 0.12647E+00 
c  r12          0.93863E-03      18   0.55015E-08   0.29156E-09 0.60334E+00 
c  r13          0.46675E-02      18   0.68561E-08   0.14559E-08 0.19776E+00 
c  r23          0.39976E-02      19   0.55779E-08   0.12547E-08 0.19750E+00 
c  epsilon      0.10969E+02      11   0.33300E-08   0.92581E-02 0.16053E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.84954E-02 0.43441E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63371         0.61359       0.0052572       0.0015076
v  Velocity[Y]            -0.57371          0.5442       0.0030808      0.00087336
v  Velocity[Z]              1.5653          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4384          4.3406          4.3632
v  Pressure                -36.397          359.98           87.62          169.82
v  r11                   0.0010606        0.081905        0.013074        0.018286
v  r22                   0.0011131        0.082631        0.013354        0.018646
v  r33                   0.0016383         0.17435         0.02725        0.037206
v  r12                   -0.010663        0.013591     -0.00023381      -0.0003093
v  r13                   -0.045541        0.052798      9.3184e-05       0.0010138
v  r23                   -0.046702        0.051218       3.047e-05      0.00057459
v  epsilon                0.069107          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05       0.0099178      0.00092496       0.0017427
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2769         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8769         0.71351         0.85283


 TIME FOR THE TIME STEP            10599:        0.77529E+02

===============================================================


 INSTANT    0.106000000E-01   TIME STEP NUMBER           10600
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239389662E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.684617093E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.254109921E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.124720836E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108613642E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81317E-03   0.45093E-02 0.19865E+01 
c  Velocity[X]                                      0.13790E-03 
c  Velocity[Y]                                      0.12824E-03 
c  Velocity[Z]                                      0.42431E-02 
c  Pressure     0.36387E-04     133   0.92626E-02   0.25665E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60297E-08   0.16479E-08 0.99851E-01 
c  r22          0.10852E-01      13   0.49183E-08   0.18280E-08 0.10149E+00 
c  r33          0.21860E-01      15   0.52700E-08   0.12544E-07 0.12748E+00 
c  r12          0.93863E-03      18   0.52992E-08   0.29445E-09 0.60423E+00 
c  r13          0.46675E-02      19   0.55866E-08   0.14822E-08 0.19871E+00 
c  r23          0.39976E-02      18   0.69791E-08   0.12754E-08 0.19906E+00 
c  epsilon      0.10969E+02      11   0.32874E-08   0.98938E-02 0.16557E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.83233E-02 0.43078E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63382         0.61361       0.0052571       0.0015076
v  Velocity[Y]            -0.57362         0.54411       0.0030807      0.00087329
v  Velocity[Z]              1.5654          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4384          4.3406          4.3632
v  Pressure                -36.485          359.99          87.627          169.82
v  r11                   0.0010606        0.081909        0.013074        0.018286
v  r22                   0.0011131        0.082631        0.013354        0.018646
v  r33                   0.0016383         0.17433         0.02725        0.037206
v  r12                   -0.010667        0.013595     -0.00023381      -0.0003093
v  r13                   -0.045543        0.052798      9.3185e-05       0.0010138
v  r23                   -0.046701        0.051208       3.047e-05      0.00057459
v  epsilon                0.069108          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9919e-05       0.0099178      0.00092496       0.0017427
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2764         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8764         0.71351         0.85284


 TIME FOR THE TIME STEP            10600:        0.77206E+02

===============================================================


 INSTANT    0.106010000E-01   TIME STEP NUMBER           10601
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.439639268E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.955096025E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.238711783E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.378453682E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.894657430E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81258E-03   0.45170E-02 0.19899E+01 
c  Velocity[X]                                      0.13747E-03 
c  Velocity[Y]                                      0.12802E-03 
c  Velocity[Z]                                      0.42515E-02 
c  Pressure     0.36215E-04     132   0.92179E-02   0.25545E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57740E-08   0.16365E-08 0.99514E-01 
c  r22          0.10852E-01      13   0.48234E-08   0.18194E-08 0.10149E+00 
c  r33          0.21860E-01      14   0.68525E-08   0.12546E-07 0.12721E+00 
c  r12          0.93863E-03      18   0.50738E-08   0.29703E-09 0.60285E+00 
c  r13          0.46675E-02      18   0.70528E-08   0.14973E-08 0.19890E+00 
c  r23          0.39976E-02      19   0.51935E-08   0.12825E-08 0.19874E+00 
c  epsilon      0.10969E+02      11   0.32281E-08   0.99595E-02 0.16584E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84007E-02 0.43273E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61359       0.0052571       0.0015075
v  Velocity[Y]            -0.57371         0.54417       0.0030806      0.00087327
v  Velocity[Z]              1.5656          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5793          5.4384          4.3406          4.3632
v  Pressure                -36.434          360.06          87.656          169.87
v  r11                   0.0010606        0.081908        0.013074        0.018286
v  r22                   0.0011131        0.082632        0.013354        0.018646
v  r33                   0.0016384         0.17429         0.02725        0.037206
v  r12                   -0.010672        0.013594     -0.00023381      -0.0003093
v  r13                   -0.045542        0.052801      9.3185e-05       0.0010138
v  r23                   -0.046701        0.051227      3.0471e-05      0.00057459
v  epsilon                0.069109          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9917e-05       0.0099177      0.00092496       0.0017427
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2764         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8764         0.71351         0.85284


 TIME FOR THE TIME STEP            10601:        0.78816E+02

===============================================================


 INSTANT    0.106020000E-01   TIME STEP NUMBER           10602
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.268615882E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138329857E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172071846E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.458603173E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.219698046E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81231E-03   0.45496E-02 0.19967E+01 
c  Velocity[X]                                      0.13870E-03 
c  Velocity[Y]                                      0.12841E-03 
c  Velocity[Z]                                      0.42825E-02 
c  Pressure     0.36869E-04     133   0.93877E-02   0.26006E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60839E-08   0.16669E-08 0.10040E+00 
c  r22          0.10852E-01      13   0.45715E-08   0.18149E-08 0.10167E+00 
c  r33          0.21860E-01      15   0.53371E-08   0.12610E-07 0.12814E+00 
c  r12          0.93863E-03      18   0.55972E-08   0.29724E-09 0.60448E+00 
c  r13          0.46675E-02      19   0.55821E-08   0.14919E-08 0.19979E+00 
c  r23          0.39976E-02      19   0.61936E-08   0.13065E-08 0.20064E+00 
c  epsilon      0.10969E+02      11   0.31979E-08   0.10082E-01 0.16942E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.84756E-02 0.43408E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63397         0.61357       0.0052572       0.0015076
v  Velocity[Y]            -0.57373         0.54429       0.0030806      0.00087328
v  Velocity[Z]              1.5656          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5794          5.4384          4.3406          4.3632
v  Pressure                -36.459             360          87.646          169.84
v  r11                   0.0010606        0.081908        0.013074        0.018286
v  r22                   0.0011131        0.082633        0.013354        0.018646
v  r33                   0.0016384          0.1743         0.02725        0.037206
v  r12                   -0.010671        0.013596     -0.00023381      -0.0003093
v  r13                    -0.04554        0.052802      9.3185e-05       0.0010138
v  r23                   -0.046701        0.051216      3.0471e-05      0.00057459
v  epsilon                 0.06911          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099178      0.00092496       0.0017427
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2767         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8767         0.71351         0.85284


 TIME FOR THE TIME STEP            10602:        0.78559E+02

===============================================================


 INSTANT    0.106030000E-01   TIME STEP NUMBER           10603
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285092554E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.523673340E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267694243E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.252061618E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106676847E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81320E-03   0.45232E-02 0.19917E+01 
c  Velocity[X]                                      0.13867E-03 
c  Velocity[Y]                                      0.12885E-03 
c  Velocity[Z]                                      0.42557E-02 
c  Pressure     0.36568E-04     133   0.93124E-02   0.25794E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58772E-08   0.16234E-08 0.99656E-01 
c  r22          0.10852E-01      13   0.50658E-08   0.17864E-08 0.10084E+00 
c  r33          0.21860E-01      15   0.59834E-08   0.12192E-07 0.12639E+00 
c  r12          0.93863E-03      18   0.62128E-08   0.30429E-09 0.61015E+00 
c  r13          0.46675E-02      19   0.67565E-08   0.14665E-08 0.19908E+00 
c  r23          0.39976E-02      19   0.58725E-08   0.12503E-08 0.19711E+00 
c  epsilon      0.10969E+02      11   0.32364E-08   0.93664E-02 0.16101E+00 
c  TempC        0.25716E+06      16   0.15099E-04   0.84068E-02 0.43268E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61361       0.0052571       0.0015076
v  Velocity[Y]            -0.57371         0.54407       0.0030807       0.0008733
v  Velocity[Z]              1.5653          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4384          4.3406          4.3632
v  Pressure                -36.435          360.07          87.665          169.89
v  r11                   0.0010606        0.081907        0.013074        0.018286
v  r22                   0.0011131        0.082629        0.013354        0.018646
v  r33                   0.0016384         0.17433         0.02725        0.037206
v  r12                   -0.010665        0.013589     -0.00023381      -0.0003093
v  r13                   -0.045542        0.052799      9.3185e-05       0.0010138
v  r23                   -0.046701        0.051205      3.0472e-05      0.00057459
v  epsilon                 0.06911           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099179      0.00092496       0.0017427
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2771         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8771          0.7135         0.85283


 TIME FOR THE TIME STEP            10603:        0.78073E+02

===============================================================


 INSTANT    0.106040000E-01   TIME STEP NUMBER           10604
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.262853380E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242360626E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.184495520E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.244007952E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.135770314E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81263E-03   0.45262E-02 0.19934E+01 
c  Velocity[X]                                      0.13823E-03 
c  Velocity[Y]                                      0.12934E-03 
c  Velocity[Z]                                      0.42586E-02 
c  Pressure     0.36455E-04     131   0.92818E-02   0.25714E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57007E-08   0.16118E-08 0.98698E-01 
c  r22          0.10852E-01      13   0.51708E-08   0.18109E-08 0.10106E+00 
c  r33          0.21860E-01      15   0.70755E-08   0.12433E-07 0.12658E+00 
c  r12          0.93863E-03      18   0.63621E-08   0.29455E-09 0.60470E+00 
c  r13          0.46675E-02      19   0.70259E-08   0.14844E-08 0.19896E+00 
c  r23          0.39976E-02      19   0.64090E-08   0.12683E-08 0.19741E+00 
c  epsilon      0.10969E+02      11   0.33644E-08   0.99469E-02 0.16531E+00 
c  TempC        0.25716E+06      16   0.15191E-04   0.84301E-02 0.43261E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162015


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6336         0.61357       0.0052572       0.0015076
v  Velocity[Y]            -0.57352         0.54418       0.0030807      0.00087329
v  Velocity[Z]              1.5654          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4384          4.3406          4.3632
v  Pressure                -36.476          359.93          87.599          169.78
v  r11                   0.0010607        0.081908        0.013074        0.018286
v  r22                   0.0011131        0.082629        0.013354        0.018646
v  r33                   0.0016384          0.1743         0.02725        0.037206
v  r12                   -0.010663        0.013593     -0.00023381      -0.0003093
v  r13                   -0.045539        0.052799      9.3186e-05       0.0010138
v  r23                   -0.046701        0.051226      3.0472e-05      0.00057459
v  epsilon                0.069111          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9911e-05       0.0099179      0.00092496       0.0017427
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2778         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8778         0.71351         0.85284


 TIME FOR THE TIME STEP            10604:        0.76101E+02

===============================================================


 INSTANT    0.106050000E-01   TIME STEP NUMBER           10605
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130793972E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.329112460E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934912E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.152417202E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276210523E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195211214E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81128E-03   0.45139E-02 0.19896E+01 
c  Velocity[X]                                      0.13843E-03 
c  Velocity[Y]                                      0.12819E-03 
c  Velocity[Z]                                      0.42473E-02 
c  Pressure     0.36362E-04     133   0.92549E-02   0.25648E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53766E-08   0.16142E-08 0.99148E-01 
c  r22          0.10852E-01      13   0.47856E-08   0.17927E-08 0.10064E+00 
c  r33          0.21860E-01      15   0.64104E-08   0.12278E-07 0.12631E+00 
c  r12          0.93863E-03      18   0.58388E-08   0.29565E-09 0.60488E+00 
c  r13          0.46675E-02      19   0.55147E-08   0.14739E-08 0.19818E+00 
c  r23          0.39976E-02      19   0.61890E-08   0.12504E-08 0.19687E+00 
c  epsilon      0.10969E+02      11   0.35037E-08   0.97315E-02 0.16440E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.83795E-02 0.43254E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63355         0.61358       0.0052571       0.0015075
v  Velocity[Y]            -0.57355         0.54386       0.0030806      0.00087327
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4384          4.3406          4.3632
v  Pressure                -36.416          360.05          87.658          169.88
v  r11                   0.0010607         0.08191        0.013074        0.018286
v  r22                   0.0011132        0.082631        0.013354        0.018646
v  r33                   0.0016384         0.17428         0.02725        0.037206
v  r12                   -0.010661        0.013587     -0.00023381      -0.0003093
v  r13                    -0.04554        0.052797      9.3185e-05       0.0010138
v  r23                   -0.046701         0.05122      3.0473e-05      0.00057459
v  epsilon                0.069112          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9912e-05       0.0099179      0.00092496       0.0017427
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2784         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8784         0.71351         0.85284


 TIME FOR THE TIME STEP            10605:        0.77613E+02

===============================================================


 INSTANT    0.106060000E-01   TIME STEP NUMBER           10606
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.598762221E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.921535600E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.169584488E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.311308976E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168983387E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81362E-03   0.44984E-02 0.19860E+01 
c  Velocity[X]                                      0.13702E-03 
c  Velocity[Y]                                      0.12796E-03 
c  Velocity[Z]                                      0.42334E-02 
c  Pressure     0.36173E-04     133   0.92102E-02   0.25515E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54844E-08   0.16217E-08 0.99095E-01 
c  r22          0.10852E-01      13   0.47298E-08   0.18187E-08 0.10142E+00 
c  r33          0.21860E-01      15   0.65415E-08   0.12356E-07 0.12674E+00 
c  r12          0.93863E-03      18   0.57279E-08   0.29078E-09 0.59934E+00 
c  r13          0.46675E-02      19   0.59732E-08   0.14571E-08 0.19818E+00 
c  r23          0.39976E-02      19   0.64077E-08   0.12603E-08 0.19752E+00 
c  epsilon      0.10969E+02      11   0.35254E-08   0.95493E-02 0.16330E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.83624E-02 0.43168E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61357       0.0052572       0.0015076
v  Velocity[Y]            -0.57337         0.54369       0.0030806      0.00087323
v  Velocity[Z]              1.5653          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4384          4.3406          4.3632
v  Pressure                -36.471          360.03          87.658          169.87
v  r11                   0.0010607        0.081914        0.013074        0.018286
v  r22                   0.0011132        0.082632        0.013354        0.018646
v  r33                   0.0016385         0.17429         0.02725        0.037206
v  r12                   -0.010659        0.013579     -0.00023381     -0.00030931
v  r13                   -0.045542        0.052797      9.3186e-05       0.0010138
v  r23                     -0.0467        0.051196      3.0474e-05      0.00057459
v  epsilon                0.069113          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9912e-05       0.0099179      0.00092496       0.0017427
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017849           5.278         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.878         0.71351         0.85284


 TIME FOR THE TIME STEP            10606:        0.75881E+02

===============================================================


 INSTANT    0.106070000E-01   TIME STEP NUMBER           10607
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.540434324E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.261554308E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.222563021E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.235219929E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116448225E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81248E-03   0.45027E-02 0.19903E+01 
c  Velocity[X]                                      0.13815E-03 
c  Velocity[Y]                                      0.12774E-03 
c  Velocity[Z]                                      0.42368E-02 
c  Pressure     0.36600E-04     133   0.93169E-02   0.25816E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57666E-08   0.16286E-08 0.99278E-01 
c  r22          0.10852E-01      13   0.50098E-08   0.18515E-08 0.10169E+00 
c  r33          0.21860E-01      15   0.53080E-08   0.12644E-07 0.12728E+00 
c  r12          0.93863E-03      18   0.55028E-08   0.29691E-09 0.60119E+00 
c  r13          0.46675E-02      19   0.69422E-08   0.15180E-08 0.19974E+00 
c  r23          0.39976E-02      19   0.57411E-08   0.12834E-08 0.19807E+00 
c  epsilon      0.10969E+02      11   0.33090E-08   0.10167E-01 0.16630E+00 
c  TempC        0.25716E+06      16   0.15122E-04   0.84286E-02 0.43289E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63355         0.61358       0.0052573       0.0015076
v  Velocity[Y]            -0.57343         0.54385       0.0030806      0.00087325
v  Velocity[Z]              1.5653          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4384          4.3406          4.3632
v  Pressure                -36.406          359.99          87.633          169.82
v  r11                   0.0010607        0.081915        0.013074        0.018286
v  r22                   0.0011132        0.082631        0.013354        0.018646
v  r33                   0.0016385         0.17432         0.02725        0.037206
v  r12                   -0.010659        0.013572     -0.00023381     -0.00030931
v  r13                   -0.045539        0.052794      9.3187e-05       0.0010138
v  r23                     -0.0467        0.051222      3.0474e-05      0.00057459
v  epsilon                0.069114           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099179      0.00092496       0.0017427
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2774         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8774         0.71351         0.85284


 TIME FOR THE TIME STEP            10607:        0.90396E+02

===============================================================


 INSTANT    0.106080000E-01   TIME STEP NUMBER           10608
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.224317991E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.424205295E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.446329352E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.974512080E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110885846E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81291E-03   0.45192E-02 0.19907E+01 
c  Velocity[X]                                      0.13789E-03 
c  Velocity[Y]                                      0.12885E-03 
c  Velocity[Z]                                      0.42525E-02 
c  Pressure     0.36017E-04     133   0.91731E-02   0.25405E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55166E-08   0.16363E-08 0.10007E+00 
c  r22          0.10852E-01      13   0.52251E-08   0.18275E-08 0.10132E+00 
c  r33          0.21860E-01      15   0.58312E-08   0.12501E-07 0.12740E+00 
c  r12          0.93863E-03      18   0.54820E-08   0.29579E-09 0.60806E+00 
c  r13          0.46675E-02      19   0.60145E-08   0.14928E-08 0.19922E+00 
c  r23          0.39977E-02      19   0.62118E-08   0.12705E-08 0.19936E+00 
c  epsilon      0.10969E+02      11   0.31613E-08   0.10206E-01 0.17105E+00 
c  TempC        0.25716E+06      16   0.15171E-04   0.84241E-02 0.43291E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63368         0.61356       0.0052573       0.0015076
v  Velocity[Y]            -0.57337         0.54405       0.0030807      0.00087327
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4384          4.3406          4.3632
v  Pressure                -36.458          359.95          87.614          169.79
v  r11                   0.0010607        0.081918        0.013074        0.018286
v  r22                   0.0011132        0.082631        0.013354        0.018646
v  r33                   0.0016385         0.17435         0.02725        0.037206
v  r12                   -0.010662        0.013568     -0.00023381     -0.00030931
v  r13                   -0.045538        0.052796      9.3187e-05       0.0010138
v  r23                     -0.0467        0.051214      3.0475e-05      0.00057459
v  epsilon                0.069115          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099179      0.00092496       0.0017427
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2767         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8767         0.71351         0.85284


 TIME FOR THE TIME STEP            10608:        0.10076E+03

===============================================================


 INSTANT    0.106090000E-01   TIME STEP NUMBER           10609
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.151985676E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.113311756E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.427217956E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183047897E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208359932E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81210E-03   0.45143E-02 0.19878E+01 
c  Velocity[X]                                      0.13804E-03 
c  Velocity[Y]                                      0.12810E-03 
c  Velocity[Z]                                      0.42482E-02 
c  Pressure     0.36370E-04     132   0.92571E-02   0.25654E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56917E-08   0.16228E-08 0.99184E-01 
c  r22          0.10852E-01      13   0.53573E-08   0.18276E-08 0.10153E+00 
c  r33          0.21860E-01      15   0.60881E-08   0.12344E-07 0.12667E+00 
c  r12          0.93863E-03      19   0.55252E-08   0.29694E-09 0.60561E+00 
c  r13          0.46675E-02      19   0.60485E-08   0.14720E-08 0.19864E+00 
c  r23          0.39977E-02      19   0.58262E-08   0.12607E-08 0.19707E+00 
c  epsilon      0.10969E+02      11   0.33804E-08   0.94672E-02 0.16208E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.84322E-02 0.43297E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61356       0.0052572       0.0015076
v  Velocity[Y]            -0.57355         0.54401       0.0030807      0.00087324
v  Velocity[Z]              1.5651          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4384          4.3406          4.3632
v  Pressure                 -36.49          359.95          87.578          169.78
v  r11                   0.0010607        0.081918        0.013074        0.018286
v  r22                   0.0011132        0.082626        0.013354        0.018646
v  r33                   0.0016385         0.17433         0.02725        0.037206
v  r12                    -0.01066        0.013571     -0.00023381     -0.00030931
v  r13                   -0.045542        0.052799      9.3187e-05       0.0010138
v  r23                     -0.0467        0.051207      3.0475e-05      0.00057459
v  epsilon                0.069116          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099178      0.00092496       0.0017427
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2773         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8773         0.71351         0.85284


 TIME FOR THE TIME STEP            10609:        0.15122E+03

===============================================================


 INSTANT    0.106100000E-01   TIME STEP NUMBER           10610
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.346103696E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.652096113E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.785154179E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120769864E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.114532751E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81252E-03   0.45194E-02 0.19903E+01 
c  Velocity[X]                                      0.13868E-03 
c  Velocity[Y]                                      0.12846E-03 
c  Velocity[Z]                                      0.42523E-02 
c  Pressure     0.36372E-04     132   0.92584E-02   0.25655E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57145E-08   0.16230E-08 0.98926E-01 
c  r22          0.10852E-01      13   0.52809E-08   0.18380E-08 0.10165E+00 
c  r33          0.21860E-01      15   0.58435E-08   0.12573E-07 0.12715E+00 
c  r12          0.93863E-03      18   0.72016E-08   0.29567E-09 0.60408E+00 
c  r13          0.46675E-02      19   0.69280E-08   0.14907E-08 0.19934E+00 
c  r23          0.39977E-02      19   0.51201E-08   0.12756E-08 0.19820E+00 
c  epsilon      0.10969E+02      11   0.33423E-08   0.98616E-02 0.16443E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84314E-02 0.43322E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63386         0.61354       0.0052572       0.0015076
v  Velocity[Y]            -0.57355         0.54412       0.0030805      0.00087317
v  Velocity[Z]              1.5651          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4384          4.3406          4.3632
v  Pressure                -36.463          359.95          87.609          169.79
v  r11                   0.0010607        0.081917        0.013074        0.018286
v  r22                   0.0011132        0.082628        0.013354        0.018646
v  r33                   0.0016386         0.17429         0.02725        0.037206
v  r12                   -0.010663        0.013571     -0.00023381     -0.00030931
v  r13                   -0.045539          0.0528      9.3188e-05       0.0010138
v  r23                   -0.046699        0.051194      3.0476e-05      0.00057459
v  epsilon                0.069117          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9919e-05       0.0099178      0.00092497       0.0017427
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8783         0.71351         0.85283


 TIME FOR THE TIME STEP            10610:        0.19633E+03

===============================================================


 INSTANT    0.106110000E-01   TIME STEP NUMBER           10611
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.827676714E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149458909E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.156620495E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203916012E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178657382E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81256E-03   0.45544E-02 0.19985E+01 
c  Velocity[X]                                      0.13958E-03 
c  Velocity[Y]                                      0.12923E-03 
c  Velocity[Z]                                      0.42856E-02 
c  Pressure     0.36682E-04     132   0.93327E-02   0.25874E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57794E-08   0.15873E-08 0.98625E-01 
c  r22          0.10852E-01      13   0.51390E-08   0.17941E-08 0.10088E+00 
c  r33          0.21860E-01      15   0.51890E-08   0.12132E-07 0.12587E+00 
c  r12          0.93863E-03      18   0.65040E-08   0.29282E-09 0.60131E+00 
c  r13          0.46675E-02      19   0.69424E-08   0.14700E-08 0.19827E+00 
c  r23          0.39977E-02      19   0.55749E-08   0.12402E-08 0.19581E+00 
c  epsilon      0.10969E+02      11   0.32078E-08   0.92450E-02 0.15927E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.84211E-02 0.43283E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361         0.61355       0.0052572       0.0015076
v  Velocity[Y]            -0.57361         0.54426       0.0030806      0.00087322
v  Velocity[Z]               1.565          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4384          4.3406          4.3632
v  Pressure                -36.402          360.13          87.696          169.92
v  r11                   0.0010607        0.081916        0.013074        0.018286
v  r22                   0.0011132        0.082629        0.013354        0.018646
v  r33                   0.0016386         0.17431         0.02725        0.037206
v  r12                   -0.010662        0.013574     -0.00023381     -0.00030931
v  r13                   -0.045539        0.052797      9.3188e-05       0.0010138
v  r23                   -0.046699        0.051217      3.0477e-05      0.00057459
v  epsilon                0.069117          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099177      0.00092497       0.0017427
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2787         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8787         0.71351         0.85284


 TIME FOR THE TIME STEP            10611:        0.18982E+03

===============================================================


 INSTANT    0.106120000E-01   TIME STEP NUMBER           10612
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.828724701E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.219673323E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.155041967E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.137535252E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.504375291E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81297E-03   0.44926E-02 0.19842E+01 
c  Velocity[X]                                      0.13811E-03 
c  Velocity[Y]                                      0.12746E-03 
c  Velocity[Z]                                      0.42270E-02 
c  Pressure     0.36529E-04     132   0.92954E-02   0.25766E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56778E-08   0.16110E-08 0.98668E-01 
c  r22          0.10852E-01      13   0.52985E-08   0.18170E-08 0.10105E+00 
c  r33          0.21860E-01      14   0.70233E-08   0.12402E-07 0.12645E+00 
c  r12          0.93863E-03      18   0.65220E-08   0.30153E-09 0.60476E+00 
c  r13          0.46675E-02      19   0.63160E-08   0.14782E-08 0.19852E+00 
c  r23          0.39977E-02      19   0.56292E-08   0.12704E-08 0.19790E+00 
c  epsilon      0.10969E+02      11   0.30982E-08   0.98283E-02 0.16431E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.84146E-02 0.43294E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63363         0.61356       0.0052573       0.0015076
v  Velocity[Y]            -0.57361          0.5441       0.0030806      0.00087317
v  Velocity[Z]              1.5649          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5787          5.4384          4.3406          4.3632
v  Pressure                -36.484          360.07           87.67          169.88
v  r11                   0.0010607        0.081912        0.013074        0.018286
v  r22                   0.0011132         0.08263        0.013354        0.018646
v  r33                   0.0016386         0.17434         0.02725        0.037206
v  r12                   -0.010668         0.01357     -0.00023381     -0.00030931
v  r13                   -0.045541        0.052796      9.3188e-05       0.0010138
v  r23                     -0.0467        0.051202      3.0477e-05      0.00057459
v  epsilon                0.069118          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099176      0.00092497       0.0017427
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8786         0.71351         0.85284


 TIME FOR THE TIME STEP            10612:        0.20387E+03

===============================================================


 INSTANT    0.106130000E-01   TIME STEP NUMBER           10613
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.487788653E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.819430551E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.575243936E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.366487289E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.388354773E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81225E-03   0.45202E-02 0.19911E+01 
c  Velocity[X]                                      0.13862E-03 
c  Velocity[Y]                                      0.12889E-03 
c  Velocity[Z]                                      0.42527E-02 
c  Pressure     0.36248E-04     133   0.92303E-02   0.25569E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58888E-08   0.16239E-08 0.99194E-01 
c  r22          0.10852E-01      13   0.49901E-08   0.18297E-08 0.10161E+00 
c  r33          0.21860E-01      15   0.53465E-08   0.12506E-07 0.12702E+00 
c  r12          0.93863E-03      18   0.64127E-08   0.29893E-09 0.60475E+00 
c  r13          0.46675E-02      19   0.60400E-08   0.15190E-08 0.20095E+00 
c  r23          0.39977E-02      19   0.58851E-08   0.12803E-08 0.19847E+00 
c  epsilon      0.10969E+02      11   0.32454E-08   0.98928E-02 0.16447E+00 
c  TempC        0.25716E+06      16   0.15142E-04   0.83802E-02 0.43219E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61353       0.0052573       0.0015076
v  Velocity[Y]            -0.57359         0.54405       0.0030806      0.00087318
v  Velocity[Z]               1.565          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4384          4.3406          4.3632
v  Pressure                -36.426          360.01          87.645          169.84
v  r11                   0.0010607        0.081907        0.013074        0.018286
v  r22                   0.0011132         0.08263        0.013354        0.018646
v  r33                   0.0016386         0.17431        0.027251        0.037206
v  r12                   -0.010667        0.013574     -0.00023381     -0.00030931
v  r13                   -0.045541        0.052797      9.3188e-05       0.0010138
v  r23                   -0.046699        0.051199      3.0477e-05      0.00057459
v  epsilon                0.069119          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099176      0.00092497       0.0017427
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2782         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8782         0.71351         0.85284


 TIME FOR THE TIME STEP            10613:        0.24069E+03

===============================================================


 INSTANT    0.106140000E-01   TIME STEP NUMBER           10614
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.355437087E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130796101E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.171400976E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.482437813E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.465631024E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81260E-03   0.45207E-02 0.19912E+01 
c  Velocity[X]                                      0.13831E-03 
c  Velocity[Y]                                      0.12944E-03 
c  Velocity[Z]                                      0.42530E-02 
c  Pressure     0.36262E-04     132   0.92267E-02   0.25578E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58517E-08   0.16555E-08 0.99930E-01 
c  r22          0.10852E-01      13   0.54475E-08   0.18154E-08 0.10143E+00 
c  r33          0.21860E-01      15   0.54053E-08   0.12625E-07 0.12779E+00 
c  r12          0.93863E-03      18   0.66230E-08   0.30369E-09 0.60808E+00 
c  r13          0.46675E-02      19   0.64089E-08   0.14860E-08 0.19971E+00 
c  r23          0.39977E-02      19   0.57654E-08   0.13104E-08 0.20110E+00 
c  epsilon      0.10969E+02      11   0.33534E-08   0.10175E-01 0.17035E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.84185E-02 0.43233E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63366         0.61353       0.0052573       0.0015077
v  Velocity[Y]            -0.57343         0.54411       0.0030806      0.00087319
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4384          4.3406          4.3632
v  Pressure                -36.442          359.93          87.584          169.77
v  r11                   0.0010608        0.081905        0.013074        0.018286
v  r22                   0.0011133        0.082631        0.013354        0.018646
v  r33                   0.0016386         0.17428        0.027251        0.037206
v  r12                   -0.010666        0.013575     -0.00023381     -0.00030931
v  r13                   -0.045539        0.052798      9.3188e-05       0.0010138
v  r23                   -0.046698        0.051198      3.0478e-05      0.00057459
v  epsilon                 0.06912          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099176      0.00092497       0.0017427
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2776         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8776         0.71351         0.85283


 TIME FOR THE TIME STEP            10614:        0.27258E+03

===============================================================


 INSTANT    0.106150000E-01   TIME STEP NUMBER           10615
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.162591829E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.690384397E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181722122E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.113207000E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.159150461E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81242E-03   0.45185E-02 0.19916E+01 
c  Velocity[X]                                      0.13817E-03 
c  Velocity[Y]                                      0.12749E-03 
c  Velocity[Z]                                      0.42529E-02 
c  Pressure     0.36764E-04     133   0.93618E-02   0.25932E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59448E-08   0.16193E-08 0.99408E-01 
c  r22          0.10852E-01      13   0.54563E-08   0.18015E-08 0.10091E+00 
c  r33          0.21860E-01      15   0.51420E-08   0.12291E-07 0.12622E+00 
c  r12          0.93863E-03      18   0.68542E-08   0.29336E-09 0.60354E+00 
c  r13          0.46675E-02      19   0.68409E-08   0.14739E-08 0.19839E+00 
c  r23          0.39977E-02      19   0.62985E-08   0.12609E-08 0.19686E+00 
c  epsilon      0.10969E+02      11   0.32987E-08   0.96697E-02 0.16336E+00 
c  TempC        0.25716E+06      16   0.15092E-04   0.84396E-02 0.43280E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63362         0.61357       0.0052573       0.0015076
v  Velocity[Y]            -0.57345         0.54421       0.0030806      0.00087319
v  Velocity[Z]              1.5651          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4384          4.3406          4.3632
v  Pressure                 -36.45          360.02          87.628          169.84
v  r11                   0.0010608         0.08191        0.013074        0.018286
v  r22                   0.0011133        0.082631        0.013354        0.018646
v  r33                   0.0016387          0.1743        0.027251        0.037206
v  r12                   -0.010663        0.013573     -0.00023381     -0.00030931
v  r13                   -0.045542        0.052796      9.3188e-05       0.0010138
v  r23                   -0.046697        0.051222      3.0478e-05      0.00057459
v  epsilon                0.069121          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099176      0.00092497       0.0017427
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2769         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8769         0.71351         0.85283


 TIME FOR THE TIME STEP            10615:        0.26100E+03

===============================================================


 INSTANT    0.106160000E-01   TIME STEP NUMBER           10616
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.969222289E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150876342E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.312965762E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.236353180E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140382426E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81313E-03   0.45067E-02 0.19874E+01 
c  Velocity[X]                                      0.13832E-03 
c  Velocity[Y]                                      0.12822E-03 
c  Velocity[Z]                                      0.42401E-02 
c  Pressure     0.36165E-04     131   0.92116E-02   0.25509E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60362E-08   0.16048E-08 0.98858E-01 
c  r22          0.10852E-01      13   0.54714E-08   0.18088E-08 0.10134E+00 
c  r33          0.21860E-01      15   0.57023E-08   0.12321E-07 0.12673E+00 
c  r12          0.93863E-03      18   0.73114E-08   0.30089E-09 0.60642E+00 
c  r13          0.46675E-02      19   0.62732E-08   0.14937E-08 0.19980E+00 
c  r23          0.39977E-02      19   0.66083E-08   0.12696E-08 0.19802E+00 
c  epsilon      0.10969E+02      11   0.32984E-08   0.93764E-02 0.16104E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.83913E-02 0.43272E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63366         0.61356       0.0052573       0.0015076
v  Velocity[Y]            -0.57344         0.54429       0.0030806      0.00087319
v  Velocity[Z]              1.5649          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4384          4.3406          4.3632
v  Pressure                -36.457          360.02          87.661          169.85
v  r11                   0.0010608        0.081914        0.013074        0.018286
v  r22                   0.0011133         0.08263        0.013354        0.018646
v  r33                   0.0016387         0.17432        0.027251        0.037206
v  r12                   -0.010664        0.013581     -0.00023381     -0.00030931
v  r13                   -0.045539        0.052796      9.3188e-05       0.0010138
v  r23                   -0.046697        0.051209      3.0478e-05      0.00057459
v  epsilon                0.069122           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099176      0.00092497       0.0017427
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2778         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8778         0.71351         0.85284


 TIME FOR THE TIME STEP            10616:        0.21366E+03

===============================================================


 INSTANT    0.106170000E-01   TIME STEP NUMBER           10617
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.821416132E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117367009E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.104583189E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.703621305E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.327649327E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81159E-03   0.45394E-02 0.19948E+01 
c  Velocity[X]                                      0.13855E-03 
c  Velocity[Y]                                      0.12867E-03 
c  Velocity[Z]                                      0.42721E-02 
c  Pressure     0.36709E-04     132   0.93445E-02   0.25893E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54836E-08   0.16224E-08 0.99708E-01 
c  r22          0.10852E-01      13   0.53026E-08   0.18102E-08 0.10118E+00 
c  r33          0.21860E-01      15   0.51871E-08   0.12351E-07 0.12699E+00 
c  r12          0.93863E-03      18   0.66039E-08   0.29423E-09 0.60390E+00 
c  r13          0.46675E-02      19   0.61086E-08   0.14769E-08 0.19885E+00 
c  r23          0.39977E-02      19   0.55123E-08   0.12522E-08 0.19763E+00 
c  epsilon      0.10969E+02      11   0.33264E-08   0.95888E-02 0.16236E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84354E-02 0.43375E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63371         0.61357       0.0052573       0.0015076
v  Velocity[Y]            -0.57363         0.54408       0.0030806       0.0008732
v  Velocity[Z]               1.565          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4384          4.3406          4.3632
v  Pressure                -36.433          360.01          87.637          169.85
v  r11                   0.0010608        0.081915        0.013074        0.018286
v  r22                   0.0011133        0.082626        0.013354        0.018646
v  r33                   0.0016387         0.17435        0.027251        0.037206
v  r12                   -0.010666        0.013577     -0.00023381     -0.00030931
v  r13                   -0.045539        0.052796      9.3189e-05       0.0010138
v  r23                   -0.046696          0.0512      3.0479e-05      0.00057459
v  epsilon                0.069122          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099177      0.00092497       0.0017427
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017849           5.278         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.878         0.71351         0.85284


 TIME FOR THE TIME STEP            10617:        0.20409E+03

===============================================================


 INSTANT    0.106180000E-01   TIME STEP NUMBER           10618
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150920859E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.861747943E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.170585303E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935015E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.771877632E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.309060524E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81275E-03   0.45341E-02 0.19926E+01 
c  Velocity[X]                                      0.13823E-03 
c  Velocity[Y]                                      0.12964E-03 
c  Velocity[Z]                                      0.42662E-02 
c  Pressure     0.36202E-04     133   0.92177E-02   0.25535E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58464E-08   0.16884E-08 0.10077E+00 
c  r22          0.10852E-01      13   0.54253E-08   0.18812E-08 0.10286E+00 
c  r33          0.21860E-01      15   0.61179E-08   0.12981E-07 0.12943E+00 
c  r12          0.93863E-03      18   0.61198E-08   0.30956E-09 0.61791E+00 
c  r13          0.46675E-02      19   0.69693E-08   0.15047E-08 0.20078E+00 
c  r23          0.39977E-02      19   0.59892E-08   0.13385E-08 0.20393E+00 
c  epsilon      0.10969E+02      11   0.34772E-08   0.99836E-02 0.16638E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.83637E-02 0.43099E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364         0.61358       0.0052572       0.0015076
v  Velocity[Y]            -0.57354         0.54414       0.0030806      0.00087317
v  Velocity[Z]              1.5653          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4384          4.3406          4.3632
v  Pressure                -36.467          359.99          87.621          169.82
v  r11                   0.0010608        0.081918        0.013074        0.018286
v  r22                   0.0011133        0.082628        0.013354        0.018646
v  r33                   0.0016387         0.17433        0.027251        0.037206
v  r12                   -0.010662        0.013582     -0.00023381     -0.00030931
v  r13                   -0.045541        0.052798      9.3189e-05       0.0010138
v  r23                   -0.046696        0.051219      3.0479e-05      0.00057459
v  epsilon                0.069123          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099178      0.00092497       0.0017427
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8783         0.71351         0.85283


 TIME FOR THE TIME STEP            10618:        0.13253E+03

===============================================================


 INSTANT    0.106190000E-01   TIME STEP NUMBER           10619
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.148237098E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.206997822E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249655806E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.651670975E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.121333963E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81241E-03   0.45034E-02 0.19889E+01 
c  Velocity[X]                                      0.13739E-03 
c  Velocity[Y]                                      0.12762E-03 
c  Velocity[Z]                                      0.42384E-02 
c  Pressure     0.36244E-04     131   0.92212E-02   0.25565E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55230E-08   0.16535E-08 0.10009E+00 
c  r22          0.10852E-01      13   0.54290E-08   0.18441E-08 0.10157E+00 
c  r33          0.21860E-01      15   0.66168E-08   0.12620E-07 0.12753E+00 
c  r12          0.93863E-03      18   0.57855E-08   0.29884E-09 0.60820E+00 
c  r13          0.46675E-02      19   0.67911E-08   0.14929E-08 0.19950E+00 
c  r23          0.39977E-02      19   0.52526E-08   0.12745E-08 0.19860E+00 
c  epsilon      0.10969E+02      11   0.33935E-08   0.99259E-02 0.16447E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84407E-02 0.43290E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63365         0.61357       0.0052574       0.0015076
v  Velocity[Y]            -0.57365          0.5443       0.0030806       0.0008732
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4384          4.3406          4.3632
v  Pressure                -36.383          360.05          87.652          169.87
v  r11                   0.0010608        0.081914        0.013074        0.018286
v  r22                   0.0011133        0.082629        0.013354        0.018646
v  r33                   0.0016388          0.1743        0.027251        0.037206
v  r12                   -0.010662        0.013582     -0.00023381     -0.00030931
v  r13                   -0.045539        0.052795      9.3189e-05       0.0010138
v  r23                   -0.046696        0.051209      3.0479e-05      0.00057459
v  epsilon                0.069124          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099179      0.00092497       0.0017427
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2785         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8785         0.71351         0.85283


 TIME FOR THE TIME STEP            10619:        0.82171E+02

===============================================================


 INSTANT    0.106200000E-01   TIME STEP NUMBER           10620
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.452412246E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.287823756E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.517385995E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.881188517E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.158913958E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81182E-03   0.45192E-02 0.19902E+01 
c  Velocity[X]                                      0.13829E-03 
c  Velocity[Y]                                      0.12743E-03 
c  Velocity[Z]                                      0.42534E-02 
c  Pressure     0.36135E-04     132   0.92089E-02   0.25488E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61079E-08   0.16346E-08 0.99617E-01 
c  r22          0.10852E-01      13   0.53736E-08   0.18323E-08 0.10147E+00 
c  r33          0.21860E-01      15   0.63097E-08   0.12626E-07 0.12780E+00 
c  r12          0.93863E-03      18   0.58933E-08   0.29672E-09 0.60347E+00 
c  r13          0.46675E-02      19   0.66549E-08   0.15298E-08 0.20043E+00 
c  r23          0.39977E-02      19   0.54729E-08   0.12974E-08 0.20020E+00 
c  epsilon      0.10969E+02      11   0.33405E-08   0.10256E-01 0.17101E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.84204E-02 0.43322E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61355       0.0052573       0.0015076
v  Velocity[Y]            -0.57356          0.5442       0.0030806      0.00087319
v  Velocity[Z]              1.5654          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4384          4.3406          4.3632
v  Pressure                -36.465          359.96          87.618           169.8
v  r11                   0.0010608        0.081909        0.013074        0.018286
v  r22                   0.0011133         0.08263        0.013354        0.018646
v  r33                   0.0016388         0.17431        0.027251        0.037206
v  r12                   -0.010662        0.013578     -0.00023381     -0.00030931
v  r13                   -0.045538        0.052795      9.3189e-05       0.0010138
v  r23                   -0.046696        0.051202      3.0479e-05      0.00057459
v  epsilon                0.069125          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099179      0.00092498       0.0017427
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2784         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8784         0.71351         0.85284


 TIME FOR THE TIME STEP            10620:        0.81908E+02

===============================================================


 INSTANT    0.106210000E-01   TIME STEP NUMBER           10621
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190542561E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.816917059E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138023919E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.890588461E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.225897881E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81322E-03   0.45095E-02 0.19891E+01 
c  Velocity[X]                                      0.13768E-03 
c  Velocity[Y]                                      0.12879E-03 
c  Velocity[Z]                                      0.42430E-02 
c  Pressure     0.36454E-04     133   0.92768E-02   0.25714E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58988E-08   0.16569E-08 0.10002E+00 
c  r22          0.10852E-01      13   0.48441E-08   0.18151E-08 0.10125E+00 
c  r33          0.21860E-01      15   0.58514E-08   0.12510E-07 0.12711E+00 
c  r12          0.93863E-03      18   0.53478E-08   0.29619E-09 0.60419E+00 
c  r13          0.46675E-02      19   0.66157E-08   0.14849E-08 0.19888E+00 
c  r23          0.39977E-02      19   0.53797E-08   0.12813E-08 0.19923E+00 
c  epsilon      0.10969E+02      11   0.33797E-08   0.99157E-02 0.16513E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.83747E-02 0.43185E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63359         0.61359       0.0052574       0.0015077
v  Velocity[Y]            -0.57363         0.54409       0.0030806      0.00087321
v  Velocity[Z]              1.5651          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4384          4.3406          4.3632
v  Pressure                -36.412             360          87.619          169.83
v  r11                   0.0010608        0.081908        0.013074        0.018286
v  r22                   0.0011134        0.082631        0.013354        0.018646
v  r33                   0.0016388         0.17433        0.027251        0.037206
v  r12                   -0.010658        0.013579     -0.00023381     -0.00030931
v  r13                   -0.045542        0.052797      9.3189e-05       0.0010138
v  r23                   -0.046696        0.051228       3.048e-05      0.00057459
v  epsilon                0.069126           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05        0.009918      0.00092498       0.0017427
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2782         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8782          0.7135         0.85283


 TIME FOR THE TIME STEP            10621:        0.81297E+02

===============================================================


 INSTANT    0.106220000E-01   TIME STEP NUMBER           10622
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.281040300E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.537328137E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934900E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.164139973E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.309350316E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.216309509E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81214E-03   0.45365E-02 0.19948E+01 
c  Velocity[X]                                      0.13774E-03 
c  Velocity[Y]                                      0.12803E-03 
c  Velocity[Z]                                      0.42708E-02 
c  Pressure     0.36670E-04     133   0.93439E-02   0.25866E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58009E-08   0.16468E-08 0.99746E-01 
c  r22          0.10852E-01      13   0.50733E-08   0.18011E-08 0.10113E+00 
c  r33          0.21860E-01      15   0.53124E-08   0.12472E-07 0.12729E+00 
c  r12          0.93863E-03      18   0.62847E-08   0.29490E-09 0.60353E+00 
c  r13          0.46675E-02      19   0.67871E-08   0.14649E-08 0.19861E+00 
c  r23          0.39977E-02      19   0.58478E-08   0.12859E-08 0.19960E+00 
c  epsilon      0.10969E+02      11   0.33488E-08   0.98850E-02 0.16642E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.84240E-02 0.43269E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63359         0.61358       0.0052573       0.0015076
v  Velocity[Y]            -0.57371         0.54418       0.0030805      0.00087317
v  Velocity[Z]              1.5654          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4384          4.3406          4.3632
v  Pressure                -36.441          360.05           87.68          169.88
v  r11                   0.0010608        0.081912        0.013074        0.018286
v  r22                   0.0011134        0.082632        0.013354        0.018646
v  r33                   0.0016388          0.1743        0.027251        0.037206
v  r12                   -0.010659        0.013581     -0.00023381     -0.00030931
v  r13                   -0.045539        0.052798       9.319e-05       0.0010138
v  r23                   -0.046696        0.051215      3.0479e-05      0.00057459
v  epsilon                0.069127          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05        0.009918      0.00092498       0.0017427
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017849           5.278         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.878         0.71351         0.85284


 TIME FOR THE TIME STEP            10622:        0.75173E+02

===============================================================


 INSTANT    0.106230000E-01   TIME STEP NUMBER           10623
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.228708871E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.674216626E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.586661549E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.269081142E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.965945430E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81217E-03   0.45288E-02 0.19951E+01 
c  Velocity[X]                                      0.13857E-03 
c  Velocity[Y]                                      0.12864E-03 
c  Velocity[Z]                                      0.42616E-02 
c  Pressure     0.36152E-04     132   0.92019E-02   0.25501E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56613E-08   0.16216E-08 0.99166E-01 
c  r22          0.10852E-01      13   0.54769E-08   0.17931E-08 0.10033E+00 
c  r33          0.21860E-01      15   0.58697E-08   0.12322E-07 0.12637E+00 
c  r12          0.93863E-03      19   0.60411E-08   0.29133E-09 0.60226E+00 
c  r13          0.46675E-02      19   0.60877E-08   0.14494E-08 0.19718E+00 
c  r23          0.39977E-02      19   0.64704E-08   0.12632E-08 0.19823E+00 
c  epsilon      0.10969E+02      11   0.32433E-08   0.97319E-02 0.16445E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.84759E-02 0.43454E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61356       0.0052573       0.0015076
v  Velocity[Y]            -0.57374         0.54427       0.0030806      0.00087321
v  Velocity[Z]              1.5654          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4384          4.3406          4.3632
v  Pressure                -36.403             360          87.626          169.83
v  r11                   0.0010608        0.081911        0.013074        0.018286
v  r22                   0.0011134        0.082632        0.013354        0.018646
v  r33                   0.0016389         0.17429        0.027251        0.037206
v  r12                   -0.010656        0.013577     -0.00023381     -0.00030931
v  r13                   -0.045537        0.052795      9.3189e-05       0.0010138
v  r23                   -0.046695        0.051207       3.048e-05      0.00057459
v  epsilon                0.069127          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9933e-05       0.0099179      0.00092498       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2771         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8771         0.71351         0.85284


 TIME FOR THE TIME STEP            10623:        0.79213E+02

===============================================================


 INSTANT    0.106240000E-01   TIME STEP NUMBER           10624
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150307050E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.167639463E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.555950813E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166052171E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.387037162E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81372E-03   0.45003E-02 0.19877E+01 
c  Velocity[X]                                      0.13788E-03 
c  Velocity[Y]                                      0.12917E-03 
c  Velocity[Z]                                      0.42332E-02 
c  Pressure     0.36227E-04     131   0.92239E-02   0.25553E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60220E-08   0.16476E-08 0.99631E-01 
c  r22          0.10852E-01      13   0.56546E-08   0.18503E-08 0.10166E+00 
c  r33          0.21860E-01      15   0.68849E-08   0.12667E-07 0.12774E+00 
c  r12          0.93863E-03      19   0.67780E-08   0.29839E-09 0.60517E+00 
c  r13          0.46675E-02      19   0.60438E-08   0.15047E-08 0.19947E+00 
c  r23          0.39977E-02      19   0.59740E-08   0.12788E-08 0.19908E+00 
c  epsilon      0.10969E+02      11   0.33505E-08   0.10127E-01 0.16797E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.84125E-02 0.43264E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334          0.6136       0.0052573       0.0015076
v  Velocity[Y]            -0.57372         0.54411       0.0030805      0.00087318
v  Velocity[Z]              1.5653          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4384          4.3406          4.3632
v  Pressure                -36.456          360.05           87.67          169.88
v  r11                   0.0010608         0.08191        0.013074        0.018286
v  r22                   0.0011134        0.082632        0.013354        0.018646
v  r33                   0.0016389          0.1743        0.027251        0.037206
v  r12                   -0.010655        0.013573     -0.00023381     -0.00030931
v  r13                    -0.04554        0.052796       9.319e-05       0.0010138
v  r23                   -0.046695        0.051224       3.048e-05      0.00057459
v  epsilon                0.069128          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099179      0.00092498       0.0017427
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2763         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8763         0.71351         0.85283


 TIME FOR THE TIME STEP            10624:        0.77242E+02

===============================================================


 INSTANT    0.106250000E-01   TIME STEP NUMBER           10625
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.121796213E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.561746341E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.211545005E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.143195713E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.286751456E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81158E-03   0.45101E-02 0.19868E+01 
c  Velocity[X]                                      0.13793E-03 
c  Velocity[Y]                                      0.12759E-03 
c  Velocity[Z]                                      0.42445E-02 
c  Pressure     0.36295E-04     131   0.92409E-02   0.25601E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60346E-08   0.16298E-08 0.99338E-01 
c  r22          0.10852E-01      13   0.57385E-08   0.18219E-08 0.10164E+00 
c  r33          0.21860E-01      15   0.69300E-08   0.12470E-07 0.12724E+00 
c  r12          0.93863E-03      19   0.64377E-08   0.29196E-09 0.60231E+00 
c  r13          0.46675E-02      19   0.67332E-08   0.14913E-08 0.20024E+00 
c  r23          0.39977E-02      19   0.65954E-08   0.12792E-08 0.19837E+00 
c  epsilon      0.10969E+02      11   0.34007E-08   0.97669E-02 0.16415E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.83974E-02 0.43204E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61355       0.0052572       0.0015075
v  Velocity[Y]            -0.57383         0.54407       0.0030805      0.00087314
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4384          4.3406          4.3632
v  Pressure                -36.392             360          87.634          169.83
v  r11                   0.0010608         0.08191        0.013074        0.018286
v  r22                   0.0011134         0.08263        0.013354        0.018646
v  r33                   0.0016389         0.17432        0.027251        0.037206
v  r12                   -0.010661        0.013576     -0.00023381     -0.00030931
v  r13                   -0.045539        0.052795       9.319e-05       0.0010138
v  r23                   -0.046696        0.051219      3.0481e-05      0.00057459
v  epsilon                0.069129          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05        0.009918      0.00092498       0.0017427
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2759         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8759         0.71351         0.85284


 TIME FOR THE TIME STEP            10625:        0.78451E+02

===============================================================


 INSTANT    0.106260000E-01   TIME STEP NUMBER           10626
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.338677223E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.219758248E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.679514890E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130999137E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.223730532E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81284E-03   0.45332E-02 0.19945E+01 
c  Velocity[X]                                      0.13896E-03 
c  Velocity[Y]                                      0.12865E-03 
c  Velocity[Z]                                      0.42656E-02 
c  Pressure     0.36224E-04     133   0.92269E-02   0.25552E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56511E-08   0.16536E-08 0.10031E+00 
c  r22          0.10852E-01      13   0.52450E-08   0.18421E-08 0.10209E+00 
c  r33          0.21860E-01      15   0.61725E-08   0.12705E-07 0.12880E+00 
c  r12          0.93863E-03      19   0.56720E-08   0.30827E-09 0.61278E+00 
c  r13          0.46675E-02      19   0.61711E-08   0.15004E-08 0.20079E+00 
c  r23          0.39977E-02      19   0.55493E-08   0.13050E-08 0.20164E+00 
c  epsilon      0.10969E+02      11   0.32813E-08   0.10232E-01 0.17170E+00 
c  TempC        0.25716E+06      16   0.15180E-04   0.84035E-02 0.43213E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61358       0.0052574       0.0015076
v  Velocity[Y]            -0.57367         0.54415       0.0030805      0.00087313
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4384          4.3406          4.3632
v  Pressure                 -36.42          360.05          87.676          169.88
v  r11                   0.0010608        0.081914        0.013074        0.018286
v  r22                   0.0011134         0.08263        0.013354        0.018646
v  r33                   0.0016389          0.1743        0.027251        0.037206
v  r12                   -0.010662        0.013577     -0.00023381     -0.00030931
v  r13                   -0.045538        0.052796      9.3191e-05       0.0010138
v  r23                   -0.046697        0.051208      3.0481e-05      0.00057459
v  epsilon                 0.06913          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099177      0.00092498       0.0017427
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2758         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8758         0.71351         0.85283


 TIME FOR THE TIME STEP            10626:        0.76841E+02

===============================================================


 INSTANT    0.106270000E-01   TIME STEP NUMBER           10627
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.261067481E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117119592E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.671199982E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.593887803E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.520140016E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81283E-03   0.45059E-02 0.19874E+01 
c  Velocity[X]                                      0.13927E-03 
c  Velocity[Y]                                      0.12736E-03 
c  Velocity[Z]                                      0.42393E-02 
c  Pressure     0.36212E-04     133   0.92151E-02   0.25542E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52669E-08   0.16800E-08 0.10047E+00 
c  r22          0.10852E-01      13   0.50837E-08   0.18526E-08 0.10188E+00 
c  r33          0.21860E-01      15   0.54306E-08   0.12814E-07 0.12847E+00 
c  r12          0.93863E-03      18   0.70345E-08   0.30630E-09 0.61515E+00 
c  r13          0.46675E-02      19   0.53270E-08   0.14914E-08 0.19909E+00 
c  r23          0.39977E-02      19   0.56731E-08   0.13025E-08 0.20100E+00 
c  epsilon      0.10969E+02      11   0.33963E-08   0.10132E-01 0.16799E+00 
c  TempC        0.25716E+06      16   0.15098E-04   0.84160E-02 0.43283E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61361       0.0052573       0.0015076
v  Velocity[Y]            -0.57374         0.54429       0.0030806      0.00087315
v  Velocity[Z]              1.5651          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4384          4.3406          4.3632
v  Pressure                -36.445          360.03          87.639          169.85
v  r11                   0.0010609        0.081918        0.013074        0.018286
v  r22                   0.0011134        0.082629        0.013354        0.018646
v  r33                    0.001639         0.17428        0.027251        0.037206
v  r12                   -0.010658        0.013576     -0.00023381     -0.00030931
v  r13                    -0.04554        0.052794      9.3191e-05       0.0010138
v  r23                   -0.046698        0.051225      3.0481e-05      0.00057459
v  epsilon                0.069131          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099179      0.00092498       0.0017427
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2772         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8772         0.71351         0.85283


 TIME FOR THE TIME STEP            10627:        0.75330E+02

===============================================================


 INSTANT    0.106280000E-01   TIME STEP NUMBER           10628
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.419606247E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.895663352E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.306858913E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.892787004E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.768676267E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81295E-03   0.45071E-02 0.19881E+01 
c  Velocity[X]                                      0.13701E-03 
c  Velocity[Y]                                      0.12875E-03 
c  Velocity[Z]                                      0.42414E-02 
c  Pressure     0.36364E-04     133   0.92604E-02   0.25650E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53441E-08   0.16243E-08 0.99343E-01 
c  r22          0.10852E-01      13   0.53967E-08   0.18217E-08 0.10158E+00 
c  r33          0.21860E-01      15   0.61701E-08   0.12470E-07 0.12742E+00 
c  r12          0.93864E-03      18   0.70033E-08   0.29984E-09 0.60753E+00 
c  r13          0.46675E-02      19   0.59821E-08   0.14883E-08 0.19959E+00 
c  r23          0.39977E-02      19   0.55349E-08   0.12748E-08 0.19938E+00 
c  epsilon      0.10969E+02      11   0.34515E-08   0.98327E-02 0.16456E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.83931E-02 0.43234E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61354       0.0052573       0.0015076
v  Velocity[Y]            -0.57378         0.54411       0.0030805      0.00087312
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4384          4.3406          4.3632
v  Pressure                -36.481          359.99          87.624          169.82
v  r11                   0.0010609        0.081918        0.013074        0.018286
v  r22                   0.0011134        0.082629        0.013354        0.018646
v  r33                    0.001639         0.17428        0.027251        0.037206
v  r12                   -0.010656        0.013572     -0.00023381     -0.00030931
v  r13                   -0.045538        0.052797       9.319e-05       0.0010138
v  r23                   -0.046699        0.051208      3.0481e-05      0.00057459
v  epsilon                0.069131          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099179      0.00092498       0.0017427
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2776         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8776         0.71351         0.85283


 TIME FOR THE TIME STEP            10628:        0.76373E+02

===============================================================


 INSTANT    0.106290000E-01   TIME STEP NUMBER           10629
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283476836E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.224162297E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.366957922E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.128946637E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.781204626E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81144E-03   0.45398E-02 0.19947E+01 
c  Velocity[X]                                      0.13784E-03 
c  Velocity[Y]                                      0.12886E-03 
c  Velocity[Z]                                      0.42731E-02 
c  Pressure     0.36262E-04     133   0.92365E-02   0.25578E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55328E-08   0.16920E-08 0.10099E+00 
c  r22          0.10852E-01      13   0.55669E-08   0.18594E-08 0.10231E+00 
c  r33          0.21860E-01      15   0.63165E-08   0.12901E-07 0.12933E+00 
c  r12          0.93864E-03      18   0.66468E-08   0.31494E-09 0.62056E+00 
c  r13          0.46675E-02      19   0.56954E-08   0.14958E-08 0.19958E+00 
c  r23          0.39977E-02      19   0.58049E-08   0.13156E-08 0.20275E+00 
c  epsilon      0.10969E+02      11   0.34847E-08   0.10197E-01 0.16769E+00 
c  TempC        0.25716E+06      16   0.15169E-04   0.84728E-02 0.43421E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61361       0.0052574       0.0015076
v  Velocity[Y]            -0.57378         0.54418       0.0030806      0.00087317
v  Velocity[Z]              1.5654          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4384          4.3406          4.3632
v  Pressure                -36.401          360.03          87.639          169.85
v  r11                   0.0010609        0.081915        0.013074        0.018286
v  r22                   0.0011134        0.082629        0.013354        0.018646
v  r33                    0.001639         0.17431        0.027251        0.037206
v  r12                   -0.010651        0.013577     -0.00023381     -0.00030931
v  r13                   -0.045539        0.052797       9.319e-05       0.0010138
v  r23                   -0.046699        0.051201      3.0481e-05      0.00057459
v  epsilon                0.069132          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099179      0.00092498       0.0017427
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2774         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8774         0.71351         0.85283


 TIME FOR THE TIME STEP            10629:        0.74821E+02

===============================================================


 INSTANT    0.106300000E-01   TIME STEP NUMBER           10630
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.380535091E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201669356E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145409018E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.418165184E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.437953653E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81241E-03   0.44771E-02 0.19832E+01 
c  Velocity[X]                                      0.13711E-03 
c  Velocity[Y]                                      0.12872E-03 
c  Velocity[Z]                                      0.42113E-02 
c  Pressure     0.36178E-04     133   0.92074E-02   0.25519E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53873E-08   0.16989E-08 0.10134E+00 
c  r22          0.10852E-01      13   0.59473E-08   0.18913E-08 0.10298E+00 
c  r33          0.21860E-01      15   0.64125E-08   0.13039E-07 0.13005E+00 
c  r12          0.93864E-03      18   0.72297E-08   0.30794E-09 0.61700E+00 
c  r13          0.46675E-02      19   0.60670E-08   0.15287E-08 0.20121E+00 
c  r23          0.39977E-02      19   0.66554E-08   0.13126E-08 0.20301E+00 
c  epsilon      0.10969E+02      11   0.33676E-08   0.10281E-01 0.16845E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84005E-02 0.43236E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61359       0.0052573       0.0015076
v  Velocity[Y]            -0.57366         0.54388       0.0030805      0.00087312
v  Velocity[Z]              1.5651          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4384          4.3406          4.3632
v  Pressure                -36.435          360.02          87.643          169.84
v  r11                   0.0010609        0.081918        0.013074        0.018286
v  r22                   0.0011135        0.082626        0.013354        0.018646
v  r33                    0.001639          0.1743        0.027251        0.037206
v  r12                   -0.010652        0.013573     -0.00023381     -0.00030931
v  r13                   -0.045541        0.052799      9.3191e-05       0.0010138
v  r23                   -0.046699        0.051219      3.0482e-05      0.00057459
v  epsilon                0.069133          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099179      0.00092499       0.0017427
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2782         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8782         0.71351         0.85283


 TIME FOR THE TIME STEP            10630:        0.77239E+02

===============================================================


 INSTANT    0.106310000E-01   TIME STEP NUMBER           10631
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.907455040E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.115563773E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.645571065E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.336072152E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.302318754E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81279E-03   0.45316E-02 0.19936E+01 
c  Velocity[X]                                      0.13824E-03 
c  Velocity[Y]                                      0.12865E-03 
c  Velocity[Z]                                      0.42647E-02 
c  Pressure     0.36365E-04     132   0.92505E-02   0.25650E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55450E-08   0.16477E-08 0.10011E+00 
c  r22          0.10852E-01      13   0.57039E-08   0.18394E-08 0.10207E+00 
c  r33          0.21860E-01      15   0.68569E-08   0.12636E-07 0.12844E+00 
c  r12          0.93864E-03      18   0.63522E-08   0.30925E-09 0.61507E+00 
c  r13          0.46675E-02      19   0.68521E-08   0.15039E-08 0.19991E+00 
c  r23          0.39977E-02      19   0.63194E-08   0.12882E-08 0.20112E+00 
c  epsilon      0.10969E+02      11   0.33782E-08   0.97319E-02 0.16403E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.83717E-02 0.43182E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63354         0.61357       0.0052573       0.0015076
v  Velocity[Y]            -0.57365         0.54395       0.0030805      0.00087312
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4384          4.3406          4.3632
v  Pressure                -36.379          359.99          87.631          169.82
v  r11                   0.0010609        0.081919        0.013074        0.018286
v  r22                   0.0011135        0.082625        0.013354        0.018646
v  r33                   0.0016391         0.17426        0.027251        0.037206
v  r12                   -0.010656        0.013568     -0.00023381     -0.00030931
v  r13                   -0.045539        0.052796      9.3191e-05       0.0010138
v  r23                   -0.046699        0.051205      3.0482e-05      0.00057459
v  epsilon                0.069134          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9941e-05       0.0099178      0.00092499       0.0017427
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2782         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8782         0.71351         0.85283


 TIME FOR THE TIME STEP            10631:        0.77453E+02

===============================================================


 INSTANT    0.106320000E-01   TIME STEP NUMBER           10632
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.218425145E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.469551504E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294337006E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.417816868E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.821696780E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81286E-03   0.45192E-02 0.19881E+01 
c  Velocity[X]                                      0.13779E-03 
c  Velocity[Y]                                      0.12788E-03 
c  Velocity[Z]                                      0.42535E-02 
c  Pressure     0.36259E-04     132   0.92348E-02   0.25576E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55025E-08   0.16587E-08 0.10038E+00 
c  r22          0.10852E-01      13   0.54886E-08   0.18512E-08 0.10220E+00 
c  r33          0.21860E-01      15   0.69793E-08   0.12690E-07 0.12842E+00 
c  r12          0.93864E-03      18   0.50520E-08   0.29928E-09 0.60530E+00 
c  r13          0.46675E-02      19   0.73243E-08   0.14968E-08 0.19980E+00 
c  r23          0.39977E-02      19   0.66354E-08   0.12941E-08 0.20131E+00 
c  epsilon      0.10969E+02      11   0.36114E-08   0.10189E-01 0.17125E+00 
c  TempC        0.25716E+06      16   0.15166E-04   0.83723E-02 0.43177E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61359       0.0052574       0.0015076
v  Velocity[Y]            -0.57343         0.54409       0.0030805      0.00087311
v  Velocity[Z]              1.5654          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5791          5.4384          4.3406          4.3632
v  Pressure                -36.419          360.08          87.677           169.9
v  r11                   0.0010609         0.08192        0.013074        0.018286
v  r22                   0.0011135        0.082626        0.013354        0.018646
v  r33                   0.0016391         0.17428        0.027251        0.037206
v  r12                   -0.010658        0.013569     -0.00023381     -0.00030931
v  r13                   -0.045537        0.052795      9.3191e-05       0.0010138
v  r23                   -0.046699        0.051191      3.0482e-05      0.00057459
v  epsilon                0.069135          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099178      0.00092499       0.0017427
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2771         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8771         0.71351         0.85283


 TIME FOR THE TIME STEP            10632:        0.79399E+02

===============================================================


 INSTANT    0.106330000E-01   TIME STEP NUMBER           10633
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.609549099E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.351859965E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168073059E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.522368547E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.639737026E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81261E-03   0.44892E-02 0.19827E+01 
c  Velocity[X]                                      0.13806E-03 
c  Velocity[Y]                                      0.12772E-03 
c  Velocity[Z]                                      0.42235E-02 
c  Pressure     0.35935E-04     132   0.91489E-02   0.25347E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53576E-08   0.16378E-08 0.99864E-01 
c  r22          0.10852E-01      13   0.52835E-08   0.18398E-08 0.10229E+00 
c  r33          0.21860E-01      15   0.62425E-08   0.12465E-07 0.12772E+00 
c  r12          0.93864E-03      18   0.52193E-08   0.29715E-09 0.60668E+00 
c  r13          0.46675E-02      19   0.70941E-08   0.14914E-08 0.19967E+00 
c  r23          0.39977E-02      19   0.68392E-08   0.12690E-08 0.19975E+00 
c  epsilon      0.10969E+02      11   0.34305E-08   0.94783E-02 0.16305E+00 
c  TempC        0.25716E+06      16   0.15114E-04   0.84033E-02 0.43274E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61359       0.0052573       0.0015075
v  Velocity[Y]            -0.57356         0.54424       0.0030806      0.00087314
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4384          4.3406          4.3632
v  Pressure                -36.406          360.02          87.632          169.83
v  r11                   0.0010609        0.081923        0.013074        0.018286
v  r22                   0.0011135        0.082627        0.013354        0.018646
v  r33                   0.0016391         0.17431        0.027251        0.037206
v  r12                   -0.010661        0.013566     -0.00023381     -0.00030931
v  r13                   -0.045541        0.052795      9.3192e-05       0.0010138
v  r23                     -0.0467        0.051205      3.0482e-05      0.00057459
v  epsilon                0.069135          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9944e-05       0.0099178      0.00092499       0.0017427
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2764         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8764         0.71351         0.85284


 TIME FOR THE TIME STEP            10633:        0.75002E+02

===============================================================


 INSTANT    0.106340000E-01   TIME STEP NUMBER           10634
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.159101793E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.650274533E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.578619490E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168676411E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.321763351E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33839E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81235E-03   0.45422E-02 0.19958E+01 
c  Velocity[X]                                      0.13886E-03 
c  Velocity[Y]                                      0.12880E-03 
c  Velocity[Z]                                      0.42746E-02 
c  Pressure     0.36595E-04     133   0.93149E-02   0.25814E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49765E-08   0.16378E-08 0.99826E-01 
c  r22          0.10852E-01      13   0.51386E-08   0.18035E-08 0.10166E+00 
c  r33          0.21860E-01      15   0.55451E-08   0.12368E-07 0.12734E+00 
c  r12          0.93864E-03      18   0.52161E-08   0.30013E-09 0.60967E+00 
c  r13          0.46675E-02      19   0.55013E-08   0.14803E-08 0.19937E+00 
c  r23          0.39977E-02      19   0.55269E-08   0.12767E-08 0.19997E+00 
c  epsilon      0.10969E+02      10   0.54641E-08   0.94868E-02 0.16220E+00 
c  TempC        0.25716E+06      16   0.15179E-04   0.85032E-02 0.43440E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61354       0.0052573       0.0015076
v  Velocity[Y]            -0.57356         0.54408       0.0030804      0.00087311
v  Velocity[Z]              1.5654          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4384          4.3406          4.3632
v  Pressure                 -36.44             360           87.64          169.83
v  r11                   0.0010609        0.081925        0.013074        0.018286
v  r22                   0.0011135        0.082629        0.013354        0.018646
v  r33                   0.0016391         0.17429        0.027251        0.037206
v  r12                    -0.01066        0.013573     -0.00023381     -0.00030931
v  r13                   -0.045538        0.052797      9.3192e-05       0.0010138
v  r23                     -0.0467        0.051185      3.0482e-05      0.00057459
v  epsilon                0.069136          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099178      0.00092499       0.0017427
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb              0.001785           5.276         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.876         0.71351         0.85283


 TIME FOR THE TIME STEP            10634:        0.76206E+02

===============================================================


 INSTANT    0.106350000E-01   TIME STEP NUMBER           10635
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.236922544E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.985977253E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.174421854E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.736492577E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.585161812E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81163E-03   0.45169E-02 0.19906E+01 
c  Velocity[X]                                      0.13846E-03 
c  Velocity[Y]                                      0.12891E-03 
c  Velocity[Z]                                      0.42495E-02 
c  Pressure     0.36302E-04     132   0.92437E-02   0.25607E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51582E-08   0.16734E-08 0.10103E+00 
c  r22          0.10852E-01      13   0.52206E-08   0.18244E-08 0.10203E+00 
c  r33          0.21860E-01      15   0.53726E-08   0.12623E-07 0.12863E+00 
c  r12          0.93864E-03      18   0.51977E-08   0.30076E-09 0.61417E+00 
c  r13          0.46675E-02      19   0.56990E-08   0.14504E-08 0.19815E+00 
c  r23          0.39977E-02      19   0.60426E-08   0.12858E-08 0.20198E+00 
c  epsilon      0.10969E+02      11   0.32682E-08   0.97378E-02 0.16420E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.84154E-02 0.43257E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61359       0.0052574       0.0015076
v  Velocity[Y]            -0.57364         0.54404       0.0030805      0.00087317
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4384          4.3406          4.3632
v  Pressure                -36.401          360.07          87.664          169.88
v  r11                   0.0010609        0.081921        0.013074        0.018286
v  r22                   0.0011135        0.082631        0.013354        0.018646
v  r33                   0.0016392         0.17427        0.027251        0.037206
v  r12                   -0.010662        0.013572     -0.00023381     -0.00030931
v  r13                   -0.045537        0.052796      9.3192e-05       0.0010138
v  r23                     -0.0467        0.051173      3.0483e-05      0.00057459
v  epsilon                0.069137          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099177      0.00092499       0.0017427
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2764         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8764         0.71351         0.85283


 TIME FOR THE TIME STEP            10635:        0.76710E+02

===============================================================


 INSTANT    0.106360000E-01   TIME STEP NUMBER           10636
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.252439107E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.419365326E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.352544372E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.245330884E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.354971938E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81373E-03   0.45084E-02 0.19875E+01 
c  Velocity[X]                                      0.13724E-03 
c  Velocity[Y]                                      0.12845E-03 
c  Velocity[Z]                                      0.42427E-02 
c  Pressure     0.36774E-04     133   0.93558E-02   0.25938E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54939E-08   0.17015E-08 0.10139E+00 
c  r22          0.10852E-01      13   0.51964E-08   0.18591E-08 0.10251E+00 
c  r33          0.21860E-01      15   0.58355E-08   0.12849E-07 0.12888E+00 
c  r12          0.93864E-03      18   0.58398E-08   0.30545E-09 0.61193E+00 
c  r13          0.46675E-02      19   0.63352E-08   0.14943E-08 0.19900E+00 
c  r23          0.39977E-02      19   0.64720E-08   0.13203E-08 0.20328E+00 
c  epsilon      0.10969E+02      11   0.34623E-08   0.10218E-01 0.16799E+00 
c  TempC        0.25716E+06      16   0.15165E-04   0.83401E-02 0.43110E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61358       0.0052574       0.0015076
v  Velocity[Y]            -0.57355         0.54408       0.0030806      0.00087317
v  Velocity[Z]              1.5654          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5792          5.4384          4.3406          4.3632
v  Pressure                -36.459          360.03          87.642          169.85
v  r11                   0.0010609        0.081916        0.013074        0.018286
v  r22                   0.0011135        0.082633        0.013354        0.018646
v  r33                   0.0016392         0.17428        0.027251        0.037206
v  r12                   -0.010664        0.013568     -0.00023381     -0.00030931
v  r13                    -0.04554        0.052798      9.3193e-05       0.0010138
v  r23                     -0.0467        0.051199      3.0483e-05      0.00057459
v  epsilon                0.069138          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099175      0.00092499       0.0017427
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017849          5.2771         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8771         0.71351         0.85283


 TIME FOR THE TIME STEP            10636:        0.76175E+02

===============================================================


 INSTANT    0.106370000E-01   TIME STEP NUMBER           10637
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145983403E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.179002632E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171991667E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.280006773E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.840022786E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81182E-03   0.45398E-02 0.19966E+01 
c  Velocity[X]                                      0.13808E-03 
c  Velocity[Y]                                      0.12801E-03 
c  Velocity[Z]                                      0.42738E-02 
c  Pressure     0.36212E-04     131   0.92214E-02   0.25542E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58552E-08   0.16739E-08 0.10091E+00 
c  r22          0.10852E-01      13   0.52829E-08   0.18166E-08 0.10180E+00 
c  r33          0.21860E-01      15   0.59531E-08   0.12586E-07 0.12825E+00 
c  r12          0.93864E-03      18   0.53992E-08   0.30048E-09 0.60946E+00 
c  r13          0.46676E-02      19   0.55614E-08   0.14951E-08 0.19920E+00 
c  r23          0.39977E-02      19   0.59443E-08   0.13046E-08 0.20254E+00 
c  epsilon      0.10969E+02      11   0.33845E-08   0.97048E-02 0.16332E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.84317E-02 0.43335E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61356       0.0052573       0.0015076
v  Velocity[Y]            -0.57369          0.5442       0.0030805      0.00087315
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4384          4.3406          4.3632
v  Pressure                -36.398          359.93          87.584          169.76
v  r11                    0.001061         0.08191        0.013074        0.018286
v  r22                   0.0011135        0.082634        0.013354        0.018646
v  r33                   0.0016392         0.17431        0.027251        0.037206
v  r12                   -0.010663        0.013577     -0.00023381     -0.00030931
v  r13                   -0.045539          0.0528      9.3194e-05       0.0010138
v  r23                     -0.0467        0.051185      3.0484e-05      0.00057459
v  epsilon                0.069138          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099175      0.00092499       0.0017427
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2777         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8777         0.71351         0.85284


 TIME FOR THE TIME STEP            10637:        0.79180E+02

===============================================================


 INSTANT    0.106380000E-01   TIME STEP NUMBER           10638
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171916422E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205413034E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.487774793E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.151549523E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.204781484E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81357E-03   0.45167E-02 0.19899E+01 
c  Velocity[X]                                      0.13795E-03 
c  Velocity[Y]                                      0.12974E-03 
c  Velocity[Z]                                      0.42490E-02 
c  Pressure     0.36113E-04     133   0.91947E-02   0.25473E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60374E-08   0.16397E-08 0.10017E+00 
c  r22          0.10852E-01      13   0.53305E-08   0.18323E-08 0.10167E+00 
c  r33          0.21860E-01      15   0.62293E-08   0.12616E-07 0.12803E+00 
c  r12          0.93864E-03      18   0.59829E-08   0.29800E-09 0.60803E+00 
c  r13          0.46676E-02      19   0.56312E-08   0.15028E-08 0.19932E+00 
c  r23          0.39977E-02      19   0.61806E-08   0.12822E-08 0.20125E+00 
c  epsilon      0.10969E+02      11   0.34081E-08   0.10316E-01 0.17148E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.84702E-02 0.43391E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63333         0.61358       0.0052574       0.0015076
v  Velocity[Y]            -0.57367           0.544       0.0030806      0.00087317
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4384          4.3406          4.3632
v  Pressure                -36.438          360.03           87.67          169.87
v  r11                    0.001061        0.081907        0.013074        0.018286
v  r22                   0.0011135        0.082637        0.013354        0.018646
v  r33                   0.0016392         0.17429        0.027251        0.037206
v  r12                   -0.010663        0.013575     -0.00023381     -0.00030931
v  r13                   -0.045536          0.0528      9.3194e-05       0.0010138
v  r23                   -0.046699        0.051176      3.0484e-05      0.00057459
v  epsilon                0.069139          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9945e-05       0.0099176      0.00092499       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2777         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8777         0.71351         0.85284


 TIME FOR THE TIME STEP            10638:        0.76076E+02

===============================================================


 INSTANT    0.106390000E-01   TIME STEP NUMBER           10639
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.281569697E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145258479E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.223235952E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935020E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.121871406E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.392473865E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935014E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81204E-03   0.45278E-02 0.19908E+01 
c  Velocity[X]                                      0.13809E-03 
c  Velocity[Y]                                      0.12761E-03 
c  Velocity[Z]                                      0.42621E-02 
c  Pressure     0.36556E-04     134   0.93060E-02   0.25786E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59388E-08   0.16218E-08 0.99579E-01 
c  r22          0.10852E-01      13   0.53287E-08   0.18166E-08 0.10128E+00 
c  r33          0.21860E-01      15   0.66556E-08   0.12382E-07 0.12688E+00 
c  r12          0.93864E-03      18   0.59034E-08   0.29711E-09 0.60515E+00 
c  r13          0.46675E-02      19   0.58699E-08   0.14966E-08 0.19895E+00 
c  r23          0.39977E-02      19   0.62172E-08   0.12626E-08 0.19904E+00 
c  epsilon      0.10969E+02      11   0.32439E-08   0.97008E-02 0.16268E+00 
c  TempC        0.25716E+06      16   0.15121E-04   0.84147E-02 0.43265E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61359       0.0052574       0.0015076
v  Velocity[Y]            -0.57367         0.54398       0.0030806      0.00087318
v  Velocity[Z]              1.5651          5.4384          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4384          4.3406          4.3632
v  Pressure                -36.401          360.07          87.647          169.88
v  r11                    0.001061        0.081902        0.013074        0.018286
v  r22                   0.0011136        0.082634        0.013354        0.018646
v  r33                   0.0016393         0.17427        0.027251        0.037206
v  r12                   -0.010664        0.013579     -0.00023381     -0.00030931
v  r13                   -0.045538        0.052799      9.3194e-05       0.0010138
v  r23                   -0.046699        0.051192      3.0484e-05      0.00057459
v  epsilon                 0.06914          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099177      0.00092499       0.0017427
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2775         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8775         0.71351         0.85284


 TIME FOR THE TIME STEP            10639:        0.76150E+02

===============================================================


 INSTANT    0.106400000E-01   TIME STEP NUMBER           10640
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.236884840E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.314687520E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.247843666E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.234344936E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.169619629E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81250E-03   0.45388E-02 0.19959E+01 
c  Velocity[X]                                      0.13878E-03 
c  Velocity[Y]                                      0.12873E-03 
c  Velocity[Z]                                      0.42713E-02 
c  Pressure     0.36309E-04     133   0.92464E-02   0.25611E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59884E-08   0.16124E-08 0.99628E-01 
c  r22          0.10852E-01      13   0.52996E-08   0.17937E-08 0.10139E+00 
c  r33          0.21860E-01      15   0.71600E-08   0.12300E-07 0.12727E+00 
c  r12          0.93864E-03      18   0.53418E-08   0.29891E-09 0.60578E+00 
c  r13          0.46676E-02      19   0.53420E-08   0.14808E-08 0.19928E+00 
c  r23          0.39977E-02      19   0.60853E-08   0.12777E-08 0.20021E+00 
c  epsilon      0.10969E+02      11   0.32995E-08   0.94281E-02 0.16168E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.83732E-02 0.43173E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61354       0.0052573       0.0015076
v  Velocity[Y]            -0.57368          0.5441       0.0030806      0.00087318
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4384          4.3406          4.3632
v  Pressure                -36.423          360.02          87.652          169.85
v  r11                    0.001061        0.081896        0.013074        0.018286
v  r22                   0.0011136        0.082636        0.013354        0.018646
v  r33                   0.0016393         0.17428        0.027251        0.037206
v  r12                   -0.010662        0.013575     -0.00023381     -0.00030931
v  r13                   -0.045536        0.052802      9.3194e-05       0.0010138
v  r23                   -0.046699         0.05119      3.0484e-05      0.00057459
v  epsilon                0.069141          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099178      0.00092499       0.0017427
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2777         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8777         0.71351         0.85284


 TIME FOR THE TIME STEP            10640:        0.75498E+02

===============================================================


 INSTANT    0.106410000E-01   TIME STEP NUMBER           10641
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.158291784E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.209000932E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.233895028E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.490901571E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.118360688E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81228E-03   0.45191E-02 0.19897E+01 
c  Velocity[X]                                      0.13852E-03 
c  Velocity[Y]                                      0.12887E-03 
c  Velocity[Z]                                      0.42517E-02 
c  Pressure     0.36285E-04     132   0.92363E-02   0.25595E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54193E-08   0.16504E-08 0.10085E+00 
c  r22          0.10852E-01      13   0.56485E-08   0.18084E-08 0.10194E+00 
c  r33          0.21860E-01      15   0.64561E-08   0.12452E-07 0.12812E+00 
c  r12          0.93864E-03      18   0.55069E-08   0.29690E-09 0.61034E+00 
c  r13          0.46676E-02      18   0.71355E-08   0.14707E-08 0.19935E+00 
c  r23          0.39977E-02      19   0.65272E-08   0.12824E-08 0.20238E+00 
c  epsilon      0.10969E+02      11   0.34204E-08   0.97268E-02 0.16402E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.83960E-02 0.43283E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61362       0.0052574       0.0015076
v  Velocity[Y]            -0.57378         0.54419       0.0030806      0.00087322
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4384          4.3406          4.3632
v  Pressure                 -36.38          360.06          87.667          169.88
v  r11                    0.001061         0.08189        0.013074        0.018286
v  r22                   0.0011136         0.08264        0.013354        0.018646
v  r33                   0.0016393         0.17431        0.027251        0.037206
v  r12                   -0.010661         0.01357     -0.00023381     -0.00030931
v  r13                   -0.045536        0.052802      9.3193e-05       0.0010138
v  r23                   -0.046699        0.051186      3.0483e-05      0.00057459
v  epsilon                0.069141          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099179        0.000925       0.0017427
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb              0.001785           5.278         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.878         0.71351         0.85284


 TIME FOR THE TIME STEP            10641:        0.73779E+02

===============================================================


 INSTANT    0.106420000E-01   TIME STEP NUMBER           10642
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.356906242E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136458847E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.219383533E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.383043824E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.366754994E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81249E-03   0.44995E-02 0.19857E+01 
c  Velocity[X]                                      0.13782E-03 
c  Velocity[Y]                                      0.12832E-03 
c  Velocity[Z]                                      0.42334E-02 
c  Pressure     0.36129E-04     133   0.91965E-02   0.25484E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55457E-08   0.16292E-08 0.99893E-01 
c  r22          0.10852E-01      13   0.51692E-08   0.18259E-08 0.10201E+00 
c  r33          0.21860E-01      15   0.58953E-08   0.12461E-07 0.12771E+00 
c  r12          0.93864E-03      18   0.58533E-08   0.29997E-09 0.60967E+00 
c  r13          0.46676E-02      19   0.58524E-08   0.14976E-08 0.19979E+00 
c  r23          0.39977E-02      19   0.58150E-08   0.12759E-08 0.20035E+00 
c  epsilon      0.10969E+02      11   0.34745E-08   0.96837E-02 0.16300E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.83793E-02 0.43125E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63331         0.61358       0.0052573       0.0015076
v  Velocity[Y]            -0.57369         0.54402       0.0030805      0.00087317
v  Velocity[Z]              1.5652          5.4384          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4384          4.3406          4.3632
v  Pressure                -36.446          359.96          87.608          169.79
v  r11                    0.001061        0.081888        0.013074        0.018286
v  r22                   0.0011136        0.082643        0.013354        0.018646
v  r33                   0.0016393         0.17429        0.027251        0.037206
v  r12                   -0.010659        0.013573     -0.00023381     -0.00030931
v  r13                   -0.045539        0.052804      9.3194e-05       0.0010138
v  r23                   -0.046698        0.051207      3.0484e-05      0.00057459
v  epsilon                0.069142          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9944e-05       0.0099181        0.000925       0.0017427
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2779         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8779         0.71351         0.85284


 TIME FOR THE TIME STEP            10642:        0.74184E+02

===============================================================


 INSTANT    0.106430000E-01   TIME STEP NUMBER           10643
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.156007906E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.426957330E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294466047E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.243204134E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171590145E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81316E-03   0.45236E-02 0.19905E+01 
c  Velocity[X]                                      0.13802E-03 
c  Velocity[Y]                                      0.12820E-03 
c  Velocity[Z]                                      0.42574E-02 
c  Pressure     0.36450E-04     131   0.92787E-02   0.25711E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58248E-08   0.16638E-08 0.10103E+00 
c  r22          0.10852E-01      13   0.53608E-08   0.18398E-08 0.10253E+00 
c  r33          0.21860E-01      15   0.62810E-08   0.12729E-07 0.12912E+00 
c  r12          0.93864E-03      18   0.60941E-08   0.30515E-09 0.61354E+00 
c  r13          0.46676E-02      19   0.74254E-08   0.15072E-08 0.20089E+00 
c  r23          0.39977E-02      19   0.65883E-08   0.13094E-08 0.20327E+00 
c  epsilon      0.10969E+02      11   0.36507E-08   0.97832E-02 0.16306E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.84539E-02 0.43354E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161986


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63336         0.61356       0.0052574       0.0015076
v  Velocity[Y]            -0.57381         0.54411       0.0030806      0.00087322
v  Velocity[Z]              1.5652          5.4385          4.3388          4.3625
v  ǁVelocityǁ                1.579          5.4385          4.3406          4.3632
v  Pressure                -36.376          360.01          87.627          169.83
v  r11                    0.001061        0.081893        0.013074        0.018286
v  r22                   0.0011136        0.082644        0.013354        0.018646
v  r33                   0.0016394         0.17427        0.027251        0.037206
v  r12                   -0.010661        0.013571     -0.00023381     -0.00030931
v  r13                   -0.045536        0.052804      9.3195e-05       0.0010138
v  r23                   -0.046698        0.051199      3.0484e-05      0.00057459
v  epsilon                0.069143          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099182        0.000925       0.0017427
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2781         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8781         0.71351         0.85284


 TIME FOR THE TIME STEP            10643:        0.75758E+02

===============================================================


 INSTANT    0.106440000E-01   TIME STEP NUMBER           10644
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.187431613E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.139630355E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.354009960E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.353739001E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.156525993E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81253E-03   0.45293E-02 0.19951E+01 
c  Velocity[X]                                      0.13872E-03 
c  Velocity[Y]                                      0.12822E-03 
c  Velocity[Z]                                      0.42623E-02 
c  Pressure     0.36419E-04     131   0.92694E-02   0.25689E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.63140E-08   0.17072E-08 0.10142E+00 
c  r22          0.10852E-01      13   0.54151E-08   0.18536E-08 0.10262E+00 
c  r33          0.21860E-01      15   0.70316E-08   0.12992E-07 0.12986E+00 
c  r12          0.93864E-03      18   0.53721E-08   0.30192E-09 0.60986E+00 
c  r13          0.46676E-02      19   0.71032E-08   0.14928E-08 0.19999E+00 
c  r23          0.39977E-02      19   0.72241E-08   0.13448E-08 0.20464E+00 
c  epsilon      0.10969E+02      11   0.37409E-08   0.10457E-01 0.17283E+00 
c  TempC        0.25716E+06      16   0.15166E-04   0.84414E-02 0.43326E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61358       0.0052574       0.0015076
v  Velocity[Y]            -0.57371         0.54425       0.0030806      0.00087324
v  Velocity[Z]              1.5651          5.4385          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4385          4.3406          4.3632
v  Pressure                -36.468          360.02          87.643          169.85
v  r11                    0.001061        0.081897        0.013074        0.018286
v  r22                   0.0011136        0.082646        0.013354        0.018646
v  r33                   0.0016394         0.17428        0.027251        0.037206
v  r12                   -0.010659        0.013569     -0.00023382     -0.00030931
v  r13                   -0.045535        0.052806      9.3195e-05       0.0010138
v  r23                   -0.046698        0.051183      3.0485e-05      0.00057459
v  epsilon                0.069144          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099182        0.000925       0.0017427
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2784         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8784         0.71351         0.85283


 TIME FOR THE TIME STEP            10644:        0.77239E+02

===============================================================


 INSTANT    0.106450000E-01   TIME STEP NUMBER           10645
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.441594221E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294153204E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.625400085E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.124610219E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.235904327E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81259E-03   0.45269E-02 0.19900E+01 
c  Velocity[X]                                      0.13856E-03 
c  Velocity[Y]                                      0.12804E-03 
c  Velocity[Z]                                      0.42603E-02 
c  Pressure     0.35943E-04     132   0.91553E-02   0.25353E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.65005E-08   0.16364E-08 0.10021E+00 
c  r22          0.10852E-01      13   0.53568E-08   0.18579E-08 0.10245E+00 
c  r33          0.21860E-01      15   0.73926E-08   0.12580E-07 0.12828E+00 
c  r12          0.93864E-03      18   0.53460E-08   0.30758E-09 0.61302E+00 
c  r13          0.46676E-02      19   0.64471E-08   0.15225E-08 0.20075E+00 
c  r23          0.39977E-02      19   0.66664E-08   0.12767E-08 0.20070E+00 
c  epsilon      0.10969E+02      11   0.35009E-08   0.96073E-02 0.16256E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.83622E-02 0.43159E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61358       0.0052574       0.0015077
v  Velocity[Y]            -0.57384          0.5441       0.0030806      0.00087323
v  Velocity[Z]               1.565          5.4385          4.3388          4.3625
v  ǁVelocityǁ               1.5788          5.4385          4.3406          4.3632
v  Pressure                -36.422             360          87.609          169.82
v  r11                    0.001061          0.0819        0.013074        0.018286
v  r22                   0.0011136        0.082648        0.013354        0.018646
v  r33                   0.0016394         0.17431        0.027251        0.037206
v  r12                   -0.010658        0.013573     -0.00023381     -0.00030931
v  r13                   -0.045538        0.052809      9.3195e-05       0.0010138
v  r23                   -0.046699        0.051206      3.0485e-05      0.00057459
v  epsilon                0.069145          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099183        0.000925       0.0017427
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2784         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8784         0.71351         0.85284


 TIME FOR THE TIME STEP            10645:        0.76443E+02

===============================================================


 INSTANT    0.106460000E-01   TIME STEP NUMBER           10646
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.397947324E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239365126E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136185998E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.245356980E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.789277926E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81234E-03   0.45324E-02 0.19927E+01 
c  Velocity[X]                                      0.13717E-03 
c  Velocity[Y]                                      0.12994E-03 
c  Velocity[Z]                                      0.42653E-02 
c  Pressure     0.36529E-04     133   0.93008E-02   0.25765E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.66298E-08   0.16364E-08 0.99897E-01 
c  r22          0.10852E-01      13   0.51536E-08   0.18342E-08 0.10188E+00 
c  r33          0.21860E-01      15   0.67270E-08   0.12504E-07 0.12766E+00 
c  r12          0.93864E-03      18   0.51691E-08   0.30402E-09 0.61259E+00 
c  r13          0.46676E-02      19   0.60205E-08   0.14965E-08 0.19977E+00 
c  r23          0.39977E-02      19   0.72611E-08   0.12835E-08 0.20015E+00 
c  epsilon      0.10969E+02      11   0.34477E-08   0.95105E-02 0.16185E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.83907E-02 0.43261E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61356       0.0052573       0.0015076
v  Velocity[Y]            -0.57379         0.54408       0.0030805      0.00087319
v  Velocity[Z]              1.5649          5.4385          4.3387          4.3625
v  ǁVelocityǁ               1.5787          5.4385          4.3406          4.3632
v  Pressure                -36.442          359.94          87.613          169.79
v  r11                    0.001061        0.081898        0.013074        0.018286
v  r22                   0.0011136        0.082649        0.013354        0.018646
v  r33                   0.0016394         0.17429        0.027251        0.037206
v  r12                   -0.010659        0.013574     -0.00023382     -0.00030931
v  r13                   -0.045536        0.052811      9.3196e-05       0.0010138
v  r23                   -0.046698        0.051198      3.0486e-05      0.00057459
v  epsilon                0.069145          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099183        0.000925       0.0017427
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8786         0.71351         0.85283


 TIME FOR THE TIME STEP            10646:        0.76260E+02

===============================================================


 INSTANT    0.106470000E-01   TIME STEP NUMBER           10647
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.510358918E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.819118465E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149237192E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.290384938E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.294571759E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81287E-03   0.45222E-02 0.19925E+01 
c  Velocity[X]                                      0.13862E-03 
c  Velocity[Y]                                      0.12735E-03 
c  Velocity[Z]                                      0.42562E-02 
c  Pressure     0.36521E-04     133   0.93035E-02   0.25761E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.63435E-08   0.16498E-08 0.10006E+00 
c  r22          0.10852E-01      13   0.50482E-08   0.18431E-08 0.10193E+00 
c  r33          0.21860E-01      15   0.65428E-08   0.12582E-07 0.12762E+00 
c  r12          0.93864E-03      18   0.52694E-08   0.29807E-09 0.61022E+00 
c  r13          0.46676E-02      19   0.58553E-08   0.14768E-08 0.19850E+00 
c  r23          0.39977E-02      19   0.65971E-08   0.12788E-08 0.19973E+00 
c  epsilon      0.10969E+02      11   0.34629E-08   0.98409E-02 0.16497E+00 
c  TempC        0.25716E+06      16   0.15124E-04   0.84776E-02 0.43453E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6333         0.61361       0.0052575       0.0015076
v  Velocity[Y]            -0.57376         0.54416       0.0030807      0.00087328
v  Velocity[Z]              1.5649          5.4385          4.3388          4.3625
v  ǁVelocityǁ               1.5787          5.4385          4.3406          4.3632
v  Pressure                -36.395          360.09           87.69           169.9
v  r11                    0.001061        0.081895        0.013074        0.018286
v  r22                   0.0011136        0.082646        0.013354        0.018646
v  r33                   0.0016395         0.17428        0.027251        0.037206
v  r12                   -0.010658        0.013573     -0.00023382     -0.00030931
v  r13                   -0.045536         0.05281      9.3196e-05       0.0010138
v  r23                   -0.046698        0.051182      3.0487e-05      0.00057459
v  epsilon                0.069146          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099182        0.000925       0.0017427
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2785         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71351         0.85284


 TIME FOR THE TIME STEP            10647:        0.77212E+02

===============================================================


 INSTANT    0.106480000E-01   TIME STEP NUMBER           10648
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205296993E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.274822055E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184765811E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200069972E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136807378E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81339E-03   0.45261E-02 0.19905E+01 
c  Velocity[X]                                      0.13735E-03 
c  Velocity[Y]                                      0.12863E-03 
c  Velocity[Z]                                      0.42602E-02 
c  Pressure     0.36426E-04     133   0.92714E-02   0.25694E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59518E-08   0.16666E-08 0.10056E+00 
c  r22          0.10852E-01      13   0.52647E-08   0.18570E-08 0.10214E+00 
c  r33          0.21860E-01      15   0.59734E-08   0.12769E-07 0.12858E+00 
c  r12          0.93864E-03      18   0.60221E-08   0.29884E-09 0.61110E+00 
c  r13          0.46676E-02      19   0.62843E-08   0.15219E-08 0.20054E+00 
c  r23          0.39977E-02      19   0.73603E-08   0.12949E-08 0.20079E+00 
c  epsilon      0.10969E+02      11   0.34114E-08   0.10113E-01 0.16798E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.84087E-02 0.43293E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61359       0.0052574       0.0015076
v  Velocity[Y]            -0.57366         0.54426       0.0030806      0.00087325
v  Velocity[Z]              1.5652          5.4385          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4385          4.3406          4.3632
v  Pressure                -36.413          360.02          87.647          169.85
v  r11                   0.0010611        0.081901        0.013074        0.018286
v  r22                   0.0011136        0.082647        0.013354        0.018646
v  r33                   0.0016395         0.17429        0.027251        0.037206
v  r12                   -0.010655        0.013571     -0.00023382     -0.00030931
v  r13                   -0.045539         0.05281      9.3196e-05       0.0010138
v  r23                   -0.046698        0.051198      3.0486e-05      0.00057459
v  epsilon                0.069147          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099176        0.000925       0.0017427
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2791         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8791         0.71351         0.85283


 TIME FOR THE TIME STEP            10648:        0.75199E+02

===============================================================


 INSTANT    0.106490000E-01   TIME STEP NUMBER           10649
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.466514947E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.937467004E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100998747E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.840311849E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.434129495E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81159E-03   0.45310E-02 0.19930E+01 
c  Velocity[X]                                      0.13782E-03 
c  Velocity[Y]                                      0.12821E-03 
c  Velocity[Z]                                      0.42649E-02 
c  Pressure     0.36349E-04     131   0.92477E-02   0.25640E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56091E-08   0.16306E-08 0.99697E-01 
c  r22          0.10852E-01      13   0.52142E-08   0.18357E-08 0.10191E+00 
c  r33          0.21860E-01      15   0.66971E-08   0.12449E-07 0.12729E+00 
c  r12          0.93864E-03      18   0.58385E-08   0.30063E-09 0.60999E+00 
c  r13          0.46676E-02      19   0.68759E-08   0.15073E-08 0.20034E+00 
c  r23          0.39977E-02      19   0.72463E-08   0.12667E-08 0.19833E+00 
c  epsilon      0.10969E+02      11   0.33610E-08   0.96648E-02 0.16315E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.83912E-02 0.43199E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61355       0.0052574       0.0015076
v  Velocity[Y]            -0.57374         0.54404       0.0030806      0.00087323
v  Velocity[Z]              1.5651          5.4385          4.3388          4.3625
v  ǁVelocityǁ               1.5789          5.4385          4.3406          4.3632
v  Pressure                -36.415          360.02          87.638          169.84
v  r11                   0.0010611          0.0819        0.013074        0.018286
v  r22                   0.0011137        0.082648        0.013354        0.018646
v  r33                   0.0016395         0.17432        0.027251        0.037206
v  r12                   -0.010654        0.013575     -0.00023382     -0.00030931
v  r13                   -0.045538        0.052809      9.3196e-05       0.0010138
v  r23                   -0.046698        0.051187      3.0486e-05      0.00057459
v  epsilon                0.069148          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099174        0.000925       0.0017427
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2784         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8784         0.71351         0.85284


 TIME FOR THE TIME STEP            10649:        0.77315E+02

===============================================================


 INSTANT    0.106500000E-01   TIME STEP NUMBER           10650
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.914805278E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.227927963E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.241304805E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.598168306E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.193500694E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81344E-03   0.45278E-02 0.19915E+01 
c  Velocity[X]                                      0.13818E-03 
c  Velocity[Y]                                      0.12877E-03 
c  Velocity[Z]                                      0.42609E-02 
c  Pressure     0.35943E-04     131   0.91525E-02   0.25353E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54953E-08   0.16792E-08 0.10089E+00 
c  r22          0.10852E-01      13   0.50654E-08   0.18649E-08 0.10221E+00 
c  r33          0.21860E-01      15   0.70382E-08   0.12947E-07 0.12911E+00 
c  r12          0.93864E-03      18   0.57600E-08   0.30175E-09 0.61141E+00 
c  r13          0.46676E-02      19   0.62392E-08   0.15170E-08 0.20091E+00 
c  r23          0.39977E-02      20   0.61616E-08   0.13140E-08 0.20253E+00 
c  epsilon      0.10969E+02      11   0.34434E-08   0.10739E-01 0.17486E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.84181E-02 0.43273E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353          0.6136       0.0052575       0.0015076
v  Velocity[Y]            -0.57373          0.5441       0.0030806      0.00087323
v  Velocity[Z]              1.5651          5.4385          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4385          4.3406          4.3632
v  Pressure                -36.451          359.96          87.609           169.8
v  r11                   0.0010611        0.081899        0.013074        0.018286
v  r22                   0.0011137         0.08265        0.013354        0.018646
v  r33                   0.0016395          0.1743        0.027251        0.037206
v  r12                   -0.010665        0.013571     -0.00023382     -0.00030931
v  r13                   -0.045536        0.052811      9.3197e-05       0.0010138
v  r23                   -0.046698        0.051181      3.0487e-05      0.00057459
v  epsilon                0.069148          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099174        0.000925       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb              0.001785           5.278         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178           5.878         0.71351         0.85284


 TIME FOR THE TIME STEP            10650:        0.76032E+02

===============================================================


 INSTANT    0.106510000E-01   TIME STEP NUMBER           10651
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153757679E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.318788840E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.325231807E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161188271E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166555635E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81244E-03   0.44859E-02 0.19854E+01 
c  Velocity[X]                                      0.13787E-03 
c  Velocity[Y]                                      0.12786E-03 
c  Velocity[Z]                                      0.42202E-02 
c  Pressure     0.36618E-04     132   0.93220E-02   0.25829E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54995E-08   0.16253E-08 0.99163E-01 
c  r22          0.10852E-01      13   0.49253E-08   0.18196E-08 0.10142E+00 
c  r33          0.21860E-01      15   0.72421E-08   0.12393E-07 0.12664E+00 
c  r12          0.93864E-03      18   0.62480E-08   0.29684E-09 0.60576E+00 
c  r13          0.46676E-02      19   0.65321E-08   0.14868E-08 0.19883E+00 
c  r23          0.39977E-02      20   0.67908E-08   0.12735E-08 0.19810E+00 
c  epsilon      0.10969E+02      11   0.35191E-08   0.97298E-02 0.16399E+00 
c  TempC        0.25716E+06      16   0.15097E-04   0.83786E-02 0.43209E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61357       0.0052576       0.0015077
v  Velocity[Y]            -0.57374         0.54425       0.0030806      0.00087325
v  Velocity[Z]              1.5648          5.4385          4.3387          4.3625
v  ǁVelocityǁ               1.5786          5.4385          4.3406          4.3632
v  Pressure                -36.413             360           87.62          169.83
v  r11                   0.0010611        0.081893        0.013074        0.018286
v  r22                   0.0011137        0.082651        0.013354        0.018646
v  r33                   0.0016395         0.17428        0.027251        0.037206
v  r12                   -0.010667        0.013577     -0.00023382     -0.00030931
v  r13                   -0.045538        0.052809      9.3198e-05       0.0010138
v  r23                   -0.046698        0.051202      3.0487e-05      0.00057459
v  epsilon                0.069149          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099176        0.000925       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2769         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71351         0.85283


 TIME FOR THE TIME STEP            10651:        0.79171E+02

===============================================================


 INSTANT    0.106520000E-01   TIME STEP NUMBER           10652
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.535748845E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111891824E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.356952464E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.894421421E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.290029694E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81241E-03   0.45078E-02 0.19899E+01 
c  Velocity[X]                                      0.13836E-03 
c  Velocity[Y]                                      0.12817E-03 
c  Velocity[Z]                                      0.42413E-02 
c  Pressure     0.36212E-04     131   0.92137E-02   0.25543E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53703E-08   0.16096E-08 0.98849E-01 
c  r22          0.10852E-01      13   0.49166E-08   0.18080E-08 0.10151E+00 
c  r33          0.21860E-01      15   0.58852E-08   0.12332E-07 0.12667E+00 
c  r12          0.93864E-03      18   0.65545E-08   0.29645E-09 0.60760E+00 
c  r13          0.46676E-02      19   0.59085E-08   0.14694E-08 0.19831E+00 
c  r23          0.39977E-02      20   0.58009E-08   0.12669E-08 0.19814E+00 
c  epsilon      0.10969E+02      11   0.34763E-08   0.95911E-02 0.16238E+00 
c  TempC        0.25716E+06      16   0.15196E-04   0.84212E-02 0.43277E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61356       0.0052575       0.0015076
v  Velocity[Y]            -0.57352         0.54414       0.0030806      0.00087324
v  Velocity[Z]              1.5651          5.4385          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4385          4.3406          4.3632
v  Pressure                -36.413          359.98          87.634          169.83
v  r11                   0.0010611        0.081886        0.013074        0.018286
v  r22                   0.0011137        0.082651        0.013354        0.018646
v  r33                   0.0016396         0.17428        0.027251        0.037206
v  r12                   -0.010664        0.013575     -0.00023382     -0.00030931
v  r13                   -0.045536        0.052811      9.3198e-05       0.0010138
v  r23                   -0.046698        0.051191      3.0487e-05      0.00057459
v  epsilon                 0.06915          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099177      0.00092501       0.0017427
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2766         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71351         0.85283


 TIME FOR THE TIME STEP            10652:        0.80061E+02

===============================================================


 INSTANT    0.106530000E-01   TIME STEP NUMBER           10653
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.368198831E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.315242879E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.430538362E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190679920E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.693975794E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81249E-03   0.45285E-02 0.19913E+01 
c  Velocity[X]                                      0.13776E-03 
c  Velocity[Y]                                      0.12927E-03 
c  Velocity[Z]                                      0.42614E-02 
c  Pressure     0.36481E-04     132   0.92854E-02   0.25733E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58310E-08   0.16280E-08 0.99473E-01 
c  r22          0.10852E-01      13   0.47109E-08   0.17931E-08 0.10128E+00 
c  r33          0.21860E-01      15   0.56593E-08   0.12329E-07 0.12684E+00 
c  r12          0.93864E-03      18   0.56471E-08   0.29537E-09 0.60703E+00 
c  r13          0.46676E-02      19   0.57000E-08   0.14542E-08 0.19865E+00 
c  r23          0.39977E-02      19   0.65695E-08   0.12672E-08 0.19880E+00 
c  epsilon      0.10969E+02      11   0.34770E-08   0.96605E-02 0.16417E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.84574E-02 0.43384E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61362       0.0052575       0.0015076
v  Velocity[Y]            -0.57354         0.54406       0.0030806      0.00087324
v  Velocity[Z]               1.565          5.4385          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4385          4.3406          4.3632
v  Pressure                -36.382          360.03          87.647          169.85
v  r11                   0.0010611        0.081884        0.013074        0.018286
v  r22                   0.0011137        0.082652        0.013354        0.018646
v  r33                   0.0016396         0.17431        0.027251        0.037206
v  r12                   -0.010659        0.013574     -0.00023382     -0.00030931
v  r13                   -0.045537        0.052811      9.3199e-05       0.0010138
v  r23                   -0.046698        0.051184      3.0487e-05      0.00057459
v  epsilon                0.069151          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099178      0.00092501       0.0017427
v  CourantNb               0.44213             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2769         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71351         0.85283


 TIME FOR THE TIME STEP            10653:        0.75449E+02

===============================================================


 INSTANT    0.106540000E-01   TIME STEP NUMBER           10654
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178236332E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.157515830E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.187131693E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.275246740E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.426847251E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81379E-03   0.45276E-02 0.19935E+01 
c  Velocity[X]                                      0.13710E-03 
c  Velocity[Y]                                      0.12884E-03 
c  Velocity[Z]                                      0.42616E-02 
c  Pressure     0.36357E-04     133   0.92567E-02   0.25644E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.62177E-08   0.16127E-08 0.99335E-01 
c  r22          0.10852E-01      13   0.47012E-08   0.18297E-08 0.10177E+00 
c  r33          0.21860E-01      14   0.71676E-08   0.12474E-07 0.12737E+00 
c  r12          0.93864E-03      18   0.57225E-08   0.29340E-09 0.60409E+00 
c  r13          0.46676E-02      19   0.54196E-08   0.15048E-08 0.20032E+00 
c  r23          0.39977E-02      19   0.64278E-08   0.12644E-08 0.19845E+00 
c  epsilon      0.10969E+02      11   0.33625E-08   0.99994E-02 0.16678E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.83930E-02 0.43166E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61359       0.0052575       0.0015077
v  Velocity[Y]            -0.57357         0.54412       0.0030805      0.00087321
v  Velocity[Z]              1.5652          5.4385          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4385          4.3406          4.3632
v  Pressure                -36.452          360.03          87.648          169.86
v  r11                   0.0010611         0.08188        0.013074        0.018286
v  r22                   0.0011137        0.082652        0.013354        0.018646
v  r33                   0.0016396          0.1743        0.027251        0.037206
v  r12                   -0.010658        0.013581     -0.00023382     -0.00030931
v  r13                   -0.045539        0.052813      9.3199e-05       0.0010138
v  r23                   -0.046698         0.05117      3.0488e-05      0.00057459
v  epsilon                0.069152          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099176      0.00092501       0.0017427
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2772         0.11442         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60178          5.8772         0.71351         0.85283


 TIME FOR THE TIME STEP            10654:        0.72639E+02

===============================================================


 INSTANT    0.106550000E-01   TIME STEP NUMBER           10655
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.266997597E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.252219673E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.337950633E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.955006263E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.433327682E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81271E-03   0.44894E-02 0.19870E+01 
c  Velocity[X]                                      0.13780E-03 
c  Velocity[Y]                                      0.12835E-03 
c  Velocity[Z]                                      0.42232E-02 
c  Pressure     0.36325E-04     131   0.92471E-02   0.25622E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.62840E-08   0.16216E-08 0.99172E-01 
c  r22          0.10852E-01      13   0.48245E-08   0.18446E-08 0.10174E+00 
c  r33          0.21860E-01      14   0.67093E-08   0.12517E-07 0.12711E+00 
c  r12          0.93864E-03      18   0.52627E-08   0.30248E-09 0.61088E+00 
c  r13          0.46676E-02      19   0.59557E-08   0.15137E-08 0.19949E+00 
c  r23          0.39977E-02      19   0.59434E-08   0.12928E-08 0.19951E+00 
c  epsilon      0.10969E+02      11   0.33074E-08   0.97787E-02 0.16318E+00 
c  TempC        0.25716E+06      16   0.15120E-04   0.83959E-02 0.43203E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61356       0.0052575       0.0015077
v  Velocity[Y]            -0.57358         0.54426       0.0030806      0.00087323
v  Velocity[Z]              1.5651          5.4385          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4385          4.3406          4.3632
v  Pressure                -36.406          360.01          87.621          169.82
v  r11                   0.0010611        0.081879        0.013074        0.018286
v  r22                   0.0011137        0.082647        0.013354        0.018646
v  r33                   0.0016396         0.17427        0.027251        0.037206
v  r12                   -0.010659        0.013579     -0.00023382     -0.00030931
v  r13                   -0.045537        0.052812      9.3199e-05       0.0010138
v  r23                   -0.046697        0.051196      3.0488e-05      0.00057459
v  epsilon                0.069152          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099175      0.00092501       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2771         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71351         0.85284


 TIME FOR THE TIME STEP            10655:        0.77988E+02

===============================================================


 INSTANT    0.106560000E-01   TIME STEP NUMBER           10656
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.174606262E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.441171553E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.788608685E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294890400E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.194643003E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81329E-03   0.44923E-02 0.19846E+01 
c  Velocity[X]                                      0.13776E-03 
c  Velocity[Y]                                      0.12799E-03 
c  Velocity[Z]                                      0.42266E-02 
c  Pressure     0.36187E-04     133   0.92098E-02   0.25525E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60287E-08   0.16416E-08 0.99870E-01 
c  r22          0.10852E-01      13   0.50941E-08   0.18213E-08 0.10132E+00 
c  r33          0.21860E-01      15   0.62392E-08   0.12599E-07 0.12772E+00 
c  r12          0.93864E-03      18   0.51916E-08   0.29900E-09 0.60760E+00 
c  r13          0.46676E-02      19   0.64707E-08   0.15134E-08 0.19991E+00 
c  r23          0.39977E-02      19   0.57400E-08   0.12930E-08 0.20087E+00 
c  epsilon      0.10969E+02      11   0.33698E-08   0.10369E-01 0.17288E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.84022E-02 0.43276E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61359       0.0052576       0.0015077
v  Velocity[Y]            -0.57348         0.54413       0.0030806      0.00087326
v  Velocity[Z]              1.5653          5.4385          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4385          4.3406          4.3632
v  Pressure                -36.435          360.01          87.634          169.83
v  r11                   0.0010611        0.081883        0.013074        0.018286
v  r22                   0.0011137        0.082647        0.013354        0.018646
v  r33                   0.0016396         0.17428        0.027251        0.037206
v  r12                   -0.010658        0.013575     -0.00023382     -0.00030931
v  r13                   -0.045535        0.052812        9.32e-05       0.0010138
v  r23                   -0.046697        0.051194      3.0489e-05      0.00057459
v  epsilon                0.069153          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099176      0.00092501       0.0017427
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2774         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71351         0.85284


 TIME FOR THE TIME STEP            10656:        0.77725E+02

===============================================================


 INSTANT    0.106570000E-01   TIME STEP NUMBER           10657
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.156606645E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.703010825E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.496764956E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.927646410E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.144991708E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81280E-03   0.45238E-02 0.19914E+01 
c  Velocity[X]                                      0.13793E-03 
c  Velocity[Y]                                      0.12787E-03 
c  Velocity[Z]                                      0.42580E-02 
c  Pressure     0.36420E-04     133   0.92763E-02   0.25689E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59341E-08   0.16073E-08 0.99082E-01 
c  r22          0.10852E-01      13   0.50393E-08   0.18014E-08 0.10128E+00 
c  r33          0.21860E-01      15   0.57986E-08   0.12219E-07 0.12622E+00 
c  r12          0.93865E-03      18   0.53664E-08   0.29836E-09 0.60805E+00 
c  r13          0.46676E-02      19   0.56860E-08   0.14723E-08 0.19913E+00 
c  r23          0.39977E-02      19   0.57067E-08   0.12520E-08 0.19723E+00 
c  epsilon      0.10969E+02      11   0.33481E-08   0.94401E-02 0.16224E+00 
c  TempC        0.25716E+06      16   0.15127E-04   0.84105E-02 0.43271E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61359       0.0052575       0.0015077
v  Velocity[Y]            -0.57342         0.54403       0.0030807      0.00087325
v  Velocity[Z]              1.5648          5.4386          4.3387          4.3625
v  ǁVelocityǁ               1.5786          5.4386          4.3406          4.3632
v  Pressure                -36.392          359.99          87.598          169.81
v  r11                   0.0010611         0.08188        0.013074        0.018286
v  r22                   0.0011137        0.082649        0.013354        0.018646
v  r33                   0.0016397         0.17432        0.027251        0.037206
v  r12                   -0.010661        0.013576     -0.00023382     -0.00030931
v  r13                   -0.045538        0.052811      9.3199e-05       0.0010138
v  r23                   -0.046696        0.051182      3.0489e-05      0.00057459
v  epsilon                0.069154           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099176      0.00092501       0.0017427
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2765         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765         0.71351         0.85284


 TIME FOR THE TIME STEP            10657:        0.79615E+02

===============================================================


 INSTANT    0.106580000E-01   TIME STEP NUMBER           10658
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.422350399E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.487288070E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.392535843E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.267195669E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.319865074E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      45   0.81296E-03   0.45209E-02 0.19905E+01 
c  Velocity[X]                                      0.13823E-03 
c  Velocity[Y]                                      0.12894E-03 
c  Velocity[Z]                                      0.42538E-02 
c  Pressure     0.36092E-04     132   0.91920E-02   0.25457E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57618E-08   0.16119E-08 0.98996E-01 
c  r22          0.10852E-01      13   0.49369E-08   0.18203E-08 0.10114E+00 
c  r33          0.21860E-01      15   0.59418E-08   0.12309E-07 0.12601E+00 
c  r12          0.93865E-03      18   0.54998E-08   0.30105E-09 0.60974E+00 
c  r13          0.46676E-02      19   0.57991E-08   0.14786E-08 0.19892E+00 
c  r23          0.39977E-02      19   0.51583E-08   0.12535E-08 0.19716E+00 
c  epsilon      0.10969E+02      11   0.33791E-08   0.95823E-02 0.16277E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.84208E-02 0.43332E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63355         0.61358       0.0052575       0.0015076
v  Velocity[Y]             -0.5733         0.54412       0.0030806      0.00087323
v  Velocity[Z]              1.5649          5.4386          4.3387          4.3625
v  ǁVelocityǁ               1.5787          5.4386          4.3406          4.3632
v  Pressure                 -36.43          359.98          87.623          169.82
v  r11                   0.0010611        0.081879        0.013074        0.018286
v  r22                   0.0011137         0.08265        0.013354        0.018646
v  r33                   0.0016397         0.17434        0.027251        0.037206
v  r12                   -0.010661        0.013573     -0.00023382     -0.00030931
v  r13                   -0.045536        0.052812        9.32e-05       0.0010138
v  r23                   -0.046696        0.051175      3.0489e-05      0.00057459
v  epsilon                0.069155          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05       0.0099177      0.00092501       0.0017427
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2765         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765         0.71351         0.85283


 TIME FOR THE TIME STEP            10658:        0.74261E+02

===============================================================


 INSTANT    0.106590000E-01   TIME STEP NUMBER           10659
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.328334439E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.252685191E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.170812362E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.185089659E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162839179E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81162E-03   0.45334E-02 0.19931E+01 
c  Velocity[X]                                      0.13838E-03 
c  Velocity[Y]                                      0.12825E-03 
c  Velocity[Z]                                      0.42668E-02 
c  Pressure     0.36624E-04     132   0.93312E-02   0.25833E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54205E-08   0.16471E-08 0.99886E-01 
c  r22          0.10852E-01      13   0.46499E-08   0.18252E-08 0.10148E+00 
c  r33          0.21860E-01      15   0.57602E-08   0.12570E-07 0.12739E+00 
c  r12          0.93865E-03      18   0.50072E-08   0.29786E-09 0.61043E+00 
c  r13          0.46676E-02      18   0.70633E-08   0.14854E-08 0.19938E+00 
c  r23          0.39977E-02      18   0.70399E-08   0.12724E-08 0.19859E+00 
c  epsilon      0.10969E+02      11   0.33653E-08   0.99229E-02 0.16527E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.84801E-02 0.43445E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161987


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61362       0.0052575       0.0015076
v  Velocity[Y]            -0.57338         0.54422       0.0030806      0.00087322
v  Velocity[Z]               1.565          5.4386          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4386          4.3406          4.3632
v  Pressure                -36.401          360.04          87.671          169.87
v  r11                   0.0010611        0.081879        0.013074        0.018286
v  r22                   0.0011138         0.08265        0.013354        0.018646
v  r33                   0.0016397         0.17432        0.027251        0.037206
v  r12                    -0.01066        0.013576     -0.00023382     -0.00030931
v  r13                   -0.045535        0.052807      9.3201e-05       0.0010138
v  r23                   -0.046696        0.051214       3.049e-05      0.00057459
v  epsilon                0.069155          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099178      0.00092501       0.0017427
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2767         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767         0.71351         0.85284


 TIME FOR THE TIME STEP            10659:        0.77021E+02

===============================================================


 INSTANT    0.106600000E-01   TIME STEP NUMBER           10660
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.122592264E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.349311499E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.667180305E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.652742645E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.486407471E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81353E-03   0.44878E-02 0.19838E+01 
c  Velocity[X]                                      0.13796E-03 
c  Velocity[Y]                                      0.12811E-03 
c  Velocity[Z]                                      0.42218E-02 
c  Pressure     0.36236E-04     132   0.92224E-02   0.25559E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52502E-08   0.16569E-08 0.99159E-01 
c  r22          0.10852E-01      13   0.49324E-08   0.18241E-08 0.10125E+00 
c  r33          0.21860E-01      15   0.64788E-08   0.12646E-07 0.12704E+00 
c  r12          0.93865E-03      17   0.65990E-08   0.29913E-09 0.60538E+00 
c  r13          0.46676E-02      19   0.54866E-08   0.14913E-08 0.19961E+00 
c  r23          0.39977E-02      19   0.53290E-08   0.13106E-08 0.19930E+00 
c  epsilon      0.10969E+02      11   0.34548E-08   0.10247E-01 0.16761E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.83481E-02 0.43093E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61361       0.0052574       0.0015076
v  Velocity[Y]            -0.57342         0.54402       0.0030806      0.00087317
v  Velocity[Z]              1.5652          5.4386          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4386          4.3406          4.3632
v  Pressure                -36.482          360.02           87.65          169.85
v  r11                   0.0010611        0.081883        0.013074        0.018286
v  r22                   0.0011138        0.082649        0.013354        0.018646
v  r33                   0.0016397         0.17428        0.027251        0.037206
v  r12                    -0.01066        0.013576     -0.00023382     -0.00030931
v  r13                   -0.045537        0.052807      9.3202e-05       0.0010138
v  r23                   -0.046695        0.051216       3.049e-05      0.00057459
v  epsilon                0.069156          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9919e-05       0.0099177      0.00092501       0.0017427
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2766         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71351         0.85284


 TIME FOR THE TIME STEP            10660:        0.72515E+02

===============================================================


 INSTANT    0.106610000E-01   TIME STEP NUMBER           10661
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.576686762E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.129961871E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.421653889E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.303650560E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111556898E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81261E-03   0.45232E-02 0.19937E+01 
c  Velocity[X]                                      0.13773E-03 
c  Velocity[Y]                                      0.12777E-03 
c  Velocity[Z]                                      0.42577E-02 
c  Pressure     0.36475E-04     133   0.92828E-02   0.25729E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52253E-08   0.16215E-08 0.99014E-01 
c  r22          0.10852E-01      13   0.50076E-08   0.18430E-08 0.10177E+00 
c  r33          0.21860E-01      15   0.56931E-08   0.12566E-07 0.12737E+00 
c  r12          0.93865E-03      17   0.70078E-08   0.29970E-09 0.60788E+00 
c  r13          0.46676E-02      19   0.64103E-08   0.15102E-08 0.20047E+00 
c  r23          0.39977E-02      18   0.69849E-08   0.12955E-08 0.19945E+00 
c  epsilon      0.10969E+02      11   0.33688E-08   0.98179E-02 0.16387E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.83927E-02 0.43197E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61357       0.0052575       0.0015076
v  Velocity[Y]            -0.57363         0.54412       0.0030807      0.00087324
v  Velocity[Z]              1.5652          5.4386          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4386          4.3406          4.3632
v  Pressure                 -36.37          359.99          87.622          169.82
v  r11                   0.0010611        0.081888        0.013074        0.018286
v  r22                   0.0011138        0.082647        0.013354        0.018646
v  r33                   0.0016397         0.17428        0.027251        0.037206
v  r12                    -0.01066        0.013573     -0.00023382     -0.00030931
v  r13                   -0.045537        0.052806      9.3202e-05       0.0010138
v  r23                   -0.046694        0.051201       3.049e-05      0.00057459
v  epsilon                0.069157          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099178      0.00092501       0.0017427
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb              0.001785          5.2768         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71351         0.85284


 TIME FOR THE TIME STEP            10661:        0.75224E+02

===============================================================


 INSTANT    0.106620000E-01   TIME STEP NUMBER           10662
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205650880E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.193148088E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.654056621E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.328014801E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.461560355E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81226E-03   0.45582E-02 0.19978E+01 
c  Velocity[X]                                      0.13806E-03 
c  Velocity[Y]                                      0.12898E-03 
c  Velocity[Z]                                      0.42911E-02 
c  Pressure     0.36311E-04     132   0.92487E-02   0.25612E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54245E-08   0.16333E-08 0.99596E-01 
c  r22          0.10852E-01      13   0.51859E-08   0.18155E-08 0.10121E+00 
c  r33          0.21860E-01      15   0.59316E-08   0.12537E-07 0.12748E+00 
c  r12          0.93865E-03      17   0.69171E-08   0.29523E-09 0.60362E+00 
c  r13          0.46676E-02      19   0.56218E-08   0.14976E-08 0.19962E+00 
c  r23          0.39977E-02      19   0.52014E-08   0.12760E-08 0.19972E+00 
c  epsilon      0.10969E+02      11   0.33415E-08   0.10172E-01 0.17080E+00 
c  TempC        0.25716E+06      16   0.15165E-04   0.84398E-02 0.43313E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61361       0.0052574       0.0015076
v  Velocity[Y]            -0.57358         0.54432       0.0030806      0.00087319
v  Velocity[Z]              1.5652          5.4386          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4386          4.3406          4.3632
v  Pressure                -36.419          359.97          87.632          169.82
v  r11                   0.0010612        0.081891        0.013074        0.018286
v  r22                   0.0011138        0.082646        0.013354        0.018646
v  r33                   0.0016398         0.17431        0.027251        0.037206
v  r12                   -0.010661        0.013575     -0.00023382     -0.00030931
v  r13                   -0.045534        0.052805      9.3203e-05       0.0010138
v  r23                   -0.046694        0.051222      3.0491e-05      0.00057459
v  epsilon                0.069158          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099175      0.00092501       0.0017427
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017851           5.277         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71351         0.85284


 TIME FOR THE TIME STEP            10662:        0.77426E+02

===============================================================


 INSTANT    0.106630000E-01   TIME STEP NUMBER           10663
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.180393668E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.164305522E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.202739615E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.127146114E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.339827852E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81353E-03   0.45084E-02 0.19879E+01 
c  Velocity[X]                                      0.13759E-03 
c  Velocity[Y]                                      0.12842E-03 
c  Velocity[Z]                                      0.42424E-02 
c  Pressure     0.36252E-04     132   0.92311E-02   0.25571E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57363E-08   0.16141E-08 0.99206E-01 
c  r22          0.10852E-01      13   0.54875E-08   0.18210E-08 0.10161E+00 
c  r33          0.21860E-01      15   0.64518E-08   0.12389E-07 0.12727E+00 
c  r12          0.93865E-03      18   0.50392E-08   0.29943E-09 0.60974E+00 
c  r13          0.46676E-02      19   0.66463E-08   0.15040E-08 0.20027E+00 
c  r23          0.39977E-02      19   0.58701E-08   0.12634E-08 0.19853E+00 
c  epsilon      0.10969E+02      11   0.32535E-08   0.94672E-02 0.16299E+00 
c  TempC        0.25716E+06      16   0.15084E-04   0.83835E-02 0.43223E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61361       0.0052574       0.0015076
v  Velocity[Y]            -0.57371         0.54401       0.0030806      0.00087324
v  Velocity[Z]              1.5649          5.4386          4.3387          4.3625
v  ǁVelocityǁ               1.5787          5.4386          4.3406          4.3632
v  Pressure                -36.407          359.99          87.613          169.82
v  r11                   0.0010612        0.081896        0.013074        0.018286
v  r22                   0.0011138        0.082641        0.013354        0.018646
v  r33                   0.0016398         0.17429        0.027251        0.037206
v  r12                   -0.010658        0.013571     -0.00023382     -0.00030931
v  r13                   -0.045537        0.052805      9.3204e-05       0.0010138
v  r23                   -0.046694        0.051207      3.0491e-05      0.00057459
v  epsilon                0.069158          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9919e-05       0.0099176      0.00092502       0.0017427
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2763         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8763         0.71351         0.85284


 TIME FOR THE TIME STEP            10663:        0.77445E+02

===============================================================


 INSTANT    0.106640000E-01   TIME STEP NUMBER           10664
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.457374030E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.219522684E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111392979E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.182398179E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.373195930E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81246E-03   0.44938E-02 0.19875E+01 
c  Velocity[X]                                      0.13772E-03 
c  Velocity[Y]                                      0.12806E-03 
c  Velocity[Z]                                      0.42280E-02 
c  Pressure     0.36431E-04     132   0.92746E-02   0.25698E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52730E-08   0.16306E-08 0.99325E-01 
c  r22          0.10852E-01      13   0.55065E-08   0.18253E-08 0.10135E+00 
c  r33          0.21860E-01      15   0.61207E-08   0.12531E-07 0.12710E+00 
c  r12          0.93865E-03      18   0.52126E-08   0.29679E-09 0.60610E+00 
c  r13          0.46676E-02      19   0.69309E-08   0.14771E-08 0.19869E+00 
c  r23          0.39977E-02      19   0.56634E-08   0.12823E-08 0.19858E+00 
c  epsilon      0.10969E+02      11   0.33254E-08   0.98807E-02 0.16636E+00 
c  TempC        0.25716E+06      16   0.15175E-04   0.84310E-02 0.43308E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61356       0.0052574       0.0015075
v  Velocity[Y]            -0.57353         0.54402       0.0030806      0.00087324
v  Velocity[Z]              1.5649          5.4386          4.3387          4.3625
v  ǁVelocityǁ               1.5787          5.4386          4.3406          4.3632
v  Pressure                -36.428          359.96          87.623          169.81
v  r11                   0.0010612          0.0819        0.013074        0.018286
v  r22                   0.0011138        0.082641        0.013354        0.018646
v  r33                   0.0016398         0.17426        0.027251        0.037206
v  r12                   -0.010663        0.013574     -0.00023382     -0.00030931
v  r13                   -0.045535        0.052807      9.3205e-05       0.0010138
v  r23                   -0.046695        0.051194      3.0492e-05      0.00057459
v  epsilon                0.069159          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9919e-05       0.0099178      0.00092502       0.0017427
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2768         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71351         0.85284


 TIME FOR THE TIME STEP            10664:        0.74183E+02

===============================================================


 INSTANT    0.106650000E-01   TIME STEP NUMBER           10665
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190076145E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.281659196E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.103217302E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115546432E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.912952973E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81216E-03   0.45139E-02 0.19891E+01 
c  Velocity[X]                                      0.13784E-03 
c  Velocity[Y]                                      0.12848E-03 
c  Velocity[Z]                                      0.42476E-02 
c  Pressure     0.35798E-04     132   0.91115E-02   0.25250E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51893E-08   0.16273E-08 0.98969E-01 
c  r22          0.10852E-01      13   0.55720E-08   0.18154E-08 0.10074E+00 
c  r33          0.21860E-01      15   0.60349E-08   0.12390E-07 0.12616E+00 
c  r12          0.93865E-03      18   0.54326E-08   0.29578E-09 0.60672E+00 
c  r13          0.46676E-02      19   0.67142E-08   0.14914E-08 0.19857E+00 
c  r23          0.39977E-02      18   0.70548E-08   0.12566E-08 0.19688E+00 
c  epsilon      0.10969E+02      11   0.35068E-08   0.98697E-02 0.16591E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.84152E-02 0.43244E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61361       0.0052574       0.0015075
v  Velocity[Y]            -0.57356         0.54414       0.0030807      0.00087326
v  Velocity[Z]               1.565          5.4386          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4386          4.3406          4.3632
v  Pressure                -36.393          360.09          87.691          169.91
v  r11                   0.0010612        0.081901        0.013074        0.018286
v  r22                   0.0011138        0.082643        0.013354        0.018646
v  r33                   0.0016398         0.17428        0.027251        0.037206
v  r12                   -0.010664        0.013579     -0.00023382     -0.00030931
v  r13                   -0.045536        0.052805      9.3205e-05       0.0010138
v  r23                   -0.046695        0.051188      3.0492e-05      0.00057459
v  epsilon                 0.06916          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099175      0.00092502       0.0017427
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2766         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71351         0.85284


 TIME FOR THE TIME STEP            10665:        0.75699E+02

===============================================================


 INSTANT    0.106660000E-01   TIME STEP NUMBER           10666
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.102712681E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.259875787E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.827276382E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.653822149E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.146965481E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81353E-03   0.45139E-02 0.19895E+01 
c  Velocity[X]                                      0.13745E-03 
c  Velocity[Y]                                      0.12849E-03 
c  Velocity[Z]                                      0.42480E-02 
c  Pressure     0.36379E-04     133   0.92598E-02   0.25660E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51140E-08   0.16204E-08 0.98981E-01 
c  r22          0.10852E-01      13   0.56127E-08   0.18186E-08 0.10069E+00 
c  r33          0.21860E-01      15   0.53289E-08   0.12424E-07 0.12635E+00 
c  r12          0.93865E-03      18   0.54731E-08   0.29397E-09 0.60112E+00 
c  r13          0.46676E-02      18   0.70823E-08   0.15036E-08 0.19889E+00 
c  r23          0.39977E-02      19   0.54275E-08   0.12740E-08 0.19784E+00 
c  epsilon      0.10969E+02      11   0.35456E-08   0.99491E-02 0.16667E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.83759E-02 0.43164E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61358       0.0052574       0.0015075
v  Velocity[Y]            -0.57342         0.54431       0.0030806      0.00087325
v  Velocity[Z]              1.5653          5.4386          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4386          4.3406          4.3632
v  Pressure                -36.438          360.03          87.658          169.86
v  r11                   0.0010612        0.081905        0.013074        0.018286
v  r22                   0.0011138        0.082644        0.013354        0.018646
v  r33                   0.0016398          0.1743        0.027251        0.037206
v  r12                   -0.010661        0.013585     -0.00023382     -0.00030931
v  r13                   -0.045538        0.052806      9.3206e-05       0.0010138
v  r23                   -0.046695        0.051219      3.0492e-05      0.00057459
v  epsilon                0.069161          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099175      0.00092502       0.0017427
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2764         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8764         0.71351         0.85284


 TIME FOR THE TIME STEP            10666:        0.75688E+02

===============================================================


 INSTANT    0.106670000E-01   TIME STEP NUMBER           10667
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190397742E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.394978531E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.993342623E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.216945548E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183100376E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81239E-03   0.44903E-02 0.19846E+01 
c  Velocity[X]                                      0.13752E-03 
c  Velocity[Y]                                      0.12744E-03 
c  Velocity[Z]                                      0.42253E-02 
c  Pressure     0.36577E-04     133   0.93173E-02   0.25800E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49483E-08   0.16300E-08 0.99558E-01 
c  r22          0.10852E-01      13   0.52483E-08   0.18034E-08 0.10068E+00 
c  r33          0.21860E-01      15   0.60260E-08   0.12441E-07 0.12688E+00 
c  r12          0.93865E-03      18   0.52530E-08   0.30026E-09 0.60886E+00 
c  r13          0.46676E-02      19   0.53692E-08   0.14913E-08 0.19921E+00 
c  r23          0.39977E-02      19   0.53178E-08   0.12790E-08 0.19937E+00 
c  epsilon      0.10969E+02      11   0.33582E-08   0.99549E-02 0.16833E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.84276E-02 0.43317E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61356       0.0052574       0.0015075
v  Velocity[Y]            -0.57347         0.54415       0.0030806      0.00087327
v  Velocity[Z]              1.5652          5.4386          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4386          4.3406          4.3632
v  Pressure                -36.378          359.98          87.619          169.82
v  r11                   0.0010612        0.081909        0.013074        0.018286
v  r22                   0.0011138        0.082645        0.013354        0.018646
v  r33                   0.0016399         0.17434        0.027251        0.037206
v  r12                   -0.010663        0.013587     -0.00023382     -0.00030931
v  r13                   -0.045535        0.052806      9.3207e-05       0.0010138
v  r23                   -0.046695        0.051206      3.0493e-05      0.00057459
v  epsilon                0.069161          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099175      0.00092502       0.0017427
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2768         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71351         0.85284


 TIME FOR THE TIME STEP            10667:        0.76396E+02

===============================================================


 INSTANT    0.106680000E-01   TIME STEP NUMBER           10668
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.265699421E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.778991584E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.366346878E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.501818819E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.252610242E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81325E-03   0.45263E-02 0.19919E+01 
c  Velocity[X]                                      0.13828E-03 
c  Velocity[Y]                                      0.12864E-03 
c  Velocity[Z]                                      0.42594E-02 
c  Pressure     0.36378E-04     132   0.92585E-02   0.25660E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.47660E-08   0.15904E-08 0.98162E-01 
c  r22          0.10852E-01      13   0.50194E-08   0.17878E-08 0.10077E+00 
c  r33          0.21860E-01      15   0.60807E-08   0.12237E-07 0.12609E+00 
c  r12          0.93865E-03      17   0.70307E-08   0.29042E-09 0.59899E+00 
c  r13          0.46676E-02      19   0.59272E-08   0.14691E-08 0.19835E+00 
c  r23          0.39977E-02      19   0.62116E-08   0.12543E-08 0.19651E+00 
c  epsilon      0.10969E+02      11   0.33089E-08   0.96832E-02 0.16418E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.84263E-02 0.43354E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61362       0.0052575       0.0015076
v  Velocity[Y]            -0.57347         0.54427       0.0030807      0.00087332
v  Velocity[Z]              1.5651          5.4386          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4386          4.3406          4.3632
v  Pressure                -36.453          360.02           87.65          169.85
v  r11                   0.0010612        0.081905        0.013074        0.018286
v  r22                   0.0011138        0.082645        0.013354        0.018646
v  r33                   0.0016399         0.17433        0.027251        0.037206
v  r12                   -0.010667        0.013587     -0.00023382     -0.00030931
v  r13                   -0.045533        0.052805      9.3207e-05       0.0010138
v  r23                   -0.046696        0.051205      3.0493e-05      0.00057459
v  epsilon                0.069162          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099176      0.00092502       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2772         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71351         0.85284


 TIME FOR THE TIME STEP            10668:        0.78192E+02

===============================================================


 INSTANT    0.106690000E-01   TIME STEP NUMBER           10669
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.541096227E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162656100E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.148549137E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.932860005E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.626007911E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81322E-03   0.45272E-02 0.19928E+01 
c  Velocity[X]                                      0.13782E-03 
c  Velocity[Y]                                      0.12776E-03 
c  Velocity[Z]                                      0.42616E-02 
c  Pressure     0.36333E-04     131   0.92467E-02   0.25628E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49325E-08   0.16260E-08 0.99192E-01 
c  r22          0.10852E-01      13   0.53395E-08   0.17840E-08 0.10072E+00 
c  r33          0.21860E-01      15   0.65331E-08   0.12310E-07 0.12654E+00 
c  r12          0.93865E-03      18   0.55434E-08   0.29494E-09 0.60417E+00 
c  r13          0.46676E-02      20   0.59367E-08   0.14724E-08 0.19872E+00 
c  r23          0.39977E-02      20   0.60611E-08   0.12714E-08 0.19774E+00 
c  epsilon      0.10969E+02      11   0.34948E-08   0.96095E-02 0.16335E+00 
c  TempC        0.25716E+06      16   0.15142E-04   0.84196E-02 0.43287E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61362       0.0052574       0.0015076
v  Velocity[Y]            -0.57358         0.54398       0.0030807       0.0008733
v  Velocity[Z]              1.5651          5.4386          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4386          4.3406          4.3632
v  Pressure                -36.416          360.01           87.63          169.84
v  r11                   0.0010612        0.081902        0.013074        0.018286
v  r22                   0.0011138        0.082646        0.013354        0.018646
v  r33                   0.0016399         0.17429        0.027251        0.037206
v  r12                   -0.010664        0.013586     -0.00023382     -0.00030931
v  r13                   -0.045537        0.052807      9.3207e-05       0.0010138
v  r23                   -0.046696        0.051204      3.0494e-05      0.00057459
v  epsilon                0.069163          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099175      0.00092502       0.0017427
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2779         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71351         0.85283


 TIME FOR THE TIME STEP            10669:        0.73339E+02

===============================================================


 INSTANT    0.106700000E-01   TIME STEP NUMBER           10670
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.519855549E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138890467E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.459450909E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129405152E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.466312358E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      45   0.81175E-03   0.45059E-02 0.19880E+01 
c  Velocity[X]                                      0.13817E-03 
c  Velocity[Y]                                      0.12826E-03 
c  Velocity[Z]                                      0.42395E-02 
c  Pressure     0.36080E-04     132   0.91840E-02   0.25448E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49329E-08   0.16336E-08 0.99450E-01 
c  r22          0.10852E-01      13   0.53678E-08   0.18190E-08 0.10152E+00 
c  r33          0.21860E-01      15   0.62484E-08   0.12442E-07 0.12717E+00 
c  r12          0.93865E-03      18   0.59113E-08   0.29752E-09 0.60432E+00 
c  r13          0.46676E-02      19   0.67497E-08   0.14838E-08 0.19968E+00 
c  r23          0.39977E-02      19   0.67473E-08   0.12574E-08 0.19754E+00 
c  epsilon      0.10969E+02      11   0.34889E-08   0.99537E-02 0.16672E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.83798E-02 0.43137E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61356       0.0052573       0.0015075
v  Velocity[Y]            -0.57354         0.54403       0.0030805      0.00087322
v  Velocity[Z]               1.565          5.4387          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4387          4.3406          4.3632
v  Pressure                -36.425          359.93          87.587          169.77
v  r11                   0.0010612        0.081904        0.013074        0.018286
v  r22                   0.0011139        0.082647        0.013354        0.018646
v  r33                   0.0016399          0.1743        0.027251        0.037206
v  r12                   -0.010664        0.013588     -0.00023382     -0.00030931
v  r13                   -0.045534         0.05281      9.3208e-05       0.0010138
v  r23                   -0.046696        0.051232      3.0494e-05      0.00057459
v  epsilon                0.069163           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099176      0.00092502       0.0017427
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2781         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71351         0.85284


 TIME FOR THE TIME STEP            10670:        0.76696E+02

===============================================================


 INSTANT    0.106710000E-01   TIME STEP NUMBER           10671
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242840926E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.110004729E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.274112699E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283012883E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.950812962E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81294E-03   0.45397E-02 0.19949E+01 
c  Velocity[X]                                      0.13837E-03 
c  Velocity[Y]                                      0.12909E-03 
c  Velocity[Z]                                      0.42723E-02 
c  Pressure     0.36448E-04     133   0.92810E-02   0.25709E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49456E-08   0.16408E-08 0.99697E-01 
c  r22          0.10852E-01      13   0.55462E-08   0.18197E-08 0.10180E+00 
c  r33          0.21860E-01      15   0.64989E-08   0.12455E-07 0.12757E+00 
c  r12          0.93865E-03      18   0.56583E-08   0.29439E-09 0.60554E+00 
c  r13          0.46676E-02      19   0.67981E-08   0.14827E-08 0.19998E+00 
c  r23          0.39977E-02      20   0.63028E-08   0.12756E-08 0.19864E+00 
c  epsilon      0.10969E+02      11   0.34998E-08   0.98233E-02 0.16573E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.83931E-02 0.43262E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63331         0.61363       0.0052574       0.0015076
v  Velocity[Y]             -0.5737          0.5442       0.0030807       0.0008733
v  Velocity[Z]              1.5648          5.4387          4.3387          4.3625
v  ǁVelocityǁ               1.5786          5.4387          4.3406          4.3632
v  Pressure                -36.408          360.03          87.646          169.86
v  r11                   0.0010612        0.081906        0.013074        0.018286
v  r22                   0.0011139        0.082643        0.013354        0.018646
v  r33                     0.00164         0.17433        0.027251        0.037206
v  r12                   -0.010661        0.013588     -0.00023382     -0.00030931
v  r13                   -0.045533        0.052811      9.3208e-05       0.0010138
v  r23                   -0.046696        0.051222      3.0495e-05      0.00057459
v  epsilon                0.069164          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099177      0.00092502       0.0017427
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2782         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71351         0.85284


 TIME FOR THE TIME STEP            10671:        0.75362E+02

===============================================================


 INSTANT    0.106720000E-01   TIME STEP NUMBER           10672
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.356385575E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.891817397E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.207640360E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.675275243E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.705869021E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81312E-03   0.45039E-02 0.19874E+01 
c  Velocity[X]                                      0.13748E-03 
c  Velocity[Y]                                      0.12853E-03 
c  Velocity[Z]                                      0.42379E-02 
c  Pressure     0.36770E-04     133   0.93550E-02   0.25936E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51915E-08   0.16500E-08 0.99803E-01 
c  r22          0.10852E-01      13   0.54805E-08   0.18396E-08 0.10157E+00 
c  r33          0.21860E-01      15   0.59326E-08   0.12706E-07 0.12820E+00 
c  r12          0.93865E-03      18   0.58930E-08   0.30248E-09 0.60772E+00 
c  r13          0.46676E-02      19   0.73306E-08   0.15066E-08 0.20010E+00 
c  r23          0.39977E-02      20   0.65013E-08   0.12952E-08 0.20052E+00 
c  epsilon      0.10969E+02      11   0.34010E-08   0.10295E-01 0.17112E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.83927E-02 0.43233E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63333         0.61361       0.0052574       0.0015076
v  Velocity[Y]            -0.57359         0.54441       0.0030806      0.00087328
v  Velocity[Z]               1.565          5.4387          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4387          4.3406          4.3632
v  Pressure                -36.449          360.01          87.642          169.84
v  r11                   0.0010612        0.081908        0.013074        0.018286
v  r22                   0.0011139        0.082645        0.013354        0.018646
v  r33                     0.00164          0.1743        0.027251        0.037206
v  r12                   -0.010658        0.013588     -0.00023382     -0.00030931
v  r13                   -0.045536        0.052813      9.3209e-05       0.0010138
v  r23                   -0.046697        0.051205      3.0496e-05      0.00057459
v  epsilon                0.069165          271.25          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099178      0.00092502       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2776         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71351         0.85284


 TIME FOR THE TIME STEP            10672:        0.78835E+02

===============================================================


 INSTANT    0.106730000E-01   TIME STEP NUMBER           10673
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149886473E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.606851084E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.129918831E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.544505961E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.465215140E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81150E-03   0.45152E-02 0.19916E+01 
c  Velocity[X]                                      0.13790E-03 
c  Velocity[Y]                                      0.12873E-03 
c  Velocity[Z]                                      0.42486E-02 
c  Pressure     0.36205E-04     133   0.92239E-02   0.25538E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55140E-08   0.16118E-08 0.98931E-01 
c  r22          0.10852E-01      13   0.56201E-08   0.18117E-08 0.10128E+00 
c  r33          0.21860E-01      15   0.57471E-08   0.12357E-07 0.12675E+00 
c  r12          0.93865E-03      18   0.64794E-08   0.29399E-09 0.60383E+00 
c  r13          0.46676E-02      19   0.71706E-08   0.15081E-08 0.20029E+00 
c  r23          0.39977E-02      20   0.61301E-08   0.12643E-08 0.19755E+00 
c  epsilon      0.10969E+02      10   0.54101E-08   0.96489E-02 0.16351E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.84540E-02 0.43374E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61359       0.0052574       0.0015076
v  Velocity[Y]            -0.57365         0.54409       0.0030807      0.00087329
v  Velocity[Z]              1.5651          5.4387          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4387          4.3406          4.3632
v  Pressure                -36.423          360.04          87.643          169.85
v  r11                   0.0010613         0.08191        0.013074        0.018286
v  r22                   0.0011139        0.082646        0.013354        0.018646
v  r33                     0.00164         0.17429        0.027251        0.037206
v  r12                   -0.010663        0.013587     -0.00023382     -0.00030931
v  r13                   -0.045535        0.052812      9.3209e-05       0.0010138
v  r23                   -0.046698        0.051228      3.0495e-05      0.00057459
v  epsilon                0.069166          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099177      0.00092502       0.0017427
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2777         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71351         0.85284


 TIME FOR THE TIME STEP            10673:        0.79599E+02

===============================================================


 INSTANT    0.106740000E-01   TIME STEP NUMBER           10674
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.283626791E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.721755568E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.515153471E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.626491152E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.771324842E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81275E-03   0.45454E-02 0.19961E+01 
c  Velocity[X]                                      0.13838E-03 
c  Velocity[Y]                                      0.12940E-03 
c  Velocity[Z]                                      0.42776E-02 
c  Pressure     0.36131E-04     132   0.92009E-02   0.25486E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52194E-08   0.16267E-08 0.99233E-01 
c  r22          0.10852E-01      13   0.52061E-08   0.18247E-08 0.10096E+00 
c  r33          0.21860E-01      15   0.56879E-08   0.12510E-07 0.12677E+00 
c  r12          0.93865E-03      18   0.65649E-08   0.29573E-09 0.60570E+00 
c  r13          0.46676E-02      20   0.58309E-08   0.14908E-08 0.19939E+00 
c  r23          0.39977E-02      20   0.67992E-08   0.12708E-08 0.19764E+00 
c  epsilon      0.10969E+02      11   0.32914E-08   0.10023E-01 0.16470E+00 
c  TempC        0.25716E+06      16   0.15169E-04   0.85089E-02 0.43487E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63327          0.6136       0.0052574       0.0015076
v  Velocity[Y]            -0.57352         0.54415       0.0030806      0.00087328
v  Velocity[Z]              1.5652          5.4387          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4387          4.3406          4.3632
v  Pressure                -36.439             360          87.629          169.83
v  r11                   0.0010613        0.081908        0.013074        0.018286
v  r22                   0.0011139        0.082647        0.013354        0.018646
v  r33                     0.00164          0.1743        0.027251        0.037206
v  r12                   -0.010662        0.013589     -0.00023382     -0.00030931
v  r13                   -0.045533        0.052811      9.3209e-05       0.0010138
v  r23                   -0.046699        0.051217      3.0496e-05      0.00057459
v  epsilon                0.069166          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099176      0.00092503       0.0017427
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2779         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71351         0.85284


 TIME FOR THE TIME STEP            10674:        0.88489E+02

===============================================================


 INSTANT    0.106750000E-01   TIME STEP NUMBER           10675
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.896176812E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.328927569E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.260294174E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.574822682E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161161297E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81261E-03   0.45025E-02 0.19877E+01 
c  Velocity[X]                                      0.13806E-03 
c  Velocity[Y]                                      0.12731E-03 
c  Velocity[Z]                                      0.42371E-02 
c  Pressure     0.36287E-04     135   0.92373E-02   0.25595E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55945E-08   0.16414E-08 0.99435E-01 
c  r22          0.10852E-01      13   0.52244E-08   0.18187E-08 0.10126E+00 
c  r33          0.21860E-01      15   0.55255E-08   0.12490E-07 0.12694E+00 
c  r12          0.93865E-03      18   0.64994E-08   0.29933E-09 0.60774E+00 
c  r13          0.46676E-02      19   0.71634E-08   0.14973E-08 0.19987E+00 
c  r23          0.39977E-02      20   0.63311E-08   0.12852E-08 0.19819E+00 
c  epsilon      0.10969E+02      11   0.32820E-08   0.98899E-02 0.16618E+00 
c  TempC        0.25716E+06      16   0.15102E-04   0.83699E-02 0.43134E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63327          0.6136       0.0052575       0.0015076
v  Velocity[Y]            -0.57364         0.54422       0.0030807       0.0008733
v  Velocity[Z]              1.5649          5.4387          4.3387          4.3625
v  ǁVelocityǁ               1.5787          5.4387          4.3406          4.3632
v  Pressure                -36.424          360.06          87.646          169.86
v  r11                   0.0010613        0.081913        0.013074        0.018286
v  r22                   0.0011139        0.082647        0.013354        0.018646
v  r33                     0.00164         0.17432        0.027251        0.037206
v  r12                   -0.010658        0.013583     -0.00023382     -0.00030931
v  r13                   -0.045536         0.05281       9.321e-05       0.0010138
v  r23                     -0.0467          0.0512      3.0497e-05      0.00057459
v  epsilon                0.069167          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099177      0.00092503       0.0017427
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2775         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71351         0.85284


 TIME FOR THE TIME STEP            10675:        0.24099E+03

===============================================================


 INSTANT    0.106760000E-01   TIME STEP NUMBER           10676
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.128231379E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.381661961E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.131126342E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.588953484E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.126918010E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81280E-03   0.45108E-02 0.19877E+01 
c  Velocity[X]                                      0.13727E-03 
c  Velocity[Y]                                      0.12845E-03 
c  Velocity[Z]                                      0.42451E-02 
c  Pressure     0.36708E-04     133   0.93473E-02   0.25892E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56432E-08   0.16007E-08 0.98339E-01 
c  r22          0.10852E-01      13   0.53456E-08   0.18110E-08 0.10092E+00 
c  r33          0.21860E-01      15   0.58821E-08   0.12372E-07 0.12631E+00 
c  r12          0.93865E-03      18   0.67881E-08   0.30154E-09 0.60521E+00 
c  r13          0.46676E-02      19   0.69567E-08   0.14862E-08 0.19859E+00 
c  r23          0.39977E-02      19   0.67480E-08   0.12634E-08 0.19689E+00 
c  epsilon      0.10969E+02      11   0.34478E-08   0.99414E-02 0.16685E+00 
c  TempC        0.25716E+06      16   0.15169E-04   0.83794E-02 0.43211E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61358       0.0052574       0.0015075
v  Velocity[Y]            -0.57363         0.54434       0.0030806      0.00087327
v  Velocity[Z]              1.5651          5.4387          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4387          4.3406          4.3632
v  Pressure                -36.457          359.99          87.633          169.83
v  r11                   0.0010613         0.08191        0.013074        0.018286
v  r22                   0.0011139        0.082646        0.013354        0.018646
v  r33                   0.0016401         0.17431        0.027251        0.037206
v  r12                   -0.010657        0.013577     -0.00023382     -0.00030931
v  r13                   -0.045534         0.05281      9.3211e-05       0.0010138
v  r23                   -0.046701         0.05119      3.0497e-05      0.00057459
v  epsilon                0.069168          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099177      0.00092503       0.0017427
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2778         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71351         0.85284


 TIME FOR THE TIME STEP            10676:        0.27481E+03

===============================================================


 INSTANT    0.106770000E-01   TIME STEP NUMBER           10677
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.461577655E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.101232811E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.355194777E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.147614301E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.211185379E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81198E-03   0.45183E-02 0.19907E+01 
c  Velocity[X]                                      0.13812E-03 
c  Velocity[Y]                                      0.12845E-03 
c  Velocity[Z]                                      0.42518E-02 
c  Pressure     0.35962E-04     133   0.91608E-02   0.25365E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54682E-08   0.16368E-08 0.99403E-01 
c  r22          0.10852E-01      13   0.55160E-08   0.18351E-08 0.10166E+00 
c  r33          0.21860E-01      15   0.60943E-08   0.12485E-07 0.12721E+00 
c  r12          0.93865E-03      19   0.57012E-08   0.29438E-09 0.60612E+00 
c  r13          0.46676E-02      20   0.67379E-08   0.14868E-08 0.19976E+00 
c  r23          0.39977E-02      19   0.63856E-08   0.12662E-08 0.19812E+00 
c  epsilon      0.10969E+02      11   0.33519E-08   0.10100E-01 0.16788E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.83900E-02 0.43227E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63329         0.61359       0.0052575       0.0015076
v  Velocity[Y]            -0.57364         0.54415       0.0030807      0.00087332
v  Velocity[Z]              1.5651          5.4387          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4387          4.3406          4.3632
v  Pressure                -36.405             360          87.616          169.83
v  r11                   0.0010613         0.08191        0.013074        0.018286
v  r22                   0.0011139        0.082645        0.013354        0.018646
v  r33                   0.0016401         0.17428        0.027251        0.037206
v  r12                   -0.010654        0.013572     -0.00023382     -0.00030931
v  r13                   -0.045535        0.052809      9.3211e-05       0.0010138
v  r23                   -0.046703         0.05121      3.0498e-05      0.00057459
v  epsilon                0.069168           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099177      0.00092503       0.0017427
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71351         0.85284


 TIME FOR THE TIME STEP            10677:        0.50185E+03

===============================================================


 INSTANT    0.106780000E-01   TIME STEP NUMBER           10678
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.845462882E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.870989962E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.322554464E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.152655271E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242936511E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81343E-03   0.44941E-02 0.19848E+01 
c  Velocity[X]                                      0.13816E-03 
c  Velocity[Y]                                      0.12832E-03 
c  Velocity[Z]                                      0.42276E-02 
c  Pressure     0.36084E-04     131   0.91855E-02   0.25452E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54025E-08   0.16395E-08 0.99394E-01 
c  r22          0.10852E-01      13   0.52632E-08   0.18234E-08 0.10117E+00 
c  r33          0.21860E-01      15   0.70484E-08   0.12523E-07 0.12730E+00 
c  r12          0.93865E-03      18   0.69903E-08   0.29637E-09 0.60360E+00 
c  r13          0.46676E-02      20   0.57204E-08   0.15058E-08 0.20034E+00 
c  r23          0.39977E-02      20   0.58227E-08   0.12905E-08 0.19953E+00 
c  epsilon      0.10969E+02      11   0.33769E-08   0.10254E-01 0.17207E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.83390E-02 0.43080E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63328          0.6136       0.0052574       0.0015076
v  Velocity[Y]            -0.57367         0.54428       0.0030806      0.00087327
v  Velocity[Z]              1.5649          5.4387          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4387          4.3406          4.3632
v  Pressure                -36.453          359.96          87.605           169.8
v  r11                   0.0010613        0.081905        0.013074        0.018286
v  r22                   0.0011139        0.082645        0.013354        0.018646
v  r33                   0.0016401         0.17429        0.027251        0.037206
v  r12                   -0.010654        0.013574     -0.00023382     -0.00030931
v  r13                   -0.045537        0.052807      9.3212e-05       0.0010138
v  r23                   -0.046704          0.0512      3.0498e-05      0.00057459
v  epsilon                0.069169          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099177      0.00092503       0.0017427
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2785         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71351         0.85284


 TIME FOR THE TIME STEP            10678:        0.54847E+03

===============================================================


 INSTANT    0.106790000E-01   TIME STEP NUMBER           10679
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162515645E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.138724967E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.166435101E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145325483E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201552877E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81163E-03   0.45154E-02 0.19913E+01 
c  Velocity[X]                                      0.13854E-03 
c  Velocity[Y]                                      0.12767E-03 
c  Velocity[Z]                                      0.42492E-02 
c  Pressure     0.36263E-04     136   0.92269E-02   0.25579E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54200E-08   0.16271E-08 0.98825E-01 
c  r22          0.10852E-01      13   0.51267E-08   0.18313E-08 0.10117E+00 
c  r33          0.21860E-01      15   0.61592E-08   0.12494E-07 0.12645E+00 
c  r12          0.93865E-03      18   0.69254E-08   0.29647E-09 0.60478E+00 
c  r13          0.46676E-02      19   0.69586E-08   0.15010E-08 0.19957E+00 
c  r23          0.39977E-02      20   0.61217E-08   0.12774E-08 0.19794E+00 
c  epsilon      0.10969E+02      11   0.33070E-08   0.99107E-02 0.16478E+00 
c  TempC        0.25716E+06      16   0.15110E-04   0.85156E-02 0.43542E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63336          0.6136       0.0052575       0.0015076
v  Velocity[Y]            -0.57376         0.54399       0.0030806      0.00087327
v  Velocity[Z]               1.565          5.4387          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4387          4.3406          4.3632
v  Pressure                -36.386          360.02          87.655          169.86
v  r11                   0.0010613        0.081905        0.013074        0.018286
v  r22                   0.0011139        0.082639        0.013354        0.018646
v  r33                   0.0016401         0.17432        0.027251        0.037206
v  r12                   -0.010659        0.013574     -0.00023382     -0.00030931
v  r13                   -0.045534        0.052805      9.3212e-05       0.0010138
v  r23                   -0.046706        0.051194      3.0498e-05      0.00057459
v  epsilon                 0.06917          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05       0.0099176      0.00092503       0.0017427
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2776         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71351         0.85284


 TIME FOR THE TIME STEP            10679:        0.12876E+03

===============================================================


 INSTANT    0.106800000E-01   TIME STEP NUMBER           10680
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.207720726E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.764069777E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.136728783E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.170322892E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.337665090E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81324E-03   0.45201E-02 0.19895E+01 
c  Velocity[X]                                      0.13765E-03 
c  Velocity[Y]                                      0.12829E-03 
c  Velocity[Z]                                      0.42542E-02 
c  Pressure     0.36508E-04     132   0.92869E-02   0.25751E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53724E-08   0.16288E-08 0.99165E-01 
c  r22          0.10852E-01      13   0.55838E-08   0.18090E-08 0.10086E+00 
c  r33          0.21860E-01      15   0.56676E-08   0.12429E-07 0.12656E+00 
c  r12          0.93865E-03      18   0.71708E-08   0.29569E-09 0.60261E+00 
c  r13          0.46676E-02      19   0.70254E-08   0.15149E-08 0.20007E+00 
c  r23          0.39977E-02      20   0.60469E-08   0.12848E-08 0.19846E+00 
c  epsilon      0.10969E+02      11   0.35838E-08   0.99412E-02 0.16479E+00 
c  TempC        0.25716E+06      16   0.15171E-04   0.84163E-02 0.43302E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338          0.6136       0.0052575       0.0015076
v  Velocity[Y]            -0.57363         0.54406       0.0030805      0.00087325
v  Velocity[Z]              1.5652          5.4387          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4387          4.3406          4.3632
v  Pressure                -36.485             360          87.659          169.85
v  r11                   0.0010613        0.081911        0.013074        0.018286
v  r22                   0.0011139        0.082638        0.013354        0.018646
v  r33                   0.0016402         0.17429        0.027251        0.037206
v  r12                    -0.01066        0.013575     -0.00023382     -0.00030931
v  r13                   -0.045533        0.052805      9.3213e-05       0.0010138
v  r23                   -0.046708        0.051223      3.0499e-05      0.00057459
v  epsilon                0.069171          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099177      0.00092503       0.0017427
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2769         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71351         0.85284


 TIME FOR THE TIME STEP            10680:        0.19374E+03

===============================================================


 INSTANT    0.106810000E-01   TIME STEP NUMBER           10681
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.167702157E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.136894168E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.343639991E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.154801749E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.747479392E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81301E-03   0.45157E-02 0.19913E+01 
c  Velocity[X]                                      0.13865E-03 
c  Velocity[Y]                                      0.12901E-03 
c  Velocity[Z]                                      0.42481E-02 
c  Pressure     0.36513E-04     133   0.92962E-02   0.25754E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57169E-08   0.16318E-08 0.99333E-01 
c  r22          0.10852E-01      13   0.54051E-08   0.18170E-08 0.10114E+00 
c  r33          0.21860E-01      15   0.57981E-08   0.12489E-07 0.12718E+00 
c  r12          0.93865E-03      19   0.54897E-08   0.29753E-09 0.60605E+00 
c  r13          0.46676E-02      19   0.71363E-08   0.15147E-08 0.20035E+00 
c  r23          0.39977E-02      20   0.57893E-08   0.12978E-08 0.19994E+00 
c  epsilon      0.10969E+02      11   0.35566E-08   0.97172E-02 0.16378E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.83438E-02 0.43099E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161985


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63317         0.61358       0.0052575       0.0015076
v  Velocity[Y]             -0.5738         0.54421       0.0030806      0.00087328
v  Velocity[Z]              1.5651          5.4388          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4388          4.3406          4.3632
v  Pressure                -36.442          360.05          87.633          169.86
v  r11                   0.0010613        0.081909        0.013074        0.018286
v  r22                    0.001114        0.082639        0.013354        0.018646
v  r33                   0.0016402         0.17427        0.027251        0.037206
v  r12                   -0.010659        0.013577     -0.00023382     -0.00030931
v  r13                   -0.045537        0.052803      9.3213e-05       0.0010138
v  r23                   -0.046709        0.051204        3.05e-05      0.00057459
v  epsilon                0.069171           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9933e-05       0.0099175      0.00092503       0.0017427
v  CourantNb               0.44264             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2772         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71351         0.85283


 TIME FOR THE TIME STEP            10681:        0.53901E+03

===============================================================


 INSTANT    0.106820000E-01   TIME STEP NUMBER           10682
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.137795863E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.280487967E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934918E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.601711934E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.121268115E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237989971E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81275E-03   0.45244E-02 0.19942E+01 
c  Velocity[X]                                      0.13786E-03 
c  Velocity[Y]                                      0.12850E-03 
c  Velocity[Z]                                      0.42580E-02 
c  Pressure     0.36239E-04     131   0.92313E-02   0.25561E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54477E-08   0.16775E-08 0.10041E+00 
c  r22          0.10852E-01      13   0.55810E-08   0.18131E-08 0.10124E+00 
c  r33          0.21860E-01      15   0.51470E-08   0.12611E-07 0.12769E+00 
c  r12          0.93865E-03      18   0.66910E-08   0.30470E-09 0.61128E+00 
c  r13          0.46676E-02      19   0.63018E-08   0.14799E-08 0.19891E+00 
c  r23          0.39977E-02      19   0.69576E-08   0.13268E-08 0.20199E+00 
c  epsilon      0.10969E+02      11   0.33526E-08   0.99949E-02 0.16677E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83923E-02 0.43189E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63324         0.61353       0.0052575       0.0015076
v  Velocity[Y]            -0.57373         0.54444       0.0030806      0.00087325
v  Velocity[Z]              1.5653          5.4387          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4387          4.3406          4.3632
v  Pressure                -36.427          359.98          87.621          169.81
v  r11                   0.0010614        0.081906        0.013074        0.018286
v  r22                    0.001114         0.08264        0.013354        0.018646
v  r33                   0.0016402         0.17429        0.027251        0.037206
v  r12                    -0.01066         0.01358     -0.00023382     -0.00030931
v  r13                   -0.045534        0.052804      9.3213e-05       0.0010138
v  r23                    -0.04671        0.051189        3.05e-05      0.00057459
v  epsilon                0.069172          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099176      0.00092503       0.0017427
v  CourantNb               0.44265             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2781         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71351         0.85283


 TIME FOR THE TIME STEP            10682:        0.43482E+03

===============================================================


 INSTANT    0.106830000E-01   TIME STEP NUMBER           10683
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.204532399E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.398601595E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.570327170E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.194616231E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276593610E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81257E-03   0.45152E-02 0.19909E+01 
c  Velocity[X]                                      0.13867E-03 
c  Velocity[Y]                                      0.12898E-03 
c  Velocity[Z]                                      0.42476E-02 
c  Pressure     0.36171E-04     132   0.92104E-02   0.25513E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.48332E-08   0.17106E-08 0.10162E+00 
c  r22          0.10852E-01      13   0.53981E-08   0.18526E-08 0.10212E+00 
c  r33          0.21860E-01      15   0.64071E-08   0.12901E-07 0.12920E+00 
c  r12          0.93865E-03      18   0.67026E-08   0.30641E-09 0.61559E+00 
c  r13          0.46676E-02      19   0.59961E-08   0.15008E-08 0.20006E+00 
c  r23          0.39977E-02      19   0.71965E-08   0.13295E-08 0.20366E+00 
c  epsilon      0.10969E+02      11   0.35601E-08   0.10036E-01 0.16620E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.84937E-02 0.43479E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63332         0.61358       0.0052575       0.0015076
v  Velocity[Y]             -0.5738         0.54412       0.0030808      0.00087333
v  Velocity[Z]               1.565          5.4388          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4388          4.3406          4.3632
v  Pressure                -36.401          360.04          87.645          169.86
v  r11                   0.0010614        0.081904        0.013074        0.018286
v  r22                    0.001114         0.08264        0.013354        0.018646
v  r33                   0.0016402         0.17431        0.027251        0.037206
v  r12                   -0.010663        0.013582     -0.00023382     -0.00030931
v  r13                   -0.045533        0.052801      9.3213e-05       0.0010138
v  r23                   -0.046712        0.051209      3.0501e-05      0.00057459
v  epsilon                0.069173          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099176      0.00092503       0.0017427
v  CourantNb               0.44272             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2769         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71351         0.85284


 TIME FOR THE TIME STEP            10683:        0.79124E+02

===============================================================


 INSTANT    0.106840000E-01   TIME STEP NUMBER           10684
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.300821600E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.359990586E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.292584560E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.977823413E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110769750E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81401E-03   0.45349E-02 0.19924E+01 
c  Velocity[X]                                      0.13772E-03 
c  Velocity[Y]                                      0.12849E-03 
c  Velocity[Z]                                      0.42687E-02 
c  Pressure     0.36505E-04     133   0.92860E-02   0.25748E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50864E-08   0.17285E-08 0.10208E+00 
c  r22          0.10852E-01      13   0.56681E-08   0.18725E-08 0.10237E+00 
c  r33          0.21860E-01      15   0.57259E-08   0.13140E-07 0.13015E+00 
c  r12          0.93865E-03      18   0.70938E-08   0.30469E-09 0.61284E+00 
c  r13          0.46676E-02      19   0.63586E-08   0.15416E-08 0.20078E+00 
c  r23          0.39977E-02      19   0.64639E-08   0.13525E-08 0.20512E+00 
c  epsilon      0.10969E+02      11   0.33552E-08   0.10434E-01 0.17253E+00 
c  TempC        0.25716E+06      16   0.15178E-04   0.84208E-02 0.43316E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63318         0.61358       0.0052574       0.0015076
v  Velocity[Y]            -0.57382         0.54414       0.0030807      0.00087329
v  Velocity[Z]              1.5653          5.4388          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4388          4.3406          4.3632
v  Pressure                -36.472             360          87.625          169.83
v  r11                   0.0010614        0.081896        0.013074        0.018286
v  r22                    0.001114         0.08264        0.013354        0.018646
v  r33                   0.0016402         0.17429        0.027251        0.037206
v  r12                   -0.010662        0.013584     -0.00023382     -0.00030931
v  r13                   -0.045536        0.052802      9.3213e-05       0.0010138
v  r23                   -0.046713        0.051199      3.0502e-05      0.00057459
v  epsilon                0.069174          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099177      0.00092503       0.0017427
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017851           5.277         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71351         0.85284


 TIME FOR THE TIME STEP            10684:        0.80009E+02

===============================================================


 INSTANT    0.106850000E-01   TIME STEP NUMBER           10685
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.281417062E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.158538930E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.352110228E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.757487240E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.832255745E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81248E-03   0.45133E-02 0.19886E+01 
c  Velocity[X]                                      0.13831E-03 
c  Velocity[Y]                                      0.12768E-03 
c  Velocity[Z]                                      0.42473E-02 
c  Pressure     0.36376E-04     133   0.92585E-02   0.25658E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52923E-08   0.16473E-08 0.10025E+00 
c  r22          0.10852E-01      13   0.54165E-08   0.18067E-08 0.10114E+00 
c  r33          0.21860E-01      15   0.66667E-08   0.12380E-07 0.12700E+00 
c  r12          0.93865E-03      18   0.62749E-08   0.29931E-09 0.61066E+00 
c  r13          0.46676E-02      20   0.60721E-08   0.14889E-08 0.19868E+00 
c  r23          0.39977E-02      19   0.68443E-08   0.12726E-08 0.19911E+00 
c  epsilon      0.10969E+02      11   0.34929E-08   0.95488E-02 0.16346E+00 
c  TempC        0.25716E+06      16   0.15142E-04   0.83793E-02 0.43178E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63326         0.61356       0.0052575       0.0015076
v  Velocity[Y]            -0.57375         0.54421       0.0030807      0.00087328
v  Velocity[Z]               1.565          5.4388          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4388          4.3406          4.3632
v  Pressure                -36.419          360.03          87.643          169.86
v  r11                   0.0010614        0.081893        0.013074        0.018286
v  r22                    0.001114        0.082641        0.013354        0.018646
v  r33                   0.0016403         0.17427        0.027251        0.037206
v  r12                    -0.01066        0.013583     -0.00023382     -0.00030931
v  r13                   -0.045535        0.052803      9.3214e-05       0.0010138
v  r23                   -0.046714        0.051188      3.0503e-05      0.00057459
v  epsilon                0.069174          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099178      0.00092504       0.0017427
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2771         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71351         0.85283


 TIME FOR THE TIME STEP            10685:        0.78952E+02

===============================================================


 INSTANT    0.106860000E-01   TIME STEP NUMBER           10686
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.978717347E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160827787E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319036575E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136824563E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.486453670E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      44   0.81312E-03   0.45391E-02 0.19948E+01 
c  Velocity[X]                                      0.13830E-03 
c  Velocity[Y]                                      0.12943E-03 
c  Velocity[Z]                                      0.42714E-02 
c  Pressure     0.36479E-04     132   0.92906E-02   0.25731E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55132E-08   0.16610E-08 0.10039E+00 
c  r22          0.10852E-01      13   0.55786E-08   0.18195E-08 0.10130E+00 
c  r33          0.21860E-01      15   0.68254E-08   0.12589E-07 0.12783E+00 
c  r12          0.93865E-03      18   0.63567E-08   0.30598E-09 0.61378E+00 
c  r13          0.46676E-02      20   0.68587E-08   0.14928E-08 0.19942E+00 
c  r23          0.39977E-02      19   0.70825E-08   0.13022E-08 0.20114E+00 
c  epsilon      0.10969E+02      11   0.34452E-08   0.99370E-02 0.16631E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84175E-02 0.43287E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63336         0.61358       0.0052576       0.0015076
v  Velocity[Y]            -0.57371         0.54437       0.0030807      0.00087327
v  Velocity[Z]               1.565          5.4388          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4388          4.3406          4.3632
v  Pressure                -36.459             360          87.632          169.83
v  r11                   0.0010614        0.081891        0.013074        0.018286
v  r22                    0.001114        0.082643        0.013354        0.018646
v  r33                   0.0016403         0.17427        0.027251        0.037206
v  r12                    -0.01066        0.013584     -0.00023382     -0.00030931
v  r13                   -0.045533        0.052804      9.3215e-05       0.0010138
v  r23                   -0.046714        0.051215      3.0503e-05      0.00057459
v  epsilon                0.069175          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.994e-05       0.0099177      0.00092504       0.0017427
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2782         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71351         0.85284


 TIME FOR THE TIME STEP            10686:        0.80298E+02

===============================================================


 INSTANT    0.106870000E-01   TIME STEP NUMBER           10687
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.449448532E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.280234378E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.140207661E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.163030817E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.144149579E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81333E-03   0.45303E-02 0.19916E+01 
c  Velocity[X]                                      0.13809E-03 
c  Velocity[Y]                                      0.12792E-03 
c  Velocity[Z]                                      0.42643E-02 
c  Pressure     0.36284E-04     131   0.92409E-02   0.25593E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54145E-08   0.16520E-08 0.10005E+00 
c  r22          0.10852E-01      13   0.58703E-08   0.18329E-08 0.10146E+00 
c  r33          0.21860E-01      15   0.59475E-08   0.12558E-07 0.12749E+00 
c  r12          0.93865E-03      18   0.67270E-08   0.30819E-09 0.61414E+00 
c  r13          0.46676E-02      20   0.64178E-08   0.15129E-08 0.20047E+00 
c  r23          0.39977E-02      19   0.70628E-08   0.12859E-08 0.19926E+00 
c  epsilon      0.10969E+02      11   0.34900E-08   0.99893E-02 0.16624E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.83815E-02 0.43165E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63327         0.61358       0.0052575       0.0015076
v  Velocity[Y]             -0.5739         0.54419       0.0030807      0.00087328
v  Velocity[Z]              1.5652          5.4388          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4388          4.3406          4.3632
v  Pressure                -36.444          359.99          87.613          169.82
v  r11                   0.0010614        0.081889        0.013074        0.018286
v  r22                    0.001114        0.082643        0.013354        0.018646
v  r33                   0.0016403         0.17431        0.027251        0.037206
v  r12                   -0.010658        0.013582     -0.00023382     -0.00030931
v  r13                   -0.045536        0.052802      9.3215e-05       0.0010138
v  r23                   -0.046714        0.051204      3.0504e-05      0.00057459
v  epsilon                0.069176          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099175      0.00092504       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71351         0.85284


 TIME FOR THE TIME STEP            10687:        0.76300E+02

===============================================================


 INSTANT    0.106880000E-01   TIME STEP NUMBER           10688
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.501893018E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.241707714E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.218120776E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.271599590E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.775200712E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69779E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81162E-03   0.45021E-02 0.19864E+01 
c  Velocity[X]                                      0.13768E-03 
c  Velocity[Y]                                      0.12797E-03 
c  Velocity[Z]                                      0.42364E-02 
c  Pressure     0.36375E-04     132   0.92623E-02   0.25658E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54646E-08   0.16175E-08 0.99022E-01 
c  r22          0.10852E-01      13   0.59910E-08   0.18206E-08 0.10144E+00 
c  r33          0.21860E-01      15   0.64011E-08   0.12444E-07 0.12709E+00 
c  r12          0.93865E-03      18   0.69698E-08   0.30211E-09 0.61197E+00 
c  r13          0.46676E-02      20   0.60341E-08   0.15121E-08 0.20061E+00 
c  r23          0.39977E-02      19   0.71370E-08   0.12838E-08 0.19876E+00 
c  epsilon      0.10969E+02      11   0.33894E-08   0.99088E-02 0.16643E+00 
c  TempC        0.25716E+06      16   0.15180E-04   0.84387E-02 0.43325E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63335         0.61353       0.0052574       0.0015076
v  Velocity[Y]            -0.57371         0.54428       0.0030806      0.00087324
v  Velocity[Z]              1.5651          5.4388          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4388          4.3406          4.3632
v  Pressure                 -36.41          359.98          87.624          169.82
v  r11                   0.0010614        0.081893        0.013074        0.018286
v  r22                    0.001114        0.082638        0.013354        0.018646
v  r33                   0.0016403         0.17429        0.027251        0.037206
v  r12                   -0.010658        0.013582     -0.00023382     -0.00030931
v  r13                   -0.045534        0.052805      9.3215e-05       0.0010138
v  r23                   -0.046714         0.05119      3.0505e-05      0.00057459
v  epsilon                0.069176          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9943e-05       0.0099176      0.00092504       0.0017427
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2788         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71351         0.85284


 TIME FOR THE TIME STEP            10688:        0.76810E+02

===============================================================


 INSTANT    0.106890000E-01   TIME STEP NUMBER           10689
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.789724977E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.291377311E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.333691269E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.189617582E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.415064444E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81317E-03   0.44989E-02 0.19873E+01 
c  Velocity[X]                                      0.13799E-03 
c  Velocity[Y]                                      0.12778E-03 
c  Velocity[Z]                                      0.42331E-02 
c  Pressure     0.36411E-04     131   0.92671E-02   0.25683E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54870E-08   0.16612E-08 0.10038E+00 
c  r22          0.10852E-01      13   0.63096E-08   0.18270E-08 0.10129E+00 
c  r33          0.21860E-01      15   0.63029E-08   0.12720E-07 0.12819E+00 
c  r12          0.93865E-03      18   0.70769E-08   0.30583E-09 0.61332E+00 
c  r13          0.46676E-02      20   0.60474E-08   0.15088E-08 0.20003E+00 
c  r23          0.39977E-02      20   0.60822E-08   0.13210E-08 0.20193E+00 
c  epsilon      0.10969E+02      11   0.33563E-08   0.10297E-01 0.17124E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.84708E-02 0.43448E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61359       0.0052576       0.0015076
v  Velocity[Y]            -0.57371          0.5444       0.0030807      0.00087328
v  Velocity[Z]              1.5651          5.4388          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4388          4.3406          4.3632
v  Pressure                -36.389          360.03          87.644          169.85
v  r11                   0.0010614        0.081896        0.013074        0.018286
v  r22                    0.001114         0.08264        0.013354        0.018646
v  r33                   0.0016403         0.17426        0.027252        0.037206
v  r12                    -0.01066        0.013581     -0.00023382     -0.00030931
v  r13                   -0.045535        0.052806      9.3216e-05       0.0010138
v  r23                   -0.046715        0.051199      3.0505e-05      0.00057459
v  epsilon                0.069177          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9943e-05       0.0099176      0.00092504       0.0017427
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2789         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71351         0.85284


 TIME FOR THE TIME STEP            10689:        0.72887E+02

===============================================================


 INSTANT    0.106900000E-01   TIME STEP NUMBER           10690
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155896076E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.469647366E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.272942002E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188056597E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.116481211E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81295E-03   0.45053E-02 0.19878E+01 
c  Velocity[X]                                      0.13797E-03 
c  Velocity[Y]                                      0.12831E-03 
c  Velocity[Z]                                      0.42390E-02 
c  Pressure     0.36219E-04     132   0.92201E-02   0.25547E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57699E-08   0.16359E-08 0.99725E-01 
c  r22          0.10852E-01      13   0.57603E-08   0.18255E-08 0.10133E+00 
c  r33          0.21860E-01      15   0.64405E-08   0.12532E-07 0.12749E+00 
c  r12          0.93865E-03      18   0.69641E-08   0.29341E-09 0.60564E+00 
c  r13          0.46676E-02      20   0.58130E-08   0.15118E-08 0.20028E+00 
c  r23          0.39977E-02      20   0.61647E-08   0.12865E-08 0.19962E+00 
c  epsilon      0.10969E+02      11   0.33725E-08   0.99568E-02 0.16706E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.83625E-02 0.43130E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63324         0.61358       0.0052575       0.0015076
v  Velocity[Y]            -0.57361         0.54428       0.0030806      0.00087321
v  Velocity[Z]              1.5651          5.4388          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4388          4.3406          4.3632
v  Pressure                -36.446          359.98          87.628          169.82
v  r11                   0.0010614        0.081897        0.013074        0.018286
v  r22                    0.001114        0.082642        0.013354        0.018646
v  r33                   0.0016404         0.17428        0.027252        0.037206
v  r12                    -0.01066        0.013584     -0.00023382     -0.00030931
v  r13                   -0.045537        0.052806      9.3216e-05       0.0010138
v  r23                   -0.046715        0.051187      3.0505e-05      0.00057459
v  epsilon                0.069178          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9943e-05       0.0099176      0.00092504       0.0017427
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2793         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8793         0.71351         0.85284


 TIME FOR THE TIME STEP            10690:        0.73942E+02

===============================================================


 INSTANT    0.106910000E-01   TIME STEP NUMBER           10691
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.465637923E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.453449062E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.140408681E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.103665377E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.174460862E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81224E-03   0.45244E-02 0.19927E+01 
c  Velocity[X]                                      0.13797E-03 
c  Velocity[Y]                                      0.12866E-03 
c  Velocity[Z]                                      0.42577E-02 
c  Pressure     0.36235E-04     133   0.92292E-02   0.25559E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61005E-08   0.16270E-08 0.99523E-01 
c  r22          0.10852E-01      13   0.55854E-08   0.18081E-08 0.10142E+00 
c  r33          0.21860E-01      15   0.61929E-08   0.12397E-07 0.12707E+00 
c  r12          0.93865E-03      18   0.66704E-08   0.30334E-09 0.61218E+00 
c  r13          0.46676E-02      19   0.73366E-08   0.15015E-08 0.20018E+00 
c  r23          0.39977E-02      19   0.74114E-08   0.12875E-08 0.19935E+00 
c  epsilon      0.10969E+02      11   0.35601E-08   0.95509E-02 0.16271E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.83738E-02 0.43160E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63325         0.61356       0.0052575       0.0015076
v  Velocity[Y]            -0.57365         0.54422       0.0030807      0.00087325
v  Velocity[Z]              1.5651          5.4388          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4388          4.3406          4.3632
v  Pressure                -36.376          360.02          87.634          169.84
v  r11                   0.0010614          0.0819        0.013074        0.018286
v  r22                    0.001114        0.082643        0.013354        0.018646
v  r33                   0.0016404         0.17431        0.027252        0.037206
v  r12                   -0.010658        0.013586     -0.00023382     -0.00030931
v  r13                   -0.045534        0.052803      9.3217e-05       0.0010138
v  r23                   -0.046715         0.05118      3.0506e-05      0.00057459
v  epsilon                0.069179           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9943e-05       0.0099176      0.00092504       0.0017427
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2783         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71351         0.85284


 TIME FOR THE TIME STEP            10691:        0.73716E+02

===============================================================


 INSTANT    0.106920000E-01   TIME STEP NUMBER           10692
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.144727236E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.204472328E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171080814E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.369591243E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.392175483E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81335E-03   0.45100E-02 0.19883E+01 
c  Velocity[X]                                      0.13841E-03 
c  Velocity[Y]                                      0.12879E-03 
c  Velocity[Z]                                      0.42428E-02 
c  Pressure     0.36658E-04     132   0.93291E-02   0.25858E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61774E-08   0.16308E-08 0.99645E-01 
c  r22          0.10852E-01      13   0.54343E-08   0.18350E-08 0.10168E+00 
c  r33          0.21860E-01      15   0.56622E-08   0.12505E-07 0.12726E+00 
c  r12          0.93865E-03      18   0.61920E-08   0.29786E-09 0.60978E+00 
c  r13          0.46676E-02      19   0.73748E-08   0.15052E-08 0.20007E+00 
c  r23          0.39977E-02      19   0.64910E-08   0.12763E-08 0.19894E+00 
c  epsilon      0.10969E+02      11   0.34208E-08   0.99069E-02 0.16570E+00 
c  TempC        0.25716E+06      16   0.15167E-04   0.84554E-02 0.43387E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63331         0.61357       0.0052575       0.0015076
v  Velocity[Y]            -0.57359          0.5443       0.0030807      0.00087323
v  Velocity[Z]              1.5653          5.4388          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4388          4.3406          4.3632
v  Pressure                 -36.45          360.01          87.637          169.83
v  r11                   0.0010614        0.081896        0.013074        0.018286
v  r22                    0.001114        0.082644        0.013354        0.018646
v  r33                   0.0016404         0.17428        0.027252        0.037206
v  r12                   -0.010655        0.013585     -0.00023382     -0.00030931
v  r13                   -0.045533        0.052803      9.3217e-05       0.0010138
v  r23                   -0.046714        0.051202      3.0507e-05      0.00057459
v  epsilon                0.069179           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099176      0.00092504       0.0017427
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2784         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71351         0.85284


 TIME FOR THE TIME STEP            10692:        0.74265E+02

===============================================================


 INSTANT    0.106930000E-01   TIME STEP NUMBER           10693
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.286584395E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162542758E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.175420562E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.430168061E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119953811E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81276E-03   0.45065E-02 0.19877E+01 
c  Velocity[X]                                      0.13732E-03 
c  Velocity[Y]                                      0.12797E-03 
c  Velocity[Z]                                      0.42412E-02 
c  Pressure     0.36189E-04     131   0.92153E-02   0.25527E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.63632E-08   0.16530E-08 0.10021E+00 
c  r22          0.10852E-01      13   0.56601E-08   0.18441E-08 0.10227E+00 
c  r33          0.21860E-01      15   0.51936E-08   0.12658E-07 0.12848E+00 
c  r12          0.93865E-03      18   0.60691E-08   0.30457E-09 0.61651E+00 
c  r13          0.46676E-02      20   0.71331E-08   0.15040E-08 0.20114E+00 
c  r23          0.39977E-02      19   0.61940E-08   0.12934E-08 0.20124E+00 
c  epsilon      0.10969E+02      11   0.34974E-08   0.97866E-02 0.16464E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.83923E-02 0.43227E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61357       0.0052575       0.0015076
v  Velocity[Y]            -0.57371         0.54441       0.0030807      0.00087328
v  Velocity[Z]              1.5652          5.4388          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4388          4.3406          4.3632
v  Pressure                -36.437          360.04          87.633          169.85
v  r11                   0.0010614        0.081894        0.013074        0.018286
v  r22                   0.0011141        0.082645        0.013354        0.018646
v  r33                   0.0016404         0.17427        0.027252        0.037206
v  r12                   -0.010652         0.01358     -0.00023382     -0.00030931
v  r13                   -0.045537        0.052804      9.3217e-05       0.0010138
v  r23                   -0.046713        0.051188      3.0507e-05      0.00057459
v  epsilon                 0.06918          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9943e-05       0.0099176      0.00092504       0.0017427
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2778         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71351         0.85284


 TIME FOR THE TIME STEP            10693:        0.72545E+02

===============================================================


 INSTANT    0.106940000E-01   TIME STEP NUMBER           10694
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149815355E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.349391694E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226374848E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.457203283E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.236258994E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81242E-03   0.45544E-02 0.19974E+01 
c  Velocity[X]                                      0.13839E-03 
c  Velocity[Y]                                      0.12829E-03 
c  Velocity[Z]                                      0.42877E-02 
c  Pressure     0.36346E-04     133   0.92494E-02   0.25637E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.66625E-08   0.16332E-08 0.99269E-01 
c  r22          0.10852E-01      13   0.56813E-08   0.18067E-08 0.10102E+00 
c  r33          0.21860E-01      15   0.52735E-08   0.12457E-07 0.12697E+00 
c  r12          0.93865E-03      18   0.57525E-08   0.29144E-09 0.60457E+00 
c  r13          0.46676E-02      20   0.60409E-08   0.14810E-08 0.19949E+00 
c  r23          0.39977E-02      19   0.61733E-08   0.12852E-08 0.19920E+00 
c  epsilon      0.10969E+02      11   0.33547E-08   0.98838E-02 0.16528E+00 
c  TempC        0.25716E+06      16   0.15182E-04   0.84559E-02 0.43366E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63321         0.61355       0.0052575       0.0015076
v  Velocity[Y]             -0.5736         0.54426       0.0030806      0.00087322
v  Velocity[Z]              1.5653          5.4388          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4388          4.3406          4.3632
v  Pressure                -36.418          359.93          87.595          169.78
v  r11                   0.0010614        0.081886        0.013074        0.018286
v  r22                   0.0011141        0.082646        0.013354        0.018646
v  r33                   0.0016404         0.17428        0.027252        0.037206
v  r12                   -0.010655        0.013576     -0.00023382     -0.00030931
v  r13                   -0.045534        0.052806      9.3218e-05       0.0010138
v  r23                   -0.046713        0.051188      3.0507e-05      0.00057459
v  epsilon                0.069181          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9944e-05       0.0099177      0.00092504       0.0017427
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2773         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71351         0.85283


 TIME FOR THE TIME STEP            10694:        0.73864E+02

===============================================================


 INSTANT    0.106950000E-01   TIME STEP NUMBER           10695
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138714306E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168701912E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160384064E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.109882423E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.599836011E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81262E-03   0.44973E-02 0.19866E+01 
c  Velocity[X]                                      0.13833E-03 
c  Velocity[Y]                                      0.12792E-03 
c  Velocity[Z]                                      0.42311E-02 
c  Pressure     0.36097E-04     133   0.91909E-02   0.25462E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.62868E-08   0.16528E-08 0.10020E+00 
c  r22          0.10852E-01      13   0.53929E-08   0.18250E-08 0.10151E+00 
c  r33          0.21860E-01      15   0.65060E-08   0.12566E-07 0.12793E+00 
c  r12          0.93866E-03      18   0.64500E-08   0.29782E-09 0.60898E+00 
c  r13          0.46676E-02      19   0.74286E-08   0.14857E-08 0.19988E+00 
c  r23          0.39977E-02      19   0.67651E-08   0.12938E-08 0.20107E+00 
c  epsilon      0.10969E+02      11   0.32836E-08   0.99770E-02 0.16910E+00 
c  TempC        0.25716E+06      16   0.15099E-04   0.84415E-02 0.43367E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63322          0.6136       0.0052575       0.0015076
v  Velocity[Y]            -0.57368         0.54421       0.0030807      0.00087325
v  Velocity[Z]               1.565          5.4388          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4388          4.3406          4.3632
v  Pressure                -36.407          360.02          87.631          169.84
v  r11                   0.0010614        0.081885        0.013074        0.018286
v  r22                   0.0011141        0.082647        0.013354        0.018646
v  r33                   0.0016405          0.1743        0.027252        0.037206
v  r12                   -0.010662        0.013579     -0.00023382     -0.00030931
v  r13                   -0.045533        0.052805      9.3218e-05       0.0010138
v  r23                   -0.046713        0.051207      3.0507e-05      0.00057459
v  epsilon                0.069182          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9945e-05       0.0099177      0.00092504       0.0017427
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2773         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71351         0.85284


 TIME FOR THE TIME STEP            10695:        0.73443E+02

===============================================================


 INSTANT    0.106960000E-01   TIME STEP NUMBER           10696
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.262005824E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.966550036E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.344521066E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.126788196E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.224702137E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81346E-03   0.44848E-02 0.19838E+01 
c  Velocity[X]                                      0.13767E-03 
c  Velocity[Y]                                      0.12784E-03 
c  Velocity[Z]                                      0.42193E-02 
c  Pressure     0.36387E-04     133   0.92626E-02   0.25665E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58694E-08   0.16454E-08 0.99481E-01 
c  r22          0.10852E-01      13   0.50284E-08   0.18198E-08 0.10132E+00 
c  r33          0.21860E-01      15   0.62940E-08   0.12542E-07 0.12724E+00 
c  r12          0.93866E-03      18   0.63527E-08   0.30092E-09 0.60762E+00 
c  r13          0.46676E-02      19   0.61170E-08   0.14932E-08 0.19988E+00 
c  r23          0.39977E-02      19   0.62655E-08   0.12988E-08 0.20001E+00 
c  epsilon      0.10969E+02      11   0.34071E-08   0.99306E-02 0.16543E+00 
c  TempC        0.25716E+06      16   0.15184E-04   0.83447E-02 0.43133E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61358       0.0052575       0.0015076
v  Velocity[Y]            -0.57371          0.5443       0.0030806      0.00087325
v  Velocity[Z]              1.5652          5.4388          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4388          4.3406          4.3632
v  Pressure                -36.428          360.05          87.672          169.88
v  r11                   0.0010615        0.081883        0.013074        0.018286
v  r22                   0.0011141        0.082645        0.013354        0.018646
v  r33                   0.0016405         0.17428        0.027252        0.037206
v  r12                   -0.010664        0.013581     -0.00023382     -0.00030931
v  r13                   -0.045536        0.052804      9.3219e-05       0.0010138
v  r23                   -0.046713        0.051199      3.0508e-05      0.00057459
v  epsilon                0.069182           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9943e-05       0.0099178      0.00092504       0.0017427
v  CourantNb                0.4422             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2776         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71351         0.85284


 TIME FOR THE TIME STEP            10696:        0.72474E+02

===============================================================


 INSTANT    0.106970000E-01   TIME STEP NUMBER           10697
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.271017786E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.315210032E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.372891936E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.433601523E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.287130110E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      40   0.81126E-03   0.45250E-02 0.19920E+01 
c  Velocity[X]                                      0.13787E-03 
c  Velocity[Y]                                      0.12812E-03 
c  Velocity[Z]                                      0.42590E-02 
c  Pressure     0.36474E-04     131   0.92895E-02   0.25727E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57947E-08   0.16324E-08 0.99130E-01 
c  r22          0.10852E-01      13   0.52605E-08   0.18436E-08 0.10142E+00 
c  r33          0.21860E-01      15   0.63644E-08   0.12625E-07 0.12724E+00 
c  r12          0.93866E-03      18   0.59866E-08   0.29632E-09 0.60636E+00 
c  r13          0.46676E-02      19   0.63800E-08   0.15156E-08 0.19994E+00 
c  r23          0.39977E-02      19   0.63442E-08   0.12896E-08 0.19922E+00 
c  epsilon      0.10969E+02      11   0.35094E-08   0.10122E-01 0.16629E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.83978E-02 0.43202E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63321         0.61357       0.0052575       0.0015076
v  Velocity[Y]            -0.57377         0.54442       0.0030807      0.00087326
v  Velocity[Z]              1.5652          5.4389          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4389          4.3406          4.3632
v  Pressure                -36.389          360.05           87.67          169.88
v  r11                   0.0010615        0.081888        0.013074        0.018286
v  r22                   0.0011141        0.082645        0.013354        0.018646
v  r33                   0.0016405         0.17426        0.027252        0.037206
v  r12                   -0.010662         0.01358     -0.00023382     -0.00030931
v  r13                   -0.045536        0.052805      9.3219e-05       0.0010138
v  r23                   -0.046713        0.051188      3.0508e-05      0.00057459
v  epsilon                0.069183          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9944e-05       0.0099178      0.00092505       0.0017427
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2777         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71351         0.85284


 TIME FOR THE TIME STEP            10697:        0.74556E+02

===============================================================


 INSTANT    0.106980000E-01   TIME STEP NUMBER           10698
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.101194494E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.160257602E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171433750E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.172139285E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.150855023E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      43   0.81311E-03   0.45333E-02 0.19957E+01 
c  Velocity[X]                                      0.13885E-03 
c  Velocity[Y]                                      0.12952E-03 
c  Velocity[Z]                                      0.42649E-02 
c  Pressure     0.36538E-04     134   0.93026E-02   0.25774E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.66310E-08   0.16291E-08 0.99690E-01 
c  r22          0.10852E-01      13   0.53454E-08   0.18280E-08 0.10171E+00 
c  r33          0.21860E-01      15   0.58141E-08   0.12429E-07 0.12751E+00 
c  r12          0.93866E-03      18   0.61137E-08   0.29688E-09 0.60799E+00 
c  r13          0.46676E-02      19   0.61721E-08   0.14933E-08 0.20047E+00 
c  r23          0.39977E-02      19   0.57876E-08   0.12767E-08 0.19971E+00 
c  epsilon      0.10969E+02      11   0.35774E-08   0.96420E-02 0.16270E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84356E-02 0.43285E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6333         0.61359       0.0052575       0.0015076
v  Velocity[Y]            -0.57365         0.54424       0.0030807      0.00087326
v  Velocity[Z]              1.5652          5.4389          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4389          4.3406          4.3632
v  Pressure                -36.453          360.02          87.642          169.84
v  r11                   0.0010615        0.081891        0.013074        0.018286
v  r22                   0.0011141        0.082642        0.013354        0.018646
v  r33                   0.0016405         0.17426        0.027252        0.037206
v  r12                    -0.01066        0.013577     -0.00023382     -0.00030931
v  r13                   -0.045534        0.052807       9.322e-05       0.0010138
v  r23                   -0.046713        0.051206      3.0509e-05       0.0005746
v  epsilon                0.069184          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099179      0.00092505       0.0017427
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2782         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71351         0.85284


 TIME FOR THE TIME STEP            10698:        0.74757E+02

===============================================================


 INSTANT    0.106990000E-01   TIME STEP NUMBER           10699
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.261225576E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.175462443E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.148004173E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935017E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.375405256E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150864454E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      41   0.81279E-03   0.45125E-02 0.19891E+01 
c  Velocity[X]                                      0.13843E-03 
c  Velocity[Y]                                      0.12848E-03 
c  Velocity[Z]                                      0.42456E-02 
c  Pressure     0.36451E-04     131   0.92877E-02   0.25711E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.63398E-08   0.16318E-08 0.99357E-01 
c  r22          0.10852E-01      13   0.52850E-08   0.18222E-08 0.10107E+00 
c  r33          0.21860E-01      16   0.66153E-08   0.12422E-07 0.12657E+00 
c  r12          0.93866E-03      18   0.60596E-08   0.29810E-09 0.60614E+00 
c  r13          0.46676E-02      20   0.60466E-08   0.14927E-08 0.19915E+00 
c  r23          0.39977E-02      19   0.67920E-08   0.12761E-08 0.19816E+00 
c  epsilon      0.10969E+02      11   0.36375E-08   0.96731E-02 0.16298E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.84437E-02 0.43355E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63331         0.61361       0.0052575       0.0015076
v  Velocity[Y]            -0.57379         0.54432       0.0030807      0.00087326
v  Velocity[Z]              1.5651          5.4389          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4389          4.3406          4.3632
v  Pressure                -36.432          359.98          87.598           169.8
v  r11                   0.0010615        0.081888        0.013074        0.018286
v  r22                   0.0011141        0.082643        0.013354        0.018646
v  r33                   0.0016406          0.1743        0.027252        0.037206
v  r12                   -0.010658        0.013582     -0.00023382     -0.00030931
v  r13                   -0.045537        0.052806       9.322e-05       0.0010138
v  r23                   -0.046713          0.0512      3.0509e-05       0.0005746
v  epsilon                0.069184          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9943e-05        0.009918      0.00092505       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2788         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71352         0.85284


 TIME FOR THE TIME STEP            10699:        0.73479E+02

===============================================================


 INSTANT    0.107000000E-01   TIME STEP NUMBER           10700
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.314574239E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.143480251E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934909E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178843182E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.366315901E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.195250851E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36450E+01      42   0.81263E-03   0.44972E-02 0.19867E+01 
c  Velocity[X]                                      0.13765E-03 
c  Velocity[Y]                                      0.12767E-03 
c  Velocity[Z]                                      0.42319E-02 
c  Pressure     0.36267E-04     133   0.92392E-02   0.25581E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60684E-08   0.16318E-08 0.99607E-01 
c  r22          0.10852E-01      13   0.57301E-08   0.18319E-08 0.10166E+00 
c  r33          0.21860E-01      16   0.58130E-08   0.12535E-07 0.12747E+00 
c  r12          0.93866E-03      18   0.68276E-08   0.29563E-09 0.60487E+00 
c  r13          0.46676E-02      20   0.74752E-08   0.15119E-08 0.20075E+00 
c  r23          0.39977E-02      19   0.65187E-08   0.13000E-08 0.19967E+00 
c  epsilon      0.10969E+02      11   0.34408E-08   0.98949E-02 0.16517E+00 
c  TempC        0.25716E+06      16   0.15167E-04   0.84195E-02 0.43310E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6332          0.6136       0.0052575       0.0015076
v  Velocity[Y]            -0.57365         0.54452       0.0030806      0.00087321
v  Velocity[Z]              1.5651          5.4389          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4389          4.3406          4.3632
v  Pressure                -36.432          359.97          87.628          169.81
v  r11                   0.0010615        0.081885        0.013074        0.018286
v  r22                   0.0011141        0.082643        0.013354        0.018646
v  r33                   0.0016406         0.17428        0.027252        0.037206
v  r12                   -0.010656        0.013585     -0.00023382     -0.00030931
v  r13                   -0.045534        0.052805      9.3221e-05       0.0010138
v  r23                   -0.046713          0.0512       3.051e-05       0.0005746
v  epsilon                0.069185          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9939e-05        0.009918      0.00092505       0.0017427
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2772         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71351         0.85283


 TIME FOR THE TIME STEP            10700:        0.73112E+02

===============================================================


 INSTANT    0.107010000E-01   TIME STEP NUMBER           10701
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.946413873E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141793110E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.693130755E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.931933136E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.354423128E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81271E-03   0.45401E-02 0.19938E+01 
c  Velocity[X]                                      0.13820E-03 
c  Velocity[Y]                                      0.12832E-03 
c  Velocity[Z]                                      0.42735E-02 
c  Pressure     0.36399E-04     133   0.92692E-02   0.25674E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59909E-08   0.16780E-08 0.10027E+00 
c  r22          0.10852E-01      13   0.52093E-08   0.18320E-08 0.10117E+00 
c  r33          0.21860E-01      15   0.55630E-08   0.12761E-07 0.12785E+00 
c  r12          0.93866E-03      18   0.62947E-08   0.30016E-09 0.60769E+00 
c  r13          0.46676E-02      19   0.59041E-08   0.15031E-08 0.19989E+00 
c  r23          0.39977E-02      19   0.57369E-08   0.13240E-08 0.20169E+00 
c  epsilon      0.10969E+02      11   0.32503E-08   0.10329E-01 0.17243E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.84159E-02 0.43313E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63324         0.61361       0.0052576       0.0015076
v  Velocity[Y]             -0.5738         0.54421       0.0030807      0.00087327
v  Velocity[Z]              1.5651          5.4389          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4389          4.3406          4.3632
v  Pressure                -36.361          360.02          87.652          169.85
v  r11                   0.0010615        0.081883        0.013074        0.018286
v  r22                   0.0011141        0.082646        0.013354        0.018646
v  r33                   0.0016406         0.17425        0.027252        0.037206
v  r12                   -0.010661        0.013582     -0.00023382     -0.00030931
v  r13                   -0.045535        0.052806      9.3222e-05       0.0010138
v  r23                   -0.046714        0.051197      3.0511e-05       0.0005746
v  epsilon                0.069186          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9939e-05       0.0099181      0.00092505       0.0017427
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2774         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71351         0.85284


 TIME FOR THE TIME STEP            10701:        0.74067E+02

===============================================================


 INSTANT    0.107020000E-01   TIME STEP NUMBER           10702
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.216769232E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.361204870E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.204355797E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.168631645E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182535033E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81263E-03   0.45260E-02 0.19926E+01 
c  Velocity[X]                                      0.13805E-03 
c  Velocity[Y]                                      0.12754E-03 
c  Velocity[Z]                                      0.42604E-02 
c  Pressure     0.36533E-04     133   0.93028E-02   0.25768E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60552E-08   0.16347E-08 0.99563E-01 
c  r22          0.10852E-01      13   0.49762E-08   0.18667E-08 0.10231E+00 
c  r33          0.21860E-01      15   0.62814E-08   0.12633E-07 0.12787E+00 
c  r12          0.93866E-03      18   0.62148E-08   0.30128E-09 0.60829E+00 
c  r13          0.46676E-02      19   0.61986E-08   0.15265E-08 0.20173E+00 
c  r23          0.39977E-02      19   0.55269E-08   0.12865E-08 0.19942E+00 
c  epsilon      0.10969E+02      11   0.34018E-08   0.99269E-02 0.16665E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.83857E-02 0.43187E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63329         0.61361       0.0052576       0.0015076
v  Velocity[Y]            -0.57373         0.54423       0.0030807      0.00087322
v  Velocity[Z]              1.5654          5.4389          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4389          4.3406          4.3632
v  Pressure                 -36.46          360.04          87.667          169.87
v  r11                   0.0010615        0.081897        0.013074        0.018286
v  r22                   0.0011141        0.082647        0.013354        0.018646
v  r33                   0.0016406         0.17426        0.027252        0.037206
v  r12                   -0.010661        0.013579     -0.00023382     -0.00030931
v  r13                   -0.045536        0.052806      9.3222e-05       0.0010138
v  r23                   -0.046714        0.051223      3.0511e-05       0.0005746
v  epsilon                0.069186          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9939e-05       0.0099181      0.00092505       0.0017427
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2775         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71351         0.85284


 TIME FOR THE TIME STEP            10702:        0.71477E+02

===============================================================


 INSTANT    0.107030000E-01   TIME STEP NUMBER           10703
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209398476E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.121825357E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285681203E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.305667009E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.273144525E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81234E-03   0.45128E-02 0.19913E+01 
c  Velocity[X]                                      0.13840E-03 
c  Velocity[Y]                                      0.12844E-03 
c  Velocity[Z]                                      0.42459E-02 
c  Pressure     0.36314E-04     133   0.92448E-02   0.25615E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60813E-08   0.16540E-08 0.99402E-01 
c  r22          0.10852E-01      13   0.50374E-08   0.18722E-08 0.10220E+00 
c  r33          0.21860E-01      15   0.62078E-08   0.12792E-07 0.12798E+00 
c  r12          0.93866E-03      18   0.60644E-08   0.30342E-09 0.60987E+00 
c  r13          0.46676E-02      19   0.60856E-08   0.15370E-08 0.20168E+00 
c  r23          0.39977E-02      19   0.57562E-08   0.13186E-08 0.20082E+00 
c  epsilon      0.10969E+02      11   0.34656E-08   0.10020E-01 0.16585E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.84307E-02 0.43357E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63323          0.6136       0.0052576       0.0015076
v  Velocity[Y]            -0.57373         0.54436       0.0030807      0.00087322
v  Velocity[Z]              1.5651          5.4389          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4389          4.3406          4.3632
v  Pressure                -36.405             360          87.636          169.83
v  r11                   0.0010615        0.081905        0.013074        0.018286
v  r22                   0.0011141        0.082646        0.013354        0.018646
v  r33                   0.0016406          0.1743        0.027252        0.037206
v  r12                   -0.010659        0.013579     -0.00023382     -0.00030931
v  r13                   -0.045534        0.052804      9.3222e-05       0.0010138
v  r23                   -0.046714        0.051216      3.0512e-05       0.0005746
v  epsilon                0.069187          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099181      0.00092505       0.0017427
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2776         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71351         0.85283


 TIME FOR THE TIME STEP            10703:        0.72274E+02

===============================================================


 INSTANT    0.107040000E-01   TIME STEP NUMBER           10704
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.403641886E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.130324041E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.203917837E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.495133791E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.355793881E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81246E-03   0.45145E-02 0.19883E+01 
c  Velocity[X]                                      0.13726E-03 
c  Velocity[Y]                                      0.12836E-03 
c  Velocity[Z]                                      0.42489E-02 
c  Pressure     0.36404E-04     131   0.92686E-02   0.25678E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58318E-08   0.16431E-08 0.99226E-01 
c  r22          0.10852E-01      13   0.51171E-08   0.18580E-08 0.10182E+00 
c  r33          0.21860E-01      15   0.57544E-08   0.12692E-07 0.12752E+00 
c  r12          0.93866E-03      18   0.59034E-08   0.30070E-09 0.61016E+00 
c  r13          0.46676E-02      19   0.55848E-08   0.15277E-08 0.20059E+00 
c  r23          0.39977E-02      19   0.59243E-08   0.12954E-08 0.19932E+00 
c  epsilon      0.10969E+02      11   0.35371E-08   0.10037E-01 0.16714E+00 
c  TempC        0.25716E+06      16   0.15185E-04   0.84269E-02 0.43309E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63325         0.61361       0.0052575       0.0015076
v  Velocity[Y]            -0.57371         0.54453       0.0030807      0.00087324
v  Velocity[Z]              1.5652          5.4389          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4389          4.3406          4.3632
v  Pressure                -36.412          360.02          87.638          169.85
v  r11                   0.0010615        0.081909        0.013074        0.018286
v  r22                   0.0011142        0.082645        0.013354        0.018646
v  r33                   0.0016407         0.17428        0.027252        0.037207
v  r12                   -0.010656        0.013575     -0.00023382     -0.00030931
v  r13                   -0.045533        0.052805      9.3223e-05       0.0010138
v  r23                   -0.046715        0.051197      3.0513e-05       0.0005746
v  epsilon                0.069188          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099181      0.00092505       0.0017427
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017851           5.278         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71351         0.85283


 TIME FOR THE TIME STEP            10704:        0.75791E+02

===============================================================


 INSTANT    0.107050000E-01   TIME STEP NUMBER           10705
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.257846488E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.222264868E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.154124447E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.735077959E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.124723762E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81348E-03   0.45060E-02 0.19860E+01 
c  Velocity[X]                                      0.13773E-03 
c  Velocity[Y]                                      0.12769E-03 
c  Velocity[Z]                                      0.42405E-02 
c  Pressure     0.36250E-04     133   0.92304E-02   0.25570E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56349E-08   0.16400E-08 0.98963E-01 
c  r22          0.10852E-01      13   0.51049E-08   0.18514E-08 0.10117E+00 
c  r33          0.21860E-01      15   0.60505E-08   0.12598E-07 0.12691E+00 
c  r12          0.93866E-03      18   0.62233E-08   0.29827E-09 0.60472E+00 
c  r13          0.46676E-02      19   0.62869E-08   0.14964E-08 0.19936E+00 
c  r23          0.39977E-02      19   0.63365E-08   0.12854E-08 0.19897E+00 
c  epsilon      0.10969E+02      11   0.34570E-08   0.98830E-02 0.16485E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.83507E-02 0.43082E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63328         0.61364       0.0052576       0.0015076
v  Velocity[Y]            -0.57372         0.54419       0.0030807      0.00087325
v  Velocity[Z]              1.5649          5.4389          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4389          4.3406          4.3632
v  Pressure                -36.398          360.04          87.643          169.87
v  r11                   0.0010615        0.081908        0.013074        0.018286
v  r22                   0.0011142        0.082641        0.013354        0.018646
v  r33                   0.0016407         0.17426        0.027252        0.037207
v  r12                   -0.010653        0.013579     -0.00023382     -0.00030931
v  r13                   -0.045536        0.052807      9.3223e-05       0.0010138
v  r23                   -0.046715        0.051222      3.0513e-05       0.0005746
v  epsilon                0.069189          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099181      0.00092505       0.0017427
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2779         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71351         0.85284


 TIME FOR THE TIME STEP            10705:        0.72954E+02

===============================================================


 INSTANT    0.107060000E-01   TIME STEP NUMBER           10706
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.207015024E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.271081502E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.255163251E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.553193010E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.170579488E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81243E-03   0.45275E-02 0.19941E+01 
c  Velocity[X]                                      0.13895E-03 
c  Velocity[Y]                                      0.12930E-03 
c  Velocity[Z]                                      0.42592E-02 
c  Pressure     0.36510E-04     133   0.92909E-02   0.25753E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59652E-08   0.16439E-08 0.99569E-01 
c  r22          0.10852E-01      13   0.52741E-08   0.18538E-08 0.10197E+00 
c  r33          0.21860E-01      15   0.64787E-08   0.12672E-07 0.12808E+00 
c  r12          0.93866E-03      18   0.60792E-08   0.29424E-09 0.60432E+00 
c  r13          0.46676E-02      19   0.63447E-08   0.14898E-08 0.20000E+00 
c  r23          0.39977E-02      19   0.52181E-08   0.13045E-08 0.20118E+00 
c  epsilon      0.10969E+02      11   0.33014E-08   0.98510E-02 0.16593E+00 
c  TempC        0.25716E+06      16   0.15180E-04   0.84130E-02 0.43266E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63327         0.61361       0.0052575       0.0015076
v  Velocity[Y]            -0.57369         0.54423       0.0030806      0.00087319
v  Velocity[Z]               1.565          5.4389          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4389          4.3406          4.3632
v  Pressure                 -36.43          360.01          87.664          169.85
v  r11                   0.0010615        0.081909        0.013074        0.018286
v  r22                   0.0011142        0.082642        0.013354        0.018646
v  r33                   0.0016407         0.17427        0.027252        0.037207
v  r12                   -0.010652        0.013582     -0.00023382     -0.00030931
v  r13                   -0.045533        0.052809      9.3224e-05       0.0010138
v  r23                   -0.046715        0.051215      3.0514e-05       0.0005746
v  epsilon                0.069189           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099177      0.00092505       0.0017427
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2781         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71351         0.85283


 TIME FOR THE TIME STEP            10706:        0.75087E+02

===============================================================


 INSTANT    0.107070000E-01   TIME STEP NUMBER           10707
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.395630941E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195544123E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116912427E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242549684E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191224288E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81188E-03   0.45174E-02 0.19923E+01 
c  Velocity[X]                                      0.13818E-03 
c  Velocity[Y]                                      0.12904E-03 
c  Velocity[Z]                                      0.42502E-02 
c  Pressure     0.36441E-04     133   0.92749E-02   0.25704E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56441E-08   0.16810E-08 0.10040E+00 
c  r22          0.10852E-01      13   0.51694E-08   0.18630E-08 0.10214E+00 
c  r33          0.21860E-01      15   0.69427E-08   0.12850E-07 0.12841E+00 
c  r12          0.93866E-03      18   0.60768E-08   0.30294E-09 0.60949E+00 
c  r13          0.46676E-02      19   0.73750E-08   0.14913E-08 0.19987E+00 
c  r23          0.39977E-02      19   0.58632E-08   0.13144E-08 0.20077E+00 
c  epsilon      0.10969E+02      11   0.34769E-08   0.10480E-01 0.17315E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.84609E-02 0.43388E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63324         0.61365       0.0052575       0.0015076
v  Velocity[Y]            -0.57379         0.54438       0.0030807      0.00087326
v  Velocity[Z]              1.5651          5.4389          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4389          4.3406          4.3632
v  Pressure                 -36.39          360.04          87.654          169.86
v  r11                   0.0010615        0.081901        0.013074        0.018286
v  r22                   0.0011142        0.082642        0.013354        0.018646
v  r33                   0.0016407         0.17429        0.027252        0.037207
v  r12                   -0.010654        0.013582     -0.00023382     -0.00030931
v  r13                   -0.045532        0.052807      9.3225e-05       0.0010138
v  r23                   -0.046715        0.051201      3.0516e-05       0.0005746
v  epsilon                 0.06919           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099175      0.00092505       0.0017427
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2787         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71351         0.85283


 TIME FOR THE TIME STEP            10707:        0.70932E+02

===============================================================


 INSTANT    0.107080000E-01   TIME STEP NUMBER           10708
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208202203E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.255995193E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150476987E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.228123773E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.396383642E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81374E-03   0.44897E-02 0.19832E+01 
c  Velocity[X]                                      0.13712E-03 
c  Velocity[Y]                                      0.12713E-03 
c  Velocity[Z]                                      0.42254E-02 
c  Pressure     0.36211E-04     133   0.92190E-02   0.25542E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55933E-08   0.16335E-08 0.99083E-01 
c  r22          0.10852E-01      13   0.51989E-08   0.18484E-08 0.10165E+00 
c  r33          0.21860E-01      15   0.66881E-08   0.12558E-07 0.12717E+00 
c  r12          0.93866E-03      18   0.59650E-08   0.29329E-09 0.60174E+00 
c  r13          0.46676E-02      19   0.64771E-08   0.15117E-08 0.20020E+00 
c  r23          0.39977E-02      19   0.62200E-08   0.12783E-08 0.19854E+00 
c  epsilon      0.10969E+02      11   0.34078E-08   0.97356E-02 0.16378E+00 
c  TempC        0.25716E+06      16   0.15167E-04   0.83864E-02 0.43226E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63329         0.61366       0.0052575       0.0015076
v  Velocity[Y]             -0.5736         0.54422       0.0030806       0.0008732
v  Velocity[Z]               1.565          5.4389          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4389          4.3406          4.3632
v  Pressure                -36.435           360.1          87.687          169.91
v  r11                   0.0010615        0.081896        0.013074        0.018286
v  r22                   0.0011142        0.082641        0.013354        0.018646
v  r33                   0.0016407         0.17432        0.027252        0.037207
v  r12                   -0.010662         0.01358     -0.00023382     -0.00030931
v  r13                   -0.045535        0.052806      9.3225e-05       0.0010138
v  r23                   -0.046716        0.051225      3.0516e-05       0.0005746
v  epsilon                0.069191          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9933e-05       0.0099176      0.00092506       0.0017427
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71351         0.85283


 TIME FOR THE TIME STEP            10708:        0.69983E+02

===============================================================


 INSTANT    0.107090000E-01   TIME STEP NUMBER           10709
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.502903959E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.651152471E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.617345940E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.171475444E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.270226780E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81186E-03   0.45015E-02 0.19890E+01 
c  Velocity[X]                                      0.13712E-03 
c  Velocity[Y]                                      0.12732E-03 
c  Velocity[Z]                                      0.42371E-02 
c  Pressure     0.36059E-04     131   0.91777E-02   0.25435E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58103E-08   0.16150E-08 0.98691E-01 
c  r22          0.10852E-01      13   0.55340E-08   0.18055E-08 0.10094E+00 
c  r33          0.21860E-01      15   0.54319E-08   0.12392E-07 0.12662E+00 
c  r12          0.93866E-03      18   0.66108E-08   0.29319E-09 0.60162E+00 
c  r13          0.46676E-02      19   0.65724E-08   0.14845E-08 0.19932E+00 
c  r23          0.39977E-02      19   0.73984E-08   0.12753E-08 0.19819E+00 
c  epsilon      0.10969E+02      11   0.34086E-08   0.95883E-02 0.16289E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84464E-02 0.43349E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61363       0.0052575       0.0015076
v  Velocity[Y]            -0.57358         0.54433       0.0030806       0.0008732
v  Velocity[Z]              1.5651          5.4389          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4389          4.3406          4.3632
v  Pressure                -36.424          359.98          87.619          169.81
v  r11                   0.0010615        0.081891        0.013074        0.018286
v  r22                   0.0011142         0.08264        0.013354        0.018646
v  r33                   0.0016407         0.17429        0.027252        0.037207
v  r12                   -0.010664        0.013587     -0.00023382     -0.00030931
v  r13                   -0.045535        0.052805      9.3226e-05       0.0010138
v  r23                   -0.046717        0.051206      3.0517e-05       0.0005746
v  epsilon                0.069191          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9933e-05       0.0099177      0.00092506       0.0017427
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017851           5.278         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71351         0.85284


 TIME FOR THE TIME STEP            10709:        0.74246E+02

===============================================================


 INSTANT    0.107100000E-01   TIME STEP NUMBER           10710
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229594133E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.101596747E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.778611051E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.411726848E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.278618138E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81334E-03   0.45122E-02 0.19897E+01 
c  Velocity[X]                                      0.13792E-03 
c  Velocity[Y]                                      0.12915E-03 
c  Velocity[Z]                                      0.42452E-02 
c  Pressure     0.36200E-04     133   0.92175E-02   0.25534E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56958E-08   0.16283E-08 0.99418E-01 
c  r22          0.10852E-01      13   0.51881E-08   0.18119E-08 0.10132E+00 
c  r33          0.21860E-01      15   0.53511E-08   0.12392E-07 0.12687E+00 
c  r12          0.93866E-03      18   0.65709E-08   0.29088E-09 0.60246E+00 
c  r13          0.46676E-02      19   0.67814E-08   0.14761E-08 0.19970E+00 
c  r23          0.39977E-02      20   0.56626E-08   0.12595E-08 0.19841E+00 
c  epsilon      0.10969E+02      11   0.33751E-08   0.95660E-02 0.16331E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.84203E-02 0.43287E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63325         0.61364       0.0052575       0.0015076
v  Velocity[Y]            -0.57347          0.5445       0.0030806      0.00087323
v  Velocity[Z]               1.565          5.4389          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4389          4.3406          4.3632
v  Pressure                 -36.43          360.04          87.678          169.88
v  r11                   0.0010615        0.081889        0.013074        0.018286
v  r22                   0.0011142        0.082641        0.013354        0.018646
v  r33                   0.0016408         0.17427        0.027252        0.037207
v  r12                   -0.010662        0.013585     -0.00023382     -0.00030931
v  r13                   -0.045533        0.052806      9.3226e-05       0.0010138
v  r23                   -0.046717        0.051194      3.0517e-05       0.0005746
v  epsilon                0.069192          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099177      0.00092506       0.0017427
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017851           5.278         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71351         0.85284


 TIME FOR THE TIME STEP            10710:        0.75377E+02

===============================================================


 INSTANT    0.107110000E-01   TIME STEP NUMBER           10711
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.454650676E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.292634193E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.527996255E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935011E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.982538631E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.216878105E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81368E-03   0.44591E-02 0.19806E+01 
c  Velocity[X]                                      0.13776E-03 
c  Velocity[Y]                                      0.12742E-03 
c  Velocity[Z]                                      0.41939E-02 
c  Pressure     0.36235E-04     132   0.92300E-02   0.25559E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59917E-08   0.16453E-08 0.99660E-01 
c  r22          0.10852E-01      13   0.49248E-08   0.18303E-08 0.10187E+00 
c  r33          0.21860E-01      15   0.59011E-08   0.12520E-07 0.12741E+00 
c  r12          0.93866E-03      18   0.58053E-08   0.30878E-09 0.61042E+00 
c  r13          0.46676E-02      19   0.66413E-08   0.14905E-08 0.19989E+00 
c  r23          0.39977E-02      19   0.63831E-08   0.12935E-08 0.19984E+00 
c  epsilon      0.10969E+02      11   0.33559E-08   0.97970E-02 0.16523E+00 
c  TempC        0.25716E+06      16   0.15118E-04   0.83811E-02 0.43242E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63321         0.61366       0.0052575       0.0015076
v  Velocity[Y]            -0.57372         0.54438       0.0030807      0.00087329
v  Velocity[Z]              1.5649          5.4389          4.3387          4.3625
v  ǁVelocityǁ               1.5787          5.4389          4.3406          4.3632
v  Pressure                -36.422          359.98          87.609          169.81
v  r11                   0.0010615        0.081904        0.013074        0.018286
v  r22                   0.0011142        0.082639        0.013354        0.018646
v  r33                   0.0016408         0.17428        0.027252        0.037207
v  r12                   -0.010659        0.013583     -0.00023382     -0.00030931
v  r13                   -0.045536        0.052804      9.3226e-05       0.0010138
v  r23                   -0.046717        0.051218      3.0518e-05       0.0005746
v  epsilon                0.069193          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099178      0.00092506       0.0017427
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71351         0.85284


 TIME FOR THE TIME STEP            10711:        0.75695E+02

===============================================================


 INSTANT    0.107120000E-01   TIME STEP NUMBER           10712
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.310668929E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.143363629E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136128342E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.917366232E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.156406888E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      45   0.81165E-03   0.45244E-02 0.19937E+01 
c  Velocity[X]                                      0.13818E-03 
c  Velocity[Y]                                      0.12878E-03 
c  Velocity[Z]                                      0.42574E-02 
c  Pressure     0.36528E-04     133   0.92935E-02   0.25764E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55732E-08   0.16660E-08 0.10001E+00 
c  r22          0.10852E-01      13   0.53147E-08   0.18048E-08 0.10109E+00 
c  r33          0.21860E-01      15   0.68297E-08   0.12483E-07 0.12714E+00 
c  r12          0.93866E-03      18   0.57846E-08   0.30147E-09 0.60698E+00 
c  r13          0.46676E-02      19   0.64494E-08   0.14831E-08 0.19931E+00 
c  r23          0.39977E-02      19   0.66459E-08   0.13097E-08 0.20142E+00 
c  epsilon      0.10969E+02      11   0.34596E-08   0.98192E-02 0.16788E+00 
c  TempC        0.25716E+06      16   0.15183E-04   0.84014E-02 0.43276E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63331         0.61362       0.0052575       0.0015076
v  Velocity[Y]            -0.57374         0.54432       0.0030807      0.00087323
v  Velocity[Z]              1.5652          5.4389          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4389          4.3406          4.3632
v  Pressure                -36.414          359.94          87.604          169.79
v  r11                   0.0010615        0.081914        0.013074        0.018286
v  r22                   0.0011142        0.082638        0.013354        0.018646
v  r33                   0.0016408          0.1743        0.027252        0.037207
v  r12                   -0.010657         0.01358     -0.00023382     -0.00030931
v  r13                   -0.045534        0.052804      9.3226e-05       0.0010138
v  r23                   -0.046717        0.051205      3.0518e-05       0.0005746
v  epsilon                0.069193           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099177      0.00092506       0.0017427
v  CourantNb               0.44219             0.6         0.59908         0.59839
v  FourierNb             0.0017851           5.278         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71351         0.85283


 TIME FOR THE TIME STEP            10712:        0.71524E+02

===============================================================


 INSTANT    0.107130000E-01   TIME STEP NUMBER           10713
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.672104363E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.175885262E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229345743E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.310666643E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.247353487E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81328E-03   0.45332E-02 0.19908E+01 
c  Velocity[X]                                      0.13807E-03 
c  Velocity[Y]                                      0.12832E-03 
c  Velocity[Z]                                      0.42668E-02 
c  Pressure     0.35829E-04     132   0.91266E-02   0.25273E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55195E-08   0.16459E-08 0.99684E-01 
c  r22          0.10852E-01      13   0.52559E-08   0.18161E-08 0.10105E+00 
c  r33          0.21860E-01      15   0.63436E-08   0.12437E-07 0.12663E+00 
c  r12          0.93866E-03      18   0.57048E-08   0.29971E-09 0.60769E+00 
c  r13          0.46676E-02      19   0.60667E-08   0.14871E-08 0.20015E+00 
c  r23          0.39977E-02      19   0.60812E-08   0.12809E-08 0.19926E+00 
c  epsilon      0.10969E+02      11   0.33598E-08   0.95670E-02 0.16172E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84483E-02 0.43347E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61365       0.0052576       0.0015076
v  Velocity[Y]            -0.57383         0.54439       0.0030807      0.00087326
v  Velocity[Z]              1.5651           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5789           5.439          4.3406          4.3632
v  Pressure                -36.378          360.03          87.648          169.86
v  r11                   0.0010615         0.08192        0.013074        0.018286
v  r22                   0.0011143        0.082639        0.013354        0.018646
v  r33                   0.0016408         0.17429        0.027252        0.037207
v  r12                   -0.010655        0.013583     -0.00023382     -0.00030931
v  r13                   -0.045534        0.052805      9.3227e-05       0.0010138
v  r23                   -0.046717        0.051185      3.0519e-05       0.0005746
v  epsilon                0.069194           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099178      0.00092506       0.0017427
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2776         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71351         0.85284


 TIME FOR THE TIME STEP            10713:        0.72491E+02

===============================================================


 INSTANT    0.107140000E-01   TIME STEP NUMBER           10714
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.176646728E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.275889111E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.173894463E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145653164E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.381428310E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81297E-03   0.45241E-02 0.19927E+01 
c  Velocity[X]                                      0.13831E-03 
c  Velocity[Y]                                      0.12813E-03 
c  Velocity[Z]                                      0.42576E-02 
c  Pressure     0.36515E-04     132   0.93009E-02   0.25756E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54092E-08   0.16213E-08 0.98964E-01 
c  r22          0.10852E-01      13   0.51443E-08   0.18265E-08 0.10097E+00 
c  r33          0.21860E-01      15   0.65702E-08   0.12492E-07 0.12697E+00 
c  r12          0.93866E-03      18   0.58936E-08   0.29739E-09 0.60537E+00 
c  r13          0.46676E-02      19   0.68096E-08   0.15073E-08 0.20017E+00 
c  r23          0.39977E-02      19   0.68063E-08   0.12766E-08 0.19871E+00 
c  epsilon      0.10969E+02      11   0.33338E-08   0.98273E-02 0.16386E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84136E-02 0.43220E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61364       0.0052575       0.0015076
v  Velocity[Y]             -0.5737         0.54452       0.0030807      0.00087322
v  Velocity[Z]              1.5653           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5791           5.439          4.3406          4.3632
v  Pressure                -36.458          359.99          87.625          169.82
v  r11                   0.0010615        0.081918        0.013074        0.018286
v  r22                   0.0011143        0.082636        0.013354        0.018646
v  r33                   0.0016408         0.17426        0.027252        0.037207
v  r12                   -0.010654        0.013586     -0.00023382     -0.00030931
v  r13                   -0.045536        0.052807      9.3226e-05       0.0010138
v  r23                   -0.046718        0.051175      3.0519e-05       0.0005746
v  epsilon                0.069195          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.994e-05       0.0099177      0.00092506       0.0017427
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2773         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71351         0.85284


 TIME FOR THE TIME STEP            10714:        0.70728E+02

===============================================================


 INSTANT    0.107150000E-01   TIME STEP NUMBER           10715
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.559325243E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157380531E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.562740670E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.429124623E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.505651122E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81185E-03   0.45157E-02 0.19921E+01 
c  Velocity[X]                                      0.13850E-03 
c  Velocity[Y]                                      0.12804E-03 
c  Velocity[Z]                                      0.42492E-02 
c  Pressure     0.36395E-04     133   0.92697E-02   0.25671E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53314E-08   0.16246E-08 0.99083E-01 
c  r22          0.10852E-01      13   0.49129E-08   0.18306E-08 0.10128E+00 
c  r33          0.21860E-01      15   0.60729E-08   0.12490E-07 0.12705E+00 
c  r12          0.93866E-03      18   0.53724E-08   0.29790E-09 0.60791E+00 
c  r13          0.46676E-02      19   0.60656E-08   0.14975E-08 0.19992E+00 
c  r23          0.39977E-02      19   0.69800E-08   0.12719E-08 0.19857E+00 
c  epsilon      0.10969E+02      11   0.34812E-08   0.99638E-02 0.16572E+00 
c  TempC        0.25716E+06      16   0.15112E-04   0.84229E-02 0.43272E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63329         0.61361       0.0052574       0.0015076
v  Velocity[Y]            -0.57387         0.54435       0.0030807      0.00087323
v  Velocity[Z]               1.565           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5789           5.439          4.3406          4.3632
v  Pressure                -36.373          360.03          87.652          169.86
v  r11                   0.0010615        0.081916        0.013074        0.018286
v  r22                   0.0011143        0.082637        0.013354        0.018646
v  r33                   0.0016409         0.17427        0.027252        0.037207
v  r12                   -0.010653        0.013586     -0.00023382     -0.00030931
v  r13                   -0.045533        0.052807      9.3226e-05       0.0010138
v  r23                   -0.046718        0.051201      3.0519e-05       0.0005746
v  epsilon                0.069195          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9943e-05       0.0099177      0.00092506       0.0017427
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2772         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85284


 TIME FOR THE TIME STEP            10715:        0.71531E+02

===============================================================


 INSTANT    0.107160000E-01   TIME STEP NUMBER           10716
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.297360525E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.420977264E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.843537549E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.861047072E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.497923295E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81382E-03   0.45149E-02 0.19898E+01 
c  Velocity[X]                                      0.13796E-03 
c  Velocity[Y]                                      0.12832E-03 
c  Velocity[Z]                                      0.42487E-02 
c  Pressure     0.36365E-04     132   0.92602E-02   0.25651E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55036E-08   0.16023E-08 0.98986E-01 
c  r22          0.10852E-01      13   0.50284E-08   0.17898E-08 0.10074E+00 
c  r33          0.21860E-01      15   0.57342E-08   0.12240E-07 0.12644E+00 
c  r12          0.93866E-03      18   0.56566E-08   0.29431E-09 0.60555E+00 
c  r13          0.46676E-02      19   0.64131E-08   0.14588E-08 0.19866E+00 
c  r23          0.39978E-02      19   0.61331E-08   0.12615E-08 0.19868E+00 
c  epsilon      0.10969E+02      11   0.33740E-08   0.94739E-02 0.16164E+00 
c  TempC        0.25716E+06      16   0.15172E-04   0.84194E-02 0.43339E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61364       0.0052575       0.0015076
v  Velocity[Y]            -0.57377         0.54443       0.0030807      0.00087324
v  Velocity[Z]              1.5653           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5791           5.439          4.3406          4.3632
v  Pressure                -36.443          360.02           87.65          169.85
v  r11                   0.0010615        0.081916        0.013074        0.018286
v  r22                   0.0011143        0.082639        0.013354        0.018646
v  r33                   0.0016409          0.1743        0.027252        0.037207
v  r12                   -0.010659        0.013585     -0.00023382     -0.00030931
v  r13                   -0.045532        0.052806      9.3227e-05       0.0010138
v  r23                   -0.046717         0.05119      3.0519e-05       0.0005746
v  epsilon                0.069196           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9944e-05       0.0099176      0.00092506       0.0017427
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2771         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71351         0.85284


 TIME FOR THE TIME STEP            10716:        0.75966E+02

===============================================================


 INSTANT    0.107170000E-01   TIME STEP NUMBER           10717
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.331906785E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.751769759E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.138049663E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935011E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151243294E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.556072434E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935016E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81206E-03   0.45020E-02 0.19867E+01 
c  Velocity[X]                                      0.13743E-03 
c  Velocity[Y]                                      0.12852E-03 
c  Velocity[Z]                                      0.42360E-02 
c  Pressure     0.36507E-04     132   0.92874E-02   0.25750E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55239E-08   0.16083E-08 0.98778E-01 
c  r22          0.10852E-01      13   0.49826E-08   0.17941E-08 0.10069E+00 
c  r33          0.21860E-01      15   0.56448E-08   0.12322E-07 0.12621E+00 
c  r12          0.93866E-03      18   0.54356E-08   0.29331E-09 0.60101E+00 
c  r13          0.46676E-02      19   0.70830E-08   0.14959E-08 0.19916E+00 
c  r23          0.39978E-02      19   0.56820E-08   0.12676E-08 0.19796E+00 
c  epsilon      0.10969E+02      11   0.33347E-08   0.97187E-02 0.16242E+00 
c  TempC        0.25716E+06      16   0.15124E-04   0.83926E-02 0.43210E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61365       0.0052576       0.0015076
v  Velocity[Y]            -0.57373         0.54454       0.0030808      0.00087329
v  Velocity[Z]              1.5651           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5789           5.439          4.3406          4.3632
v  Pressure                 -36.42          359.98           87.59           169.8
v  r11                   0.0010615        0.081915        0.013074        0.018286
v  r22                   0.0011143        0.082641        0.013354        0.018646
v  r33                   0.0016409         0.17428        0.027252        0.037207
v  r12                   -0.010658        0.013592     -0.00023382     -0.00030931
v  r13                   -0.045536        0.052805      9.3227e-05       0.0010138
v  r23                   -0.046717        0.051181      3.0519e-05       0.0005746
v  epsilon                0.069197          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099177      0.00092506       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2772         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71351         0.85284


 TIME FOR THE TIME STEP            10717:        0.74751E+02

===============================================================


 INSTANT    0.107180000E-01   TIME STEP NUMBER           10718
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106622649E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.344257305E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.259009170E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.352538957E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.350038125E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81273E-03   0.45157E-02 0.19905E+01 
c  Velocity[X]                                      0.13785E-03 
c  Velocity[Y]                                      0.12856E-03 
c  Velocity[Z]                                      0.42493E-02 
c  Pressure     0.36134E-04     132   0.92036E-02   0.25488E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57993E-08   0.16289E-08 0.99651E-01 
c  r22          0.10852E-01      13   0.49823E-08   0.17791E-08 0.10049E+00 
c  r33          0.21860E-01      15   0.60540E-08   0.12252E-07 0.12640E+00 
c  r12          0.93866E-03      18   0.49203E-08   0.29727E-09 0.60298E+00 
c  r13          0.46676E-02      19   0.62594E-08   0.14507E-08 0.19764E+00 
c  r23          0.39978E-02      19   0.52528E-08   0.12919E-08 0.20090E+00 
c  epsilon      0.10969E+02      11   0.32872E-08   0.97550E-02 0.16821E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.83610E-02 0.43150E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63335          0.6136       0.0052576       0.0015076
v  Velocity[Y]            -0.57365         0.54441       0.0030807      0.00087328
v  Velocity[Z]              1.5651           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5789           5.439          4.3406          4.3632
v  Pressure                -36.442             360          87.641          169.83
v  r11                   0.0010615        0.081909        0.013074        0.018286
v  r22                   0.0011143         0.08264        0.013354        0.018646
v  r33                   0.0016409         0.17426        0.027252        0.037207
v  r12                   -0.010658        0.013592     -0.00023382     -0.00030931
v  r13                   -0.045533        0.052806      9.3228e-05       0.0010138
v  r23                   -0.046717         0.05121       3.052e-05       0.0005746
v  epsilon                0.069198          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099176      0.00092506       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017851           5.277         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71351         0.85284


 TIME FOR THE TIME STEP            10718:        0.73455E+02

===============================================================


 INSTANT    0.107190000E-01   TIME STEP NUMBER           10719
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.196160511E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.131030662E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130065917E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.239590063E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.154132860E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81219E-03   0.45300E-02 0.19930E+01 
c  Velocity[X]                                      0.13795E-03 
c  Velocity[Y]                                      0.12795E-03 
c  Velocity[Z]                                      0.42641E-02 
c  Pressure     0.36379E-04     133   0.92577E-02   0.25661E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60039E-08   0.16205E-08 0.98514E-01 
c  r22          0.10852E-01      13   0.48289E-08   0.18258E-08 0.10077E+00 
c  r33          0.21860E-01      15   0.63524E-08   0.12499E-07 0.12601E+00 
c  r12          0.93866E-03      18   0.49802E-08   0.29088E-09 0.59847E+00 
c  r13          0.46676E-02      19   0.57574E-08   0.14825E-08 0.19782E+00 
c  r23          0.39978E-02      19   0.57383E-08   0.12646E-08 0.19667E+00 
c  epsilon      0.10969E+02      11   0.33281E-08   0.10157E-01 0.16605E+00 
c  TempC        0.25716E+06      16   0.15110E-04   0.84992E-02 0.43455E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61364       0.0052576       0.0015077
v  Velocity[Y]            -0.57375         0.54433       0.0030808      0.00087332
v  Velocity[Z]              1.5652           5.439          4.3387          4.3625
v  ǁVelocityǁ                1.579           5.439          4.3406          4.3632
v  Pressure                -36.392             360          87.614          169.82
v  r11                   0.0010615        0.081909        0.013074        0.018286
v  r22                   0.0011143        0.082641        0.013354        0.018646
v  r33                   0.0016409         0.17428        0.027252        0.037207
v  r12                   -0.010655        0.013588     -0.00023382     -0.00030931
v  r13                   -0.045532        0.052806      9.3228e-05       0.0010138
v  r23                   -0.046716        0.051191       3.052e-05       0.0005746
v  epsilon                0.069198          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9951e-05       0.0099175      0.00092506       0.0017427
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2773         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71351         0.85283


 TIME FOR THE TIME STEP            10719:        0.74071E+02

===============================================================


 INSTANT    0.107200000E-01   TIME STEP NUMBER           10720
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.557916798E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249566985E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125483545E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.236409615E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.212731149E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81328E-03   0.44528E-02 0.19782E+01 
c  Velocity[X]                                      0.13717E-03 
c  Velocity[Y]                                      0.12708E-03 
c  Velocity[Z]                                      0.41885E-02 
c  Pressure     0.36036E-04     131   0.91786E-02   0.25418E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53075E-08   0.16230E-08 0.98638E-01 
c  r22          0.10852E-01      13   0.48969E-08   0.18256E-08 0.10071E+00 
c  r33          0.21860E-01      14   0.65504E-08   0.12445E-07 0.12598E+00 
c  r12          0.93867E-03      18   0.52318E-08   0.29631E-09 0.60186E+00 
c  r13          0.46676E-02      18   0.69260E-08   0.14990E-08 0.19816E+00 
c  r23          0.39978E-02      19   0.59852E-08   0.12791E-08 0.19778E+00 
c  epsilon      0.10969E+02      11   0.31766E-08   0.99235E-02 0.16418E+00 
c  TempC        0.25716E+06      16   0.15169E-04   0.84119E-02 0.43252E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61365       0.0052575       0.0015076
v  Velocity[Y]            -0.57369         0.54435       0.0030808      0.00087333
v  Velocity[Z]              1.5652           5.439          4.3387          4.3625
v  ǁVelocityǁ                1.579           5.439          4.3406          4.3632
v  Pressure                -36.448          359.99          87.619          169.82
v  r11                   0.0010616          0.0819        0.013074        0.018286
v  r22                   0.0011143         0.08264        0.013354        0.018646
v  r33                    0.001641          0.1743        0.027252        0.037207
v  r12                   -0.010652        0.013589     -0.00023382     -0.00030931
v  r13                   -0.045534        0.052805      9.3229e-05       0.0010138
v  r23                   -0.046715        0.051179       3.052e-05       0.0005746
v  epsilon                0.069199          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099174      0.00092507       0.0017427
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2774         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71351         0.85284


 TIME FOR THE TIME STEP            10720:        0.72749E+02

===============================================================


 INSTANT    0.107210000E-01   TIME STEP NUMBER           10721
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.188298110E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.302347366E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.217968577E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.101965492E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.186231517E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81214E-03   0.44989E-02 0.19877E+01 
c  Velocity[X]                                      0.13855E-03 
c  Velocity[Y]                                      0.12828E-03 
c  Velocity[Z]                                      0.42320E-02 
c  Pressure     0.36424E-04     133   0.92762E-02   0.25692E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54524E-08   0.15904E-08 0.98134E-01 
c  r22          0.10852E-01      13   0.52988E-08   0.18090E-08 0.10030E+00 
c  r33          0.21860E-01      15   0.57037E-08   0.12284E-07 0.12531E+00 
c  r12          0.93867E-03      18   0.53934E-08   0.29377E-09 0.60234E+00 
c  r13          0.46676E-02      19   0.55084E-08   0.15007E-08 0.19804E+00 
c  r23          0.39978E-02      19   0.69195E-08   0.12566E-08 0.19616E+00 
c  epsilon      0.10969E+02      11   0.33860E-08   0.97746E-02 0.16383E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.84157E-02 0.43319E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63329         0.61362       0.0052576       0.0015076
v  Velocity[Y]            -0.57378         0.54432       0.0030807      0.00087328
v  Velocity[Z]              1.5653           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5791           5.439          4.3406          4.3632
v  Pressure                -36.417          359.97          87.608          169.81
v  r11                   0.0010616         0.08189        0.013074        0.018286
v  r22                   0.0011143        0.082636        0.013354        0.018646
v  r33                    0.001641         0.17429        0.027252        0.037207
v  r12                    -0.01065        0.013589     -0.00023382     -0.00030931
v  r13                   -0.045533        0.052808      9.3229e-05       0.0010138
v  r23                   -0.046715        0.051168       3.052e-05       0.0005746
v  epsilon                  0.0692          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099175      0.00092507       0.0017427
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2776         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71351         0.85284


 TIME FOR THE TIME STEP            10721:        0.74148E+02

===============================================================


 INSTANT    0.107220000E-01   TIME STEP NUMBER           10722
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.118427802E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.124811319E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.171026283E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.929241739E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.109933506E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81263E-03   0.45702E-02 0.19995E+01 
c  Velocity[X]                                      0.13818E-03 
c  Velocity[Y]                                      0.12919E-03 
c  Velocity[Z]                                      0.43029E-02 
c  Pressure     0.36355E-04     133   0.92535E-02   0.25643E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57294E-08   0.16401E-08 0.99035E-01 
c  r22          0.10852E-01      13   0.52021E-08   0.18413E-08 0.10121E+00 
c  r33          0.21860E-01      15   0.61205E-08   0.12645E-07 0.12701E+00 
c  r12          0.93867E-03      18   0.60092E-08   0.29755E-09 0.60680E+00 
c  r13          0.46676E-02      19   0.60182E-08   0.15012E-08 0.19998E+00 
c  r23          0.39978E-02      19   0.70380E-08   0.12744E-08 0.19770E+00 
c  epsilon      0.10969E+02      11   0.35757E-08   0.10273E-01 0.16751E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.84297E-02 0.43318E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61364       0.0052575       0.0015076
v  Velocity[Y]            -0.57388         0.54441       0.0030808      0.00087331
v  Velocity[Z]              1.5652           5.439          4.3387          4.3625
v  ǁVelocityǁ                1.579           5.439          4.3406          4.3632
v  Pressure                -36.462          359.98          87.633          169.82
v  r11                   0.0010616        0.081887        0.013074        0.018286
v  r22                   0.0011143        0.082636        0.013354        0.018646
v  r33                    0.001641         0.17427        0.027252        0.037207
v  r12                    -0.01065        0.013585     -0.00023382     -0.00030931
v  r13                   -0.045531        0.052808       9.323e-05       0.0010138
v  r23                   -0.046713        0.051193       3.052e-05       0.0005746
v  epsilon                  0.0692          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9948e-05       0.0099177      0.00092507       0.0017427
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2772         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71351         0.85284


 TIME FOR THE TIME STEP            10722:        0.74790E+02

===============================================================


 INSTANT    0.107230000E-01   TIME STEP NUMBER           10723
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.160808043E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.992346315E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.359100917E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935023E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.413525634E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.271851144E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81294E-03   0.44857E-02 0.19831E+01 
c  Velocity[X]                                      0.13790E-03 
c  Velocity[Y]                                      0.12832E-03 
c  Velocity[Z]                                      0.42195E-02 
c  Pressure     0.36009E-04     131   0.91670E-02   0.25399E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54825E-08   0.16276E-08 0.98926E-01 
c  r22          0.10852E-01      13   0.51500E-08   0.18099E-08 0.10093E+00 
c  r33          0.21860E-01      15   0.57893E-08   0.12414E-07 0.12662E+00 
c  r12          0.93867E-03      18   0.52971E-08   0.30142E-09 0.60722E+00 
c  r13          0.46676E-02      19   0.65680E-08   0.14848E-08 0.19928E+00 
c  r23          0.39978E-02      19   0.62619E-08   0.12969E-08 0.19940E+00 
c  epsilon      0.10969E+02      11   0.33686E-08   0.96941E-02 0.16407E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.83732E-02 0.43139E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161988


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61367       0.0052576       0.0015076
v  Velocity[Y]            -0.57384         0.54421       0.0030808       0.0008733
v  Velocity[Z]               1.565           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5788           5.439          4.3406          4.3632
v  Pressure                -36.446          360.01          87.606          169.82
v  r11                   0.0010616        0.081883        0.013074        0.018286
v  r22                   0.0011143        0.082637        0.013355        0.018646
v  r33                    0.001641         0.17428        0.027252        0.037207
v  r12                   -0.010652         0.01359     -0.00023382     -0.00030931
v  r13                   -0.045533        0.052805       9.323e-05       0.0010138
v  r23                   -0.046712        0.051185       3.052e-05       0.0005746
v  epsilon                0.069201          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099175      0.00092507       0.0017427
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2773         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71351         0.85284


 TIME FOR THE TIME STEP            10723:        0.71495E+02

===============================================================


 INSTANT    0.107240000E-01   TIME STEP NUMBER           10724
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.724644407E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.676859491E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934918E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172142806E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.133838276E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.378975513E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81213E-03   0.44941E-02 0.19889E+01 
c  Velocity[X]                                      0.13762E-03 
c  Velocity[Y]                                      0.12821E-03 
c  Velocity[Z]                                      0.42282E-02 
c  Pressure     0.36744E-04     132   0.93531E-02   0.25917E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50068E-08   0.16074E-08 0.98826E-01 
c  r22          0.10852E-01      13   0.48119E-08   0.17907E-08 0.10017E+00 
c  r33          0.21860E-01      15   0.57132E-08   0.12274E-07 0.12609E+00 
c  r12          0.93867E-03      17   0.67686E-08   0.29504E-09 0.60472E+00 
c  r13          0.46676E-02      19   0.62026E-08   0.14555E-08 0.19662E+00 
c  r23          0.39978E-02      19   0.61818E-08   0.12874E-08 0.20002E+00 
c  epsilon      0.10969E+02      11   0.32858E-08   0.98393E-02 0.16850E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.84741E-02 0.43401E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61364       0.0052576       0.0015076
v  Velocity[Y]            -0.57384         0.54429       0.0030807      0.00087324
v  Velocity[Z]              1.5652           5.439          4.3387          4.3625
v  ǁVelocityǁ                1.579           5.439          4.3406          4.3632
v  Pressure                -36.438          359.99           87.62          169.82
v  r11                   0.0010616        0.081879        0.013074        0.018286
v  r22                   0.0011144        0.082636        0.013355        0.018646
v  r33                    0.001641         0.17431        0.027252        0.037207
v  r12                   -0.010653        0.013592     -0.00023382     -0.00030931
v  r13                   -0.045531        0.052805       9.323e-05       0.0010138
v  r23                    -0.04671        0.051183       3.052e-05       0.0005746
v  epsilon                0.069202          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9941e-05       0.0099176      0.00092507       0.0017427
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2777         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71351         0.85283


 TIME FOR THE TIME STEP            10724:        0.73039E+02

===============================================================


 INSTANT    0.107250000E-01   TIME STEP NUMBER           10725
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.290600354E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.207888352E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934904E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.359889311E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.287044619E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229700313E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81240E-03   0.45446E-02 0.19938E+01 
c  Velocity[X]                                      0.13835E-03 
c  Velocity[Y]                                      0.12895E-03 
c  Velocity[Z]                                      0.42773E-02 
c  Pressure     0.36439E-04     133   0.92760E-02   0.25702E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51024E-08   0.16200E-08 0.98865E-01 
c  r22          0.10852E-01      13   0.47668E-08   0.18301E-08 0.10110E+00 
c  r33          0.21860E-01      14   0.69053E-08   0.12414E-07 0.12639E+00 
c  r12          0.93867E-03      18   0.50055E-08   0.29515E-09 0.60249E+00 
c  r13          0.46676E-02      19   0.62279E-08   0.14989E-08 0.19923E+00 
c  r23          0.39978E-02      19   0.67047E-08   0.12658E-08 0.19777E+00 
c  epsilon      0.10969E+02      11   0.32240E-08   0.98815E-02 0.16468E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.84011E-02 0.43249E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61365       0.0052576       0.0015077
v  Velocity[Y]            -0.57385         0.54443       0.0030808      0.00087331
v  Velocity[Z]              1.5652           5.439          4.3387          4.3625
v  ǁVelocityǁ                1.579           5.439          4.3406          4.3632
v  Pressure                -36.435           360.1          87.698          169.92
v  r11                   0.0010616        0.081876        0.013074        0.018286
v  r22                   0.0011144        0.082636        0.013355        0.018646
v  r33                   0.0016411          0.1743        0.027252        0.037207
v  r12                   -0.010653        0.013592     -0.00023382     -0.00030931
v  r13                   -0.045532        0.052806      9.3231e-05       0.0010138
v  r23                   -0.046709        0.051206       3.052e-05       0.0005746
v  epsilon                0.069202          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9939e-05       0.0099176      0.00092507       0.0017427
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2783         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71351         0.85284


 TIME FOR THE TIME STEP            10725:        0.73416E+02

===============================================================


 INSTANT    0.107260000E-01   TIME STEP NUMBER           10726
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.745413139E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.127348683E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154121784E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935014E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116685298E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.341341005E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81324E-03   0.45084E-02 0.19904E+01 
c  Velocity[X]                                      0.13798E-03 
c  Velocity[Y]                                      0.12867E-03 
c  Velocity[Z]                                      0.42418E-02 
c  Pressure     0.36177E-04     132   0.92114E-02   0.25517E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50785E-08   0.16006E-08 0.98273E-01 
c  r22          0.10852E-01      13   0.47442E-08   0.18140E-08 0.10097E+00 
c  r33          0.21860E-01      14   0.68123E-08   0.12349E-07 0.12626E+00 
c  r12          0.93867E-03      18   0.51380E-08   0.29850E-09 0.60430E+00 
c  r13          0.46676E-02      19   0.61453E-08   0.15006E-08 0.19978E+00 
c  r23          0.39978E-02      19   0.58480E-08   0.12590E-08 0.19719E+00 
c  epsilon      0.10969E+02      11   0.31175E-08   0.96724E-02 0.16333E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.83370E-02 0.43088E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61368       0.0052576       0.0015076
v  Velocity[Y]            -0.57385         0.54426       0.0030807      0.00087326
v  Velocity[Z]              1.5653           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5791           5.439          4.3406          4.3632
v  Pressure                -36.471          359.99          87.625          169.82
v  r11                   0.0010616        0.081874        0.013074        0.018286
v  r22                   0.0011144        0.082637        0.013355        0.018646
v  r33                   0.0016411         0.17425        0.027252        0.037207
v  r12                   -0.010653        0.013594     -0.00023382     -0.00030931
v  r13                   -0.045534        0.052806      9.3231e-05       0.0010138
v  r23                   -0.046708        0.051194      3.0521e-05       0.0005746
v  epsilon                0.069203           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099177      0.00092507       0.0017427
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71351         0.85284


 TIME FOR THE TIME STEP            10726:        0.72015E+02

===============================================================


 INSTANT    0.107270000E-01   TIME STEP NUMBER           10727
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.141959404E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283741206E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.442016313E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.442511759E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.913544104E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81184E-03   0.45145E-02 0.19906E+01 
c  Velocity[X]                                      0.13849E-03 
c  Velocity[Y]                                      0.12782E-03 
c  Velocity[Z]                                      0.42482E-02 
c  Pressure     0.36166E-04     131   0.92135E-02   0.25510E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53246E-08   0.16333E-08 0.98926E-01 
c  r22          0.10852E-01      13   0.49589E-08   0.18015E-08 0.10054E+00 
c  r33          0.21860E-01      14   0.68360E-08   0.12439E-07 0.12647E+00 
c  r12          0.93867E-03      18   0.53277E-08   0.30132E-09 0.60794E+00 
c  r13          0.46676E-02      19   0.57833E-08   0.14771E-08 0.19856E+00 
c  r23          0.39978E-02      19   0.61005E-08   0.12829E-08 0.19820E+00 
c  epsilon      0.10969E+02      11   0.32614E-08   0.98572E-02 0.16539E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.84046E-02 0.43273E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61367       0.0052576       0.0015076
v  Velocity[Y]            -0.57384         0.54421       0.0030807      0.00087327
v  Velocity[Z]              1.5651           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4391          4.3406          4.3632
v  Pressure                -36.432          359.98          87.604          169.81
v  r11                   0.0010616        0.081876        0.013074        0.018286
v  r22                   0.0011144        0.082635        0.013355        0.018646
v  r33                   0.0016411         0.17427        0.027252        0.037207
v  r12                   -0.010659        0.013595     -0.00023382     -0.00030931
v  r13                   -0.045532        0.052804      9.3231e-05       0.0010138
v  r23                   -0.046708        0.051179      3.0521e-05       0.0005746
v  epsilon                0.069204          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099177      0.00092507       0.0017427
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2787         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71351         0.85284


 TIME FOR THE TIME STEP            10727:        0.94419E+02

===============================================================


 INSTANT    0.107280000E-01   TIME STEP NUMBER           10728
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.649929636E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125516815E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.530820566E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154191875E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191211038E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81316E-03   0.45236E-02 0.19920E+01 
c  Velocity[X]                                      0.13783E-03 
c  Velocity[Y]                                      0.12833E-03 
c  Velocity[Z]                                      0.42574E-02 
c  Pressure     0.36292E-04     133   0.92405E-02   0.25599E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55826E-08   0.16732E-08 0.10020E+00 
c  r22          0.10852E-01      13   0.51335E-08   0.18465E-08 0.10126E+00 
c  r33          0.21860E-01      14   0.68995E-08   0.12724E-07 0.12764E+00 
c  r12          0.93867E-03      18   0.63731E-08   0.29861E-09 0.60834E+00 
c  r13          0.46676E-02      19   0.57782E-08   0.14864E-08 0.19903E+00 
c  r23          0.39978E-02      19   0.53739E-08   0.12838E-08 0.19981E+00 
c  epsilon      0.10969E+02      11   0.34934E-08   0.10136E-01 0.16714E+00 
c  TempC        0.25716E+06      16   0.15189E-04   0.84477E-02 0.43345E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63336         0.61368       0.0052576       0.0015076
v  Velocity[Y]            -0.57374         0.54428       0.0030807      0.00087326
v  Velocity[Z]              1.5652           5.439          4.3387          4.3625
v  ǁVelocityǁ                1.579           5.439          4.3406          4.3632
v  Pressure                -36.465          359.98          87.617          169.82
v  r11                   0.0010616        0.081873        0.013074        0.018286
v  r22                   0.0011144        0.082636        0.013355        0.018646
v  r33                   0.0016411         0.17431        0.027252        0.037207
v  r12                   -0.010659        0.013591     -0.00023382     -0.00030931
v  r13                    -0.04553        0.052805      9.3232e-05       0.0010138
v  r23                   -0.046708        0.051204      3.0523e-05       0.0005746
v  epsilon                0.069205          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05       0.0099177      0.00092507       0.0017427
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2782         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71351         0.85284


 TIME FOR THE TIME STEP            10728:        0.28631E+03

===============================================================


 INSTANT    0.107290000E-01   TIME STEP NUMBER           10729
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.192430442E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.108017384E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154863725E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119484791E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.814254486E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81247E-03   0.45210E-02 0.19932E+01 
c  Velocity[X]                                      0.13793E-03 
c  Velocity[Y]                                      0.12781E-03 
c  Velocity[Z]                                      0.42552E-02 
c  Pressure     0.36616E-04     131   0.93199E-02   0.25828E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60728E-08   0.17180E-08 0.10142E+00 
c  r22          0.10852E-01      13   0.49511E-08   0.18383E-08 0.10142E+00 
c  r33          0.21860E-01      14   0.67101E-08   0.12866E-07 0.12854E+00 
c  r12          0.93867E-03      18   0.63625E-08   0.30858E-09 0.61395E+00 
c  r13          0.46676E-02      18   0.68484E-08   0.15082E-08 0.19924E+00 
c  r23          0.39978E-02      19   0.50983E-08   0.13438E-08 0.20319E+00 
c  epsilon      0.10969E+02      11   0.34974E-08   0.98832E-02 0.16516E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.84562E-02 0.43374E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63333         0.61371       0.0052576       0.0015077
v  Velocity[Y]            -0.57383         0.54437       0.0030808      0.00087326
v  Velocity[Z]              1.5651          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4391          4.3406          4.3632
v  Pressure                -36.436          360.03          87.623          169.84
v  r11                   0.0010616        0.081874        0.013075        0.018286
v  r22                   0.0011144        0.082633        0.013355        0.018646
v  r33                   0.0016411         0.17428        0.027252        0.037207
v  r12                   -0.010659        0.013598     -0.00023382     -0.00030931
v  r13                   -0.045534        0.052805      9.3233e-05       0.0010138
v  r23                   -0.046709        0.051197      3.0523e-05       0.0005746
v  epsilon                0.069205           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9933e-05       0.0099177      0.00092507       0.0017427
v  CourantNb                0.4422             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71351         0.85284


 TIME FOR THE TIME STEP            10729:        0.73579E+02

===============================================================


 INSTANT    0.107300000E-01   TIME STEP NUMBER           10730
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.210223936E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.363860475E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.512823386E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.557313323E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.259496190E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81224E-03   0.45413E-02 0.19961E+01 
c  Velocity[X]                                      0.13813E-03 
c  Velocity[Y]                                      0.12895E-03 
c  Velocity[Z]                                      0.42742E-02 
c  Pressure     0.36483E-04     133   0.92826E-02   0.25733E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50700E-08   0.16583E-08 0.10032E+00 
c  r22          0.10852E-01      13   0.46864E-08   0.17980E-08 0.10078E+00 
c  r33          0.21860E-01      15   0.55117E-08   0.12444E-07 0.12716E+00 
c  r12          0.93867E-03      18   0.55549E-08   0.29582E-09 0.60757E+00 
c  r13          0.46676E-02      18   0.71173E-08   0.14735E-08 0.19853E+00 
c  r23          0.39978E-02      19   0.57176E-08   0.12984E-08 0.20075E+00 
c  epsilon      0.10969E+02      11   0.34522E-08   0.10049E-01 0.16980E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.84230E-02 0.43248E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61365       0.0052576       0.0015077
v  Velocity[Y]            -0.57372         0.54416       0.0030807      0.00087322
v  Velocity[Z]              1.5652          5.4391          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4391          4.3406          4.3632
v  Pressure                 -36.48          360.03          87.667          169.86
v  r11                   0.0010616        0.081873        0.013075        0.018286
v  r22                   0.0011144        0.082634        0.013355        0.018646
v  r33                   0.0016411         0.17426        0.027252        0.037207
v  r12                   -0.010661        0.013596     -0.00023382     -0.00030931
v  r13                   -0.045532        0.052806      9.3234e-05       0.0010138
v  r23                   -0.046709        0.051187      3.0523e-05       0.0005746
v  epsilon                0.069206          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099176      0.00092507       0.0017427
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71351         0.85284


 TIME FOR THE TIME STEP            10730:        0.76535E+02

===============================================================


 INSTANT    0.107310000E-01   TIME STEP NUMBER           10731
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.103896998E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.835664925E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267535427E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.251760083E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.275825084E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81324E-03   0.45296E-02 0.19916E+01 
c  Velocity[X]                                      0.13834E-03 
c  Velocity[Y]                                      0.12834E-03 
c  Velocity[Z]                                      0.42629E-02 
c  Pressure     0.36260E-04     132   0.92338E-02   0.25576E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50960E-08   0.16661E-08 0.10018E+00 
c  r22          0.10852E-01      13   0.49943E-08   0.18140E-08 0.10124E+00 
c  r33          0.21860E-01      15   0.67207E-08   0.12476E-07 0.12694E+00 
c  r12          0.93867E-03      18   0.55397E-08   0.29594E-09 0.60787E+00 
c  r13          0.46676E-02      19   0.59609E-08   0.14532E-08 0.19767E+00 
c  r23          0.39978E-02      19   0.56871E-08   0.12908E-08 0.19909E+00 
c  epsilon      0.10969E+02      11   0.34194E-08   0.95251E-02 0.16213E+00 
c  TempC        0.25716E+06      16   0.15124E-04   0.84256E-02 0.43333E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61366       0.0052577       0.0015077
v  Velocity[Y]            -0.57365         0.54425       0.0030808      0.00087328
v  Velocity[Z]              1.5649          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5787          5.4391          4.3406          4.3632
v  Pressure                -36.443          359.99          87.617          169.82
v  r11                   0.0010616        0.081876        0.013075        0.018286
v  r22                   0.0011144        0.082636        0.013355        0.018646
v  r33                   0.0016412         0.17428        0.027252        0.037207
v  r12                   -0.010672        0.013594     -0.00023382     -0.00030931
v  r13                   -0.045531        0.052804      9.3234e-05       0.0010138
v  r23                   -0.046709        0.051211      3.0525e-05       0.0005746
v  epsilon                0.069207          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099175      0.00092508       0.0017427
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2782         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71351         0.85283


 TIME FOR THE TIME STEP            10731:        0.76709E+02

===============================================================


 INSTANT    0.107320000E-01   TIME STEP NUMBER           10732
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.204620661E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.355048343E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.141495977E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.383389069E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.211657232E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81348E-03   0.44935E-02 0.19861E+01 
c  Velocity[X]                                      0.13734E-03 
c  Velocity[Y]                                      0.12802E-03 
c  Velocity[Z]                                      0.42281E-02 
c  Pressure     0.36332E-04     132   0.92465E-02   0.25626E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49758E-08   0.16577E-08 0.99376E-01 
c  r22          0.10852E-01      13   0.49857E-08   0.18671E-08 0.10181E+00 
c  r33          0.21860E-01      15   0.61343E-08   0.12828E-07 0.12749E+00 
c  r12          0.93867E-03      18   0.51934E-08   0.30072E-09 0.60555E+00 
c  r13          0.46676E-02      19   0.64586E-08   0.15425E-08 0.20130E+00 
c  r23          0.39978E-02      19   0.62460E-08   0.13097E-08 0.19999E+00 
c  epsilon      0.10969E+02      11   0.34388E-08   0.10211E-01 0.16637E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.83666E-02 0.43232E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63332         0.61368       0.0052576       0.0015076
v  Velocity[Y]            -0.57358         0.54441       0.0030807      0.00087323
v  Velocity[Z]              1.5651           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5789           5.439          4.3406          4.3632
v  Pressure                -36.464          359.97           87.62          169.81
v  r11                   0.0010616        0.081879        0.013075        0.018286
v  r22                   0.0011144        0.082637        0.013355        0.018646
v  r33                   0.0016412          0.1743        0.027252        0.037207
v  r12                    -0.01067        0.013592     -0.00023383     -0.00030931
v  r13                   -0.045534        0.052805      9.3235e-05       0.0010138
v  r23                   -0.046709        0.051195      3.0526e-05       0.0005746
v  epsilon                0.069207           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9939e-05       0.0099175      0.00092508       0.0017427
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2771         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71351         0.85284


 TIME FOR THE TIME STEP            10732:        0.73191E+02

===============================================================


 INSTANT    0.107330000E-01   TIME STEP NUMBER           10733
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.541015851E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.308527160E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171832843E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.265273295E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.875404024E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81197E-03   0.44967E-02 0.19880E+01 
c  Velocity[X]                                      0.13772E-03 
c  Velocity[Y]                                      0.12779E-03 
c  Velocity[Z]                                      0.42312E-02 
c  Pressure     0.36539E-04     133   0.92964E-02   0.25773E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52741E-08   0.16312E-08 0.99098E-01 
c  r22          0.10852E-01      13   0.53156E-08   0.18232E-08 0.10105E+00 
c  r33          0.21860E-01      15   0.61759E-08   0.12465E-07 0.12647E+00 
c  r12          0.93867E-03      18   0.53218E-08   0.29527E-09 0.60458E+00 
c  r13          0.46676E-02      19   0.55188E-08   0.14941E-08 0.19873E+00 
c  r23          0.39978E-02      19   0.62865E-08   0.12848E-08 0.19823E+00 
c  epsilon      0.10969E+02      11   0.36290E-08   0.96909E-02 0.16482E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84237E-02 0.43294E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61366       0.0052576       0.0015077
v  Velocity[Y]            -0.57356         0.54411       0.0030807       0.0008732
v  Velocity[Z]               1.565           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5788           5.439          4.3406          4.3632
v  Pressure                -36.447          360.04           87.65          169.86
v  r11                   0.0010616        0.081876        0.013075        0.018286
v  r22                   0.0011144        0.082639        0.013355        0.018646
v  r33                   0.0016412         0.17428        0.027252        0.037207
v  r12                   -0.010665        0.013596     -0.00023383     -0.00030931
v  r13                   -0.045533        0.052805      9.3235e-05       0.0010138
v  r23                   -0.046709        0.051177      3.0526e-05       0.0005746
v  epsilon                0.069208          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9943e-05       0.0099175      0.00092508       0.0017427
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2766         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71352         0.85284


 TIME FOR THE TIME STEP            10733:        0.74572E+02

===============================================================


 INSTANT    0.107340000E-01   TIME STEP NUMBER           10734
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.129968050E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.770979252E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184395513E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.579133016E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.284805318E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81281E-03   0.45195E-02 0.19924E+01 
c  Velocity[X]                                      0.13802E-03 
c  Velocity[Y]                                      0.12901E-03 
c  Velocity[Z]                                      0.42525E-02 
c  Pressure     0.36277E-04     131   0.92323E-02   0.25587E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54847E-08   0.16566E-08 0.99664E-01 
c  r22          0.10852E-01      13   0.55828E-08   0.18144E-08 0.10081E+00 
c  r33          0.21860E-01      15   0.63330E-08   0.12634E-07 0.12729E+00 
c  r12          0.93867E-03      17   0.69619E-08   0.29444E-09 0.60381E+00 
c  r13          0.46676E-02      19   0.61651E-08   0.14993E-08 0.19968E+00 
c  r23          0.39978E-02      19   0.64397E-08   0.13076E-08 0.19986E+00 
c  epsilon      0.10969E+02      11   0.35211E-08   0.99408E-02 0.16571E+00 
c  TempC        0.25716E+06      16   0.15155E-04   0.84178E-02 0.43244E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61367       0.0052577       0.0015077
v  Velocity[Y]            -0.57343         0.54414       0.0030806      0.00087318
v  Velocity[Z]              1.5651           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5789           5.439          4.3406          4.3632
v  Pressure                -36.472             360          87.625          169.83
v  r11                   0.0010616        0.081874        0.013075        0.018286
v  r22                   0.0011145         0.08264        0.013355        0.018646
v  r33                   0.0016412         0.17424        0.027252        0.037207
v  r12                   -0.010661        0.013591     -0.00023383     -0.00030931
v  r13                   -0.045531        0.052806      9.3236e-05       0.0010138
v  r23                   -0.046708         0.05121      3.0527e-05       0.0005746
v  epsilon                0.069209          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099175      0.00092508       0.0017427
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2772         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71351         0.85283


 TIME FOR THE TIME STEP            10734:        0.73232E+02

===============================================================


 INSTANT    0.107350000E-01   TIME STEP NUMBER           10735
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.143067608E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.241037450E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934903E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.303623452E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.217576430E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.717525533E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11550E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15628E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81296E-03   0.45207E-02 0.19914E+01 
c  Velocity[X]                                      0.13792E-03 
c  Velocity[Y]                                      0.12815E-03 
c  Velocity[Z]                                      0.42546E-02 
c  Pressure     0.36188E-04     136   0.92151E-02   0.25525E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56853E-08   0.16908E-08 0.10110E+00 
c  r22          0.10852E-01      13   0.54679E-08   0.18516E-08 0.10176E+00 
c  r33          0.21860E-01      15   0.65561E-08   0.12849E-07 0.12887E+00 
c  r12          0.93867E-03      18   0.51547E-08   0.30288E-09 0.60690E+00 
c  r13          0.46676E-02      19   0.64790E-08   0.15159E-08 0.20056E+00 
c  r23          0.39978E-02      19   0.66855E-08   0.13269E-08 0.20296E+00 
c  epsilon      0.10969E+02      11   0.34300E-08   0.98445E-02 0.16499E+00 
c  TempC        0.25716E+06      16   0.15093E-04   0.84077E-02 0.43212E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63333         0.61368       0.0052576       0.0015077
v  Velocity[Y]            -0.57338         0.54426       0.0030807      0.00087321
v  Velocity[Z]              1.5649           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5787           5.439          4.3406          4.3632
v  Pressure                -36.414          360.05          87.649          169.86
v  r11                   0.0010616        0.081872        0.013075        0.018286
v  r22                   0.0011145         0.08264        0.013355        0.018646
v  r33                   0.0016412         0.17426        0.027252        0.037207
v  r12                   -0.010657        0.013589     -0.00023383     -0.00030931
v  r13                   -0.045533        0.052806      9.3236e-05       0.0010138
v  r23                   -0.046708          0.0512      3.0527e-05       0.0005746
v  epsilon                0.069209          271.14          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9951e-05       0.0099175      0.00092508       0.0017427
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2779         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71351         0.85284


 TIME FOR THE TIME STEP            10735:        0.74041E+02

===============================================================


 INSTANT    0.107360000E-01   TIME STEP NUMBER           10736
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.427907416E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155136007E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.290124688E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.739445345E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.262074668E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81249E-03   0.45139E-02 0.19916E+01 
c  Velocity[X]                                      0.13773E-03 
c  Velocity[Y]                                      0.12798E-03 
c  Velocity[Z]                                      0.42482E-02 
c  Pressure     0.36197E-04     132   0.92145E-02   0.25531E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57931E-08   0.16578E-08 0.99929E-01 
c  r22          0.10852E-01      13   0.53254E-08   0.18309E-08 0.10128E+00 
c  r33          0.21860E-01      15   0.61497E-08   0.12712E-07 0.12786E+00 
c  r12          0.93867E-03      18   0.51238E-08   0.29775E-09 0.60395E+00 
c  r13          0.46676E-02      19   0.64600E-08   0.15194E-08 0.20019E+00 
c  r23          0.39978E-02      19   0.60979E-08   0.13123E-08 0.20133E+00 
c  epsilon      0.10969E+02      11   0.35090E-08   0.10475E-01 0.17434E+00 
c  TempC        0.25716E+06      16   0.15188E-04   0.84317E-02 0.43361E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61364       0.0052576       0.0015076
v  Velocity[Y]            -0.57337         0.54439       0.0030806      0.00087318
v  Velocity[Z]              1.5651           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5789           5.439          4.3406          4.3632
v  Pressure                -36.459          359.94            87.6          169.78
v  r11                   0.0010616        0.081865        0.013075        0.018286
v  r22                   0.0011145        0.082639        0.013355        0.018646
v  r33                   0.0016413         0.17428        0.027252        0.037207
v  r12                   -0.010657        0.013584     -0.00023383     -0.00030931
v  r13                   -0.045531        0.052807      9.3236e-05       0.0010138
v  r23                   -0.046707        0.051193      3.0527e-05       0.0005746
v  epsilon                 0.06921          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9953e-05       0.0099175      0.00092508       0.0017427
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2777         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71351         0.85283


 TIME FOR THE TIME STEP            10736:        0.73627E+02

===============================================================


 INSTANT    0.107370000E-01   TIME STEP NUMBER           10737
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.158284504E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133555149E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.135720469E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237198687E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.705005512E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81129E-03   0.44931E-02 0.19849E+01 
c  Velocity[X]                                      0.13802E-03 
c  Velocity[Y]                                      0.12795E-03 
c  Velocity[Z]                                      0.42271E-02 
c  Pressure     0.35724E-04     131   0.90956E-02   0.25198E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61881E-08   0.16457E-08 0.99204E-01 
c  r22          0.10852E-01      13   0.49586E-08   0.18129E-08 0.10066E+00 
c  r33          0.21860E-01      15   0.65129E-08   0.12452E-07 0.12607E+00 
c  r12          0.93867E-03      18   0.54927E-08   0.29491E-09 0.60261E+00 
c  r13          0.46676E-02      20   0.59682E-08   0.14793E-08 0.19792E+00 
c  r23          0.39978E-02      19   0.64559E-08   0.12794E-08 0.19755E+00 
c  epsilon      0.10969E+02      11   0.34273E-08   0.98373E-02 0.16507E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.84392E-02 0.43390E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61368       0.0052576       0.0015077
v  Velocity[Y]            -0.57349         0.54421       0.0030807      0.00087323
v  Velocity[Z]              1.5651           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5788           5.439          4.3406          4.3632
v  Pressure                -36.411          360.02          87.638          169.85
v  r11                   0.0010616        0.081861        0.013075        0.018286
v  r22                   0.0011145        0.082636        0.013355        0.018646
v  r33                   0.0016413         0.17425        0.027252        0.037207
v  r12                   -0.010657        0.013586     -0.00023383     -0.00030931
v  r13                   -0.045532        0.052809      9.3236e-05       0.0010138
v  r23                   -0.046707        0.051218      3.0528e-05       0.0005746
v  epsilon                0.069211          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9955e-05       0.0099174      0.00092508       0.0017427
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71351         0.85284


 TIME FOR THE TIME STEP            10737:        0.71974E+02

===============================================================


 INSTANT    0.107380000E-01   TIME STEP NUMBER           10738
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.180335630E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.313895724E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.593530460E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.351349585E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.644499755E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81277E-03   0.45029E-02 0.19861E+01 
c  Velocity[X]                                      0.13745E-03 
c  Velocity[Y]                                      0.12833E-03 
c  Velocity[Z]                                      0.42371E-02 
c  Pressure     0.36410E-04     133   0.92668E-02   0.25681E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61883E-08   0.16480E-08 0.99348E-01 
c  r22          0.10852E-01      13   0.49364E-08   0.18575E-08 0.10113E+00 
c  r33          0.21860E-01      15   0.59848E-08   0.12661E-07 0.12674E+00 
c  r12          0.93867E-03      18   0.54356E-08   0.30377E-09 0.60608E+00 
c  r13          0.46676E-02      19   0.66856E-08   0.15101E-08 0.19912E+00 
c  r23          0.39978E-02      19   0.54236E-08   0.12860E-08 0.19879E+00 
c  epsilon      0.10969E+02      11   0.32284E-08   0.99852E-02 0.16463E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.83635E-02 0.43108E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61367       0.0052576       0.0015077
v  Velocity[Y]            -0.57352         0.54435       0.0030806       0.0008732
v  Velocity[Z]               1.565           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5789           5.439          4.3406          4.3632
v  Pressure                -36.475          359.98          87.623          169.82
v  r11                   0.0010616        0.081859        0.013075        0.018286
v  r22                   0.0011145        0.082637        0.013355        0.018646
v  r33                   0.0016413         0.17422        0.027252        0.037207
v  r12                    -0.01066        0.013584     -0.00023383     -0.00030931
v  r13                   -0.045534         0.05281      9.3236e-05       0.0010138
v  r23                   -0.046707        0.051213      3.0528e-05       0.0005746
v  epsilon                0.069212          271.13          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9957e-05       0.0099174      0.00092508       0.0017427
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017851           5.279         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71351         0.85284


 TIME FOR THE TIME STEP            10738:        0.72327E+02

===============================================================


 INSTANT    0.107390000E-01   TIME STEP NUMBER           10739
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.330809707E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.204521138E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.311760253E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.382591848E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.442329511E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81258E-03   0.45245E-02 0.19932E+01 
c  Velocity[X]                                      0.13837E-03 
c  Velocity[Y]                                      0.12745E-03 
c  Velocity[Z]                                      0.42587E-02 
c  Pressure     0.36593E-04     132   0.93219E-02   0.25811E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60329E-08   0.16578E-08 0.99138E-01 
c  r22          0.10852E-01      13   0.53226E-08   0.18169E-08 0.10061E+00 
c  r33          0.21860E-01      15   0.53728E-08   0.12582E-07 0.12639E+00 
c  r12          0.93867E-03      18   0.55455E-08   0.29646E-09 0.60285E+00 
c  r13          0.46676E-02      19   0.64988E-08   0.15005E-08 0.19817E+00 
c  r23          0.39978E-02      19   0.53089E-08   0.12920E-08 0.19786E+00 
c  epsilon      0.10969E+02      11   0.32492E-08   0.10101E-01 0.16579E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.84378E-02 0.43284E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61367       0.0052576       0.0015077
v  Velocity[Y]            -0.57358         0.54405       0.0030806      0.00087318
v  Velocity[Z]              1.5652           5.439          4.3387          4.3625
v  ǁVelocityǁ                1.579           5.439          4.3406          4.3632
v  Pressure                -36.425          359.99          87.642          169.84
v  r11                   0.0010616        0.081858        0.013075        0.018286
v  r22                   0.0011145        0.082637        0.013355        0.018646
v  r33                   0.0016413         0.17423        0.027252        0.037207
v  r12                   -0.010662        0.013579     -0.00023383     -0.00030931
v  r13                   -0.045532        0.052806      9.3236e-05       0.0010138
v  r23                   -0.046707        0.051203      3.0527e-05       0.0005746
v  epsilon                0.069212          271.14          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099175      0.00092508       0.0017427
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017851           5.279         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71351         0.85283


 TIME FOR THE TIME STEP            10739:        0.73256E+02

===============================================================


 INSTANT    0.107400000E-01   TIME STEP NUMBER           10740
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237257726E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.108361622E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.970084104E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.134998600E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.407372095E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81260E-03   0.45232E-02 0.19907E+01 
c  Velocity[X]                                      0.13791E-03 
c  Velocity[Y]                                      0.12743E-03 
c  Velocity[Z]                                      0.42578E-02 
c  Pressure     0.36123E-04     131   0.91962E-02   0.25479E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60118E-08   0.16293E-08 0.98830E-01 
c  r22          0.10852E-01      13   0.51954E-08   0.18251E-08 0.10089E+00 
c  r33          0.21860E-01      15   0.53071E-08   0.12498E-07 0.12653E+00 
c  r12          0.93867E-03      18   0.56316E-08   0.29955E-09 0.60357E+00 
c  r13          0.46676E-02      19   0.65318E-08   0.14935E-08 0.19867E+00 
c  r23          0.39978E-02      19   0.53413E-08   0.12749E-08 0.19761E+00 
c  epsilon      0.10969E+02      11   0.33036E-08   0.99936E-02 0.16569E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.83986E-02 0.43273E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61367       0.0052576       0.0015077
v  Velocity[Y]            -0.57348         0.54409       0.0030806      0.00087318
v  Velocity[Z]              1.5654           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5792           5.439          4.3406          4.3632
v  Pressure                -36.474          359.98          87.625          169.82
v  r11                   0.0010616        0.081859        0.013075        0.018286
v  r22                   0.0011145        0.082638        0.013355        0.018646
v  r33                   0.0016413         0.17423        0.027252        0.037207
v  r12                   -0.010666        0.013577     -0.00023383     -0.00030931
v  r13                    -0.04553        0.052807      9.3236e-05       0.0010138
v  r23                   -0.046708         0.05122      3.0528e-05       0.0005746
v  epsilon                0.069213          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099174      0.00092508       0.0017427
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            10740:        0.75306E+02

===============================================================


 INSTANT    0.107410000E-01   TIME STEP NUMBER           10741
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.180980458E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.378029233E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.408453102E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.303774082E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285754568E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81269E-03   0.44887E-02 0.19840E+01 
c  Velocity[X]                                      0.13757E-03 
c  Velocity[Y]                                      0.12836E-03 
c  Velocity[Z]                                      0.42228E-02 
c  Pressure     0.36211E-04     132   0.92205E-02   0.25540E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60166E-08   0.16302E-08 0.98959E-01 
c  r22          0.10852E-01      13   0.51865E-08   0.18232E-08 0.10088E+00 
c  r33          0.21860E-01      15   0.59432E-08   0.12414E-07 0.12621E+00 
c  r12          0.93867E-03      18   0.52377E-08   0.29208E-09 0.59964E+00 
c  r13          0.46676E-02      20   0.57243E-08   0.14810E-08 0.19835E+00 
c  r23          0.39978E-02      19   0.53181E-08   0.12772E-08 0.19800E+00 
c  epsilon      0.10969E+02      11   0.34261E-08   0.97685E-02 0.16350E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.83202E-02 0.43075E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61367       0.0052576       0.0015077
v  Velocity[Y]            -0.57355         0.54427       0.0030807       0.0008732
v  Velocity[Z]              1.5653           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5791           5.439          4.3406          4.3632
v  Pressure                 -36.43          360.09          87.678          169.91
v  r11                   0.0010616        0.081861        0.013075        0.018286
v  r22                   0.0011145        0.082638        0.013355        0.018646
v  r33                   0.0016414         0.17421        0.027252        0.037207
v  r12                   -0.010669        0.013584     -0.00023383     -0.00030931
v  r13                   -0.045534        0.052805      9.3237e-05       0.0010138
v  r23                   -0.046709        0.051211      3.0529e-05       0.0005746
v  epsilon                0.069213          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9962e-05       0.0099174      0.00092508       0.0017427
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71351         0.85283


 TIME FOR THE TIME STEP            10741:        0.71925E+02

===============================================================


 INSTANT    0.107420000E-01   TIME STEP NUMBER           10742
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.499064412E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154550530E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.222316903E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.143777179E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.373249403E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81203E-03   0.45088E-02 0.19902E+01 
c  Velocity[X]                                      0.13882E-03 
c  Velocity[Y]                                      0.12916E-03 
c  Velocity[Z]                                      0.42408E-02 
c  Pressure     0.36033E-04     132   0.91758E-02   0.25415E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61446E-08   0.16392E-08 0.99645E-01 
c  r22          0.10852E-01      13   0.48203E-08   0.17965E-08 0.10075E+00 
c  r33          0.21860E-01      15   0.63365E-08   0.12390E-07 0.12717E+00 
c  r12          0.93867E-03      18   0.53160E-08   0.29679E-09 0.60463E+00 
c  r13          0.46676E-02      19   0.70810E-08   0.14780E-08 0.19938E+00 
c  r23          0.39978E-02      19   0.54487E-08   0.12951E-08 0.20091E+00 
c  epsilon      0.10969E+02      11   0.33501E-08   0.97659E-02 0.16865E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84734E-02 0.43462E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61362       0.0052576       0.0015076
v  Velocity[Y]            -0.57347         0.54439       0.0030806      0.00087314
v  Velocity[Z]              1.5652           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5791           5.439          4.3406          4.3632
v  Pressure                -36.443          359.95          87.617           169.8
v  r11                   0.0010616        0.081862        0.013075        0.018286
v  r22                   0.0011145        0.082638        0.013355        0.018646
v  r33                   0.0016414         0.17421        0.027252        0.037207
v  r12                    -0.01067        0.013582     -0.00023383     -0.00030931
v  r13                   -0.045531        0.052806      9.3237e-05       0.0010138
v  r23                    -0.04671        0.051193      3.0528e-05       0.0005746
v  epsilon                0.069214          271.13          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9965e-05       0.0099176      0.00092508       0.0017427
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2782         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71351         0.85283


 TIME FOR THE TIME STEP            10742:        0.71950E+02

===============================================================


 INSTANT    0.107430000E-01   TIME STEP NUMBER           10743
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.219615625E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.111355140E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.821594532E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117740264E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.436527300E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81239E-03   0.45159E-02 0.19901E+01 
c  Velocity[X]                                      0.13866E-03 
c  Velocity[Y]                                      0.12829E-03 
c  Velocity[Z]                                      0.42489E-02 
c  Pressure     0.36339E-04     131   0.92528E-02   0.25631E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.62037E-08   0.16577E-08 0.99643E-01 
c  r22          0.10852E-01      13   0.52839E-08   0.18402E-08 0.10153E+00 
c  r33          0.21860E-01      15   0.57803E-08   0.12640E-07 0.12760E+00 
c  r12          0.93867E-03      18   0.52975E-08   0.31177E-09 0.61475E+00 
c  r13          0.46676E-02      19   0.70896E-08   0.14967E-08 0.20031E+00 
c  r23          0.39978E-02      19   0.55076E-08   0.12884E-08 0.19927E+00 
c  epsilon      0.10969E+02      11   0.31941E-08   0.99162E-02 0.16491E+00 
c  TempC        0.25716E+06      16   0.15096E-04   0.84784E-02 0.43402E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61365       0.0052577       0.0015077
v  Velocity[Y]            -0.57354         0.54425       0.0030807       0.0008732
v  Velocity[Z]               1.565           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5788           5.439          4.3406          4.3632
v  Pressure                -36.414          360.05           87.67          169.88
v  r11                   0.0010616        0.081858        0.013075        0.018286
v  r22                   0.0011145        0.082632        0.013355        0.018646
v  r33                   0.0016414         0.17422        0.027252        0.037207
v  r12                   -0.010669         0.01358     -0.00023383     -0.00030931
v  r13                   -0.045531        0.052804      9.3237e-05       0.0010138
v  r23                   -0.046711        0.051216      3.0528e-05       0.0005746
v  epsilon                0.069215          271.13          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9967e-05       0.0099176      0.00092509       0.0017427
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2787         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71351         0.85284


 TIME FOR THE TIME STEP            10743:        0.75522E+02

===============================================================


 INSTANT    0.107440000E-01   TIME STEP NUMBER           10744
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133125840E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.224828830E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.144117462E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.656815425E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.849455272E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81312E-03   0.45152E-02 0.19913E+01 
c  Velocity[X]                                      0.13778E-03 
c  Velocity[Y]                                      0.12813E-03 
c  Velocity[Z]                                      0.42493E-02 
c  Pressure     0.36407E-04     133   0.92656E-02   0.25679E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61302E-08   0.16443E-08 0.99046E-01 
c  r22          0.10852E-01      13   0.46168E-08   0.18542E-08 0.10125E+00 
c  r33          0.21860E-01      15   0.57477E-08   0.12736E-07 0.12733E+00 
c  r12          0.93867E-03      18   0.55669E-08   0.30500E-09 0.60869E+00 
c  r13          0.46676E-02      19   0.70199E-08   0.15109E-08 0.19987E+00 
c  r23          0.39978E-02      19   0.56617E-08   0.12944E-08 0.19958E+00 
c  epsilon      0.10969E+02      11   0.32556E-08   0.10209E-01 0.16648E+00 
c  TempC        0.25716E+06      16   0.15188E-04   0.84154E-02 0.43264E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61366       0.0052576       0.0015076
v  Velocity[Y]            -0.57362         0.54417       0.0030807      0.00087318
v  Velocity[Z]              1.5653           5.439          4.3387          4.3625
v  ǁVelocityǁ                1.579           5.439          4.3406          4.3632
v  Pressure                 -36.47          360.01           87.62          169.83
v  r11                   0.0010616        0.081857        0.013075        0.018286
v  r22                   0.0011145        0.082632        0.013355        0.018646
v  r33                   0.0016414         0.17422        0.027252        0.037207
v  r12                   -0.010669        0.013583     -0.00023383     -0.00030931
v  r13                   -0.045533        0.052803      9.3238e-05       0.0010138
v  r23                   -0.046712        0.051209      3.0529e-05       0.0005746
v  epsilon                0.069216          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9967e-05       0.0099176      0.00092509       0.0017427
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017851           5.279         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71351         0.85284


 TIME FOR THE TIME STEP            10744:        0.74550E+02

===============================================================


 INSTANT    0.107450000E-01   TIME STEP NUMBER           10745
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.277885997E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.394008724E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934913E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.667992951E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.675420941E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.339216004E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81185E-03   0.45034E-02 0.19900E+01 
c  Velocity[X]                                      0.13798E-03 
c  Velocity[Y]                                      0.12795E-03 
c  Velocity[Z]                                      0.42375E-02 
c  Pressure     0.36204E-04     133   0.92227E-02   0.25537E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.64401E-08   0.16188E-08 0.98519E-01 
c  r22          0.10852E-01      12   0.65967E-08   0.18115E-08 0.10077E+00 
c  r33          0.21860E-01      15   0.52249E-08   0.12420E-07 0.12624E+00 
c  r12          0.93867E-03      18   0.54861E-08   0.29984E-09 0.60453E+00 
c  r13          0.46676E-02      19   0.63876E-08   0.14884E-08 0.19819E+00 
c  r23          0.39978E-02      19   0.52674E-08   0.12676E-08 0.19678E+00 
c  epsilon      0.10969E+02      11   0.33277E-08   0.98551E-02 0.16406E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.84050E-02 0.43184E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61363       0.0052576       0.0015076
v  Velocity[Y]            -0.57367         0.54422       0.0030806      0.00087317
v  Velocity[Z]              1.5654           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5791           5.439          4.3406          4.3632
v  Pressure                -36.419          360.08          87.682           169.9
v  r11                   0.0010616        0.081853        0.013075        0.018286
v  r22                   0.0011146        0.082632        0.013355        0.018646
v  r33                   0.0016414         0.17422        0.027252        0.037207
v  r12                   -0.010669        0.013586     -0.00023383     -0.00030931
v  r13                   -0.045532        0.052803      9.3237e-05       0.0010138
v  r23                   -0.046712        0.051197      3.0529e-05       0.0005746
v  epsilon                0.069216          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9968e-05       0.0099177      0.00092509       0.0017427
v  CourantNb               0.44218             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2791         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71351         0.85283


 TIME FOR THE TIME STEP            10745:        0.75693E+02

===============================================================


 INSTANT    0.107460000E-01   TIME STEP NUMBER           10746
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.149339582E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.206324440E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.672652658E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.846441946E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166688866E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81280E-03   0.45197E-02 0.19914E+01 
c  Velocity[X]                                      0.13802E-03 
c  Velocity[Y]                                      0.12780E-03 
c  Velocity[Z]                                      0.42539E-02 
c  Pressure     0.36269E-04     131   0.92356E-02   0.25583E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60978E-08   0.16510E-08 0.99228E-01 
c  r22          0.10852E-01      13   0.48055E-08   0.18213E-08 0.10071E+00 
c  r33          0.21860E-01      15   0.53190E-08   0.12612E-07 0.12682E+00 
c  r12          0.93867E-03      18   0.49663E-08   0.29930E-09 0.60424E+00 
c  r13          0.46676E-02      19   0.73152E-08   0.14938E-08 0.19871E+00 
c  r23          0.39978E-02      19   0.62182E-08   0.12889E-08 0.19845E+00 
c  epsilon      0.10969E+02      11   0.33828E-08   0.10116E-01 0.16611E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.84151E-02 0.43318E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61364       0.0052577       0.0015076
v  Velocity[Y]            -0.57363         0.54436       0.0030806      0.00087319
v  Velocity[Z]              1.5653           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5791           5.439          4.3406          4.3632
v  Pressure                -36.421          359.96          87.628          169.81
v  r11                   0.0010616        0.081859        0.013075        0.018286
v  r22                   0.0011146        0.082632        0.013355        0.018646
v  r33                   0.0016414         0.17422        0.027252        0.037207
v  r12                    -0.01067        0.013589     -0.00023383     -0.00030931
v  r13                    -0.04553        0.052802      9.3237e-05       0.0010138
v  r23                   -0.046713        0.051214       3.053e-05       0.0005746
v  epsilon                0.069217          271.13          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9967e-05       0.0099176      0.00092509       0.0017427
v  CourantNb               0.44214             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2792         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8792         0.71352         0.85284


 TIME FOR THE TIME STEP            10746:        0.73547E+02

===============================================================


 INSTANT    0.107470000E-01   TIME STEP NUMBER           10747
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.218610544E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.444413615E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.222700768E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111604460E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.423047582E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81253E-03   0.44827E-02 0.19821E+01 
c  Velocity[X]                                      0.13761E-03 
c  Velocity[Y]                                      0.12739E-03 
c  Velocity[Z]                                      0.42177E-02 
c  Pressure     0.35743E-04     132   0.91008E-02   0.25210E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61687E-08   0.16398E-08 0.99102E-01 
c  r22          0.10852E-01      13   0.47985E-08   0.18097E-08 0.10067E+00 
c  r33          0.21860E-01      15   0.52330E-08   0.12500E-07 0.12700E+00 
c  r12          0.93867E-03      18   0.55291E-08   0.30134E-09 0.60544E+00 
c  r13          0.46676E-02      19   0.67850E-08   0.14973E-08 0.19934E+00 
c  r23          0.39978E-02      19   0.60599E-08   0.13033E-08 0.20032E+00 
c  epsilon      0.10969E+02      11   0.32245E-08   0.99958E-02 0.16826E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.83963E-02 0.43234E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61368       0.0052576       0.0015076
v  Velocity[Y]            -0.57377         0.54419       0.0030807       0.0008732
v  Velocity[Z]              1.5652           5.439          4.3387          4.3625
v  ǁVelocityǁ                1.579           5.439          4.3406          4.3632
v  Pressure                 -36.38          360.04           87.66          169.88
v  r11                   0.0010616        0.081856        0.013075        0.018286
v  r22                   0.0011146        0.082632        0.013355        0.018646
v  r33                   0.0016415         0.17422        0.027252        0.037207
v  r12                   -0.010667        0.013599     -0.00023383     -0.00030931
v  r13                   -0.045533          0.0528      9.3237e-05       0.0010138
v  r23                   -0.046713        0.051202      3.0531e-05       0.0005746
v  epsilon                0.069218          271.14          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9967e-05       0.0099176      0.00092509       0.0017427
v  CourantNb               0.44219             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2792         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8792         0.71352         0.85284


 TIME FOR THE TIME STEP            10747:        0.75409E+02

===============================================================


 INSTANT    0.107480000E-01   TIME STEP NUMBER           10748
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.818126638E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.545328595E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.231922698E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.476022084E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.445802677E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81261E-03   0.44787E-02 0.19816E+01 
c  Velocity[X]                                      0.13760E-03 
c  Velocity[Y]                                      0.12765E-03 
c  Velocity[Z]                                      0.42135E-02 
c  Pressure     0.36629E-04     131   0.93256E-02   0.25835E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59400E-08   0.16044E-08 0.98258E-01 
c  r22          0.10852E-01      13   0.46080E-08   0.18066E-08 0.10071E+00 
c  r33          0.21860E-01      14   0.70423E-08   0.12250E-07 0.12577E+00 
c  r12          0.93868E-03      18   0.70924E-08   0.29195E-09 0.60017E+00 
c  r13          0.46676E-02      19   0.58112E-08   0.14677E-08 0.19807E+00 
c  r23          0.39978E-02      19   0.55221E-08   0.12561E-08 0.19642E+00 
c  epsilon      0.10969E+02      11   0.31953E-08   0.96484E-02 0.16463E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.84148E-02 0.43313E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61364       0.0052575       0.0015076
v  Velocity[Y]            -0.57372         0.54428       0.0030807      0.00087321
v  Velocity[Z]              1.5652           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5791           5.439          4.3406          4.3632
v  Pressure                -36.442          360.03          87.662          169.86
v  r11                   0.0010616        0.081857        0.013075        0.018286
v  r22                   0.0011146         0.08263        0.013355        0.018646
v  r33                   0.0016415         0.17422        0.027252        0.037207
v  r12                   -0.010669        0.013597     -0.00023383     -0.00030931
v  r13                   -0.045531          0.0528      9.3238e-05       0.0010138
v  r23                   -0.046714        0.051196      3.0531e-05       0.0005746
v  epsilon                0.069218          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9966e-05       0.0099176      0.00092509       0.0017427
v  CourantNb               0.44216             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2796         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8796         0.71351         0.85284


 TIME FOR THE TIME STEP            10748:        0.73843E+02

===============================================================


 INSTANT    0.107490000E-01   TIME STEP NUMBER           10749
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.303616589E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.314118587E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.291154995E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935015E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.170906302E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.456562973E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81210E-03   0.45538E-02 0.19960E+01 
c  Velocity[X]                                      0.13848E-03 
c  Velocity[Y]                                      0.12925E-03 
c  Velocity[Z]                                      0.42860E-02 
c  Pressure     0.36367E-04     132   0.92524E-02   0.25652E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.62020E-08   0.16339E-08 0.99239E-01 
c  r22          0.10852E-01      13   0.48229E-08   0.18017E-08 0.10052E+00 
c  r33          0.21860E-01      15   0.53645E-08   0.12383E-07 0.12618E+00 
c  r12          0.93868E-03      18   0.60696E-08   0.29112E-09 0.60098E+00 
c  r13          0.46676E-02      19   0.65302E-08   0.14962E-08 0.19874E+00 
c  r23          0.39978E-02      19   0.59092E-08   0.12799E-08 0.19787E+00 
c  epsilon      0.10969E+02      11   0.32659E-08   0.96413E-02 0.16272E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.84433E-02 0.43343E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61366       0.0052575       0.0015076
v  Velocity[Y]            -0.57379         0.54441       0.0030806      0.00087322
v  Velocity[Z]               1.565           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5789           5.439          4.3406          4.3632
v  Pressure                -36.384          360.02          87.628          169.84
v  r11                   0.0010616        0.081854        0.013075        0.018286
v  r22                   0.0011146         0.08263        0.013355        0.018646
v  r33                   0.0016415         0.17423        0.027252        0.037207
v  r12                   -0.010671        0.013599     -0.00023383     -0.00030931
v  r13                   -0.045532          0.0528      9.3238e-05       0.0010138
v  r23                   -0.046714         0.05122      3.0531e-05       0.0005746
v  epsilon                0.069219          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9965e-05       0.0099177      0.00092509       0.0017427
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2795         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8795         0.71351         0.85284


 TIME FOR THE TIME STEP            10749:        0.72787E+02

===============================================================


 INSTANT    0.107500000E-01   TIME STEP NUMBER           10750
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.386893099E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.330883294E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.127297730E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.156289232E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.854337082E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81380E-03   0.45386E-02 0.19961E+01 
c  Velocity[X]                                      0.13844E-03 
c  Velocity[Y]                                      0.12854E-03 
c  Velocity[Z]                                      0.42716E-02 
c  Pressure     0.36359E-04     134   0.92563E-02   0.25646E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.62380E-08   0.16178E-08 0.99065E-01 
c  r22          0.10852E-01      13   0.48535E-08   0.18312E-08 0.10115E+00 
c  r33          0.21860E-01      14   0.68365E-08   0.12554E-07 0.12725E+00 
c  r12          0.93868E-03      18   0.65700E-08   0.28988E-09 0.60141E+00 
c  r13          0.46676E-02      19   0.60316E-08   0.14969E-08 0.19996E+00 
c  r23          0.39978E-02      19   0.54209E-08   0.12744E-08 0.19833E+00 
c  epsilon      0.10969E+02      11   0.33341E-08   0.10124E-01 0.16796E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.83638E-02 0.43105E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61367       0.0052575       0.0015076
v  Velocity[Y]            -0.57358         0.54406       0.0030807      0.00087321
v  Velocity[Z]              1.5653           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5791           5.439          4.3406          4.3632
v  Pressure                -36.414          360.04          87.669          169.87
v  r11                   0.0010616        0.081855        0.013075        0.018286
v  r22                   0.0011146        0.082626        0.013355        0.018646
v  r33                   0.0016415         0.17423        0.027252        0.037207
v  r12                   -0.010672        0.013597     -0.00023383     -0.00030931
v  r13                   -0.045534        0.052804      9.3239e-05       0.0010138
v  r23                   -0.046714        0.051205      3.0531e-05       0.0005746
v  epsilon                 0.06922          271.14          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9966e-05       0.0099177      0.00092509       0.0017427
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2794         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8794         0.71351         0.85283


 TIME FOR THE TIME STEP            10750:        0.73886E+02

===============================================================


 INSTANT    0.107510000E-01   TIME STEP NUMBER           10751
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.458001586E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157861168E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.201424277E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.159449803E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.139904084E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81248E-03   0.45165E-02 0.19922E+01 
c  Velocity[X]                                      0.13861E-03 
c  Velocity[Y]                                      0.12832E-03 
c  Velocity[Z]                                      0.42496E-02 
c  Pressure     0.36112E-04     132   0.91978E-02   0.25473E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61714E-08   0.16187E-08 0.98708E-01 
c  r22          0.10852E-01      13   0.48712E-08   0.18112E-08 0.10082E+00 
c  r33          0.21860E-01      15   0.54236E-08   0.12421E-07 0.12634E+00 
c  r12          0.93868E-03      18   0.60431E-08   0.29669E-09 0.60471E+00 
c  r13          0.46676E-02      19   0.64151E-08   0.14855E-08 0.19903E+00 
c  r23          0.39978E-02      19   0.64741E-08   0.12749E-08 0.19758E+00 
c  epsilon      0.10969E+02      11   0.34167E-08   0.98600E-02 0.16499E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.83853E-02 0.43188E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61364       0.0052577       0.0015076
v  Velocity[Y]            -0.57361         0.54406       0.0030807      0.00087325
v  Velocity[Z]               1.565           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5788           5.439          4.3406          4.3632
v  Pressure                -36.391          359.98          87.627          169.82
v  r11                   0.0010617        0.081857        0.013075        0.018286
v  r22                   0.0011146        0.082627        0.013355        0.018646
v  r33                   0.0016415         0.17423        0.027252        0.037207
v  r12                   -0.010668          0.0136     -0.00023383     -0.00030931
v  r13                   -0.045531        0.052803      9.3239e-05       0.0010138
v  r23                   -0.046714        0.051187      3.0532e-05       0.0005746
v  epsilon                0.069221          271.14          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9965e-05       0.0099177      0.00092509       0.0017427
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017851          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71351         0.85283


 TIME FOR THE TIME STEP            10751:        0.72835E+02

===============================================================


 INSTANT    0.107520000E-01   TIME STEP NUMBER           10752
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.245608674E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.221776220E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.422533805E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.995385302E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.226987488E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81283E-03   0.44891E-02 0.19835E+01 
c  Velocity[X]                                      0.13732E-03 
c  Velocity[Y]                                      0.12788E-03 
c  Velocity[Z]                                      0.42239E-02 
c  Pressure     0.36242E-04     133   0.92223E-02   0.25563E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.66074E-08   0.16354E-08 0.99001E-01 
c  r22          0.10852E-01      13   0.50717E-08   0.18481E-08 0.10116E+00 
c  r33          0.21860E-01      15   0.58641E-08   0.12663E-07 0.12680E+00 
c  r12          0.93868E-03      18   0.51408E-08   0.30094E-09 0.60865E+00 
c  r13          0.46676E-02      19   0.69737E-08   0.15375E-08 0.19992E+00 
c  r23          0.39978E-02      19   0.62938E-08   0.13021E-08 0.19918E+00 
c  epsilon      0.10969E+02      11   0.33499E-08   0.10220E-01 0.16668E+00 
c  TempC        0.25716E+06      16   0.15173E-04   0.84148E-02 0.43365E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61363       0.0052576       0.0015076
v  Velocity[Y]            -0.57351         0.54422       0.0030807      0.00087325
v  Velocity[Z]              1.5652           5.439          4.3387          4.3625
v  ǁVelocityǁ                1.579           5.439          4.3406          4.3632
v  Pressure                -36.433          359.99          87.636          169.82
v  r11                   0.0010617        0.081852        0.013075        0.018286
v  r22                   0.0011146        0.082628        0.013355        0.018646
v  r33                   0.0016415         0.17423        0.027252        0.037207
v  r12                   -0.010666        0.013597     -0.00023383     -0.00030931
v  r13                   -0.045529        0.052802      9.3239e-05       0.0010138
v  r23                   -0.046714        0.051172      3.0532e-05       0.0005746
v  epsilon                0.069221          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9962e-05       0.0099176      0.00092509       0.0017427
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2784         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85284


 TIME FOR THE TIME STEP            10752:        0.71395E+02

===============================================================


 INSTANT    0.107530000E-01   TIME STEP NUMBER           10753
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.396323781E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157228455E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.774484638E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.970464344E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173039468E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81226E-03   0.44975E-02 0.19882E+01 
c  Velocity[X]                                      0.13809E-03 
c  Velocity[Y]                                      0.12777E-03 
c  Velocity[Z]                                      0.42316E-02 
c  Pressure     0.36683E-04     133   0.93383E-02   0.25875E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.68944E-08   0.16305E-08 0.99380E-01 
c  r22          0.10852E-01      13   0.54106E-08   0.18246E-08 0.10125E+00 
c  r33          0.21860E-01      15   0.58968E-08   0.12565E-07 0.12747E+00 
c  r12          0.93868E-03      18   0.52444E-08   0.29910E-09 0.60837E+00 
c  r13          0.46676E-02      19   0.73493E-08   0.15090E-08 0.19998E+00 
c  r23          0.39978E-02      19   0.71420E-08   0.13033E-08 0.20081E+00 
c  epsilon      0.10969E+02      11   0.33565E-08   0.10052E-01 0.16949E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.83803E-02 0.43193E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63335         0.61364       0.0052575       0.0015076
v  Velocity[Y]            -0.57348         0.54433       0.0030807      0.00087326
v  Velocity[Z]              1.5651           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5789           5.439          4.3406          4.3632
v  Pressure                  -36.4          360.11          87.691          169.92
v  r11                   0.0010617        0.081843        0.013075        0.018286
v  r22                   0.0011146         0.08263        0.013355        0.018646
v  r33                   0.0016416         0.17423        0.027252        0.037207
v  r12                   -0.010662        0.013591     -0.00023383     -0.00030931
v  r13                   -0.045534        0.052801      9.3239e-05       0.0010138
v  r23                   -0.046714        0.051198      3.0532e-05       0.0005746
v  epsilon                0.069222          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9962e-05       0.0099176      0.00092509       0.0017427
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2778         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71351         0.85283


 TIME FOR THE TIME STEP            10753:        0.72015E+02

===============================================================


 INSTANT    0.107540000E-01   TIME STEP NUMBER           10754
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.374695913E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.858197946E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.525617815E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.408795598E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.490488802E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81267E-03   0.45401E-02 0.19973E+01 
c  Velocity[X]                                      0.13800E-03 
c  Velocity[Y]                                      0.12854E-03 
c  Velocity[Z]                                      0.42736E-02 
c  Pressure     0.36248E-04     133   0.92257E-02   0.25568E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.69205E-08   0.16118E-08 0.98608E-01 
c  r22          0.10852E-01      13   0.46001E-08   0.18077E-08 0.10072E+00 
c  r33          0.21860E-01      15   0.59541E-08   0.12348E-07 0.12621E+00 
c  r12          0.93868E-03      18   0.52305E-08   0.29310E-09 0.60348E+00 
c  r13          0.46676E-02      20   0.57152E-08   0.14776E-08 0.19878E+00 
c  r23          0.39978E-02      19   0.65070E-08   0.12638E-08 0.19733E+00 
c  epsilon      0.10969E+02      11   0.32667E-08   0.96455E-02 0.16274E+00 
c  TempC        0.25716E+06      16   0.15155E-04   0.84368E-02 0.43249E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61361       0.0052575       0.0015076
v  Velocity[Y]            -0.57355         0.54411       0.0030807      0.00087324
v  Velocity[Z]              1.5651           5.439          4.3387          4.3625
v  ǁVelocityǁ               1.5789           5.439          4.3406          4.3632
v  Pressure                 -36.41             360          87.643          169.84
v  r11                   0.0010617        0.081845        0.013075        0.018286
v  r22                   0.0011146        0.082631        0.013355        0.018646
v  r33                   0.0016416         0.17422        0.027252        0.037207
v  r12                   -0.010659        0.013589     -0.00023383     -0.00030931
v  r13                   -0.045531        0.052803      9.3239e-05       0.0010138
v  r23                   -0.046713        0.051196      3.0532e-05       0.0005746
v  epsilon                0.069223          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099176      0.00092509       0.0017427
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2769         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71351         0.85284


 TIME FOR THE TIME STEP            10754:        0.70540E+02

===============================================================


 INSTANT    0.107550000E-01   TIME STEP NUMBER           10755
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.556002477E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.207921874E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.660322050E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153379448E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.174265103E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81254E-03   0.45084E-02 0.19869E+01 
c  Velocity[X]                                      0.13783E-03 
c  Velocity[Y]                                      0.12865E-03 
c  Velocity[Z]                                      0.42419E-02 
c  Pressure     0.36220E-04     131   0.92170E-02   0.25548E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.67141E-08   0.16056E-08 0.98450E-01 
c  r22          0.10852E-01      13   0.50594E-08   0.18078E-08 0.10080E+00 
c  r33          0.21860E-01      16   0.58632E-08   0.12394E-07 0.12649E+00 
c  r12          0.93868E-03      18   0.50980E-08   0.29741E-09 0.60547E+00 
c  r13          0.46676E-02      20   0.65153E-08   0.14962E-08 0.19963E+00 
c  r23          0.39978E-02      19   0.67817E-08   0.12715E-08 0.19770E+00 
c  epsilon      0.10969E+02      11   0.35302E-08   0.96710E-02 0.16309E+00 
c  TempC        0.25716E+06      16   0.15120E-04   0.84541E-02 0.43361E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61364       0.0052576       0.0015076
v  Velocity[Y]            -0.57361         0.54426       0.0030808      0.00087329
v  Velocity[Z]              1.5653          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4391          4.3406          4.3632
v  Pressure                -36.351          360.04          87.652          169.86
v  r11                   0.0010617        0.081847        0.013075        0.018286
v  r22                   0.0011147        0.082631        0.013355        0.018646
v  r33                   0.0016416         0.17423        0.027252        0.037207
v  r12                   -0.010662        0.013583     -0.00023383     -0.00030931
v  r13                    -0.04553        0.052801       9.324e-05       0.0010138
v  r23                   -0.046714        0.051185      3.0533e-05       0.0005746
v  epsilon                0.069223          271.14          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9958e-05       0.0099176       0.0009251       0.0017427
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2769         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71351         0.85284


 TIME FOR THE TIME STEP            10755:        0.70210E+02

===============================================================


 INSTANT    0.107560000E-01   TIME STEP NUMBER           10756
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203779409E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.237548769E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.412276414E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106563284E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123356946E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81321E-03   0.44866E-02 0.19849E+01 
c  Velocity[X]                                      0.13729E-03 
c  Velocity[Y]                                      0.12766E-03 
c  Velocity[Z]                                      0.42216E-02 
c  Pressure     0.36233E-04     133   0.92298E-02   0.25556E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.68397E-08   0.16524E-08 0.99385E-01 
c  r22          0.10852E-01      13   0.53062E-08   0.18425E-08 0.10132E+00 
c  r33          0.21860E-01      15   0.73011E-08   0.12759E-07 0.12773E+00 
c  r12          0.93868E-03      18   0.61194E-08   0.29640E-09 0.60356E+00 
c  r13          0.46676E-02      20   0.66204E-08   0.15065E-08 0.20018E+00 
c  r23          0.39978E-02      19   0.59570E-08   0.12935E-08 0.19909E+00 
c  epsilon      0.10969E+02      11   0.36762E-08   0.10462E-01 0.17010E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.83613E-02 0.43181E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61363       0.0052575       0.0015075
v  Velocity[Y]            -0.57353         0.54422       0.0030807      0.00087324
v  Velocity[Z]              1.5651          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4391          4.3406          4.3632
v  Pressure                -36.401          360.05          87.672          169.88
v  r11                   0.0010617         0.08185        0.013075        0.018286
v  r22                   0.0011147         0.08263        0.013355        0.018646
v  r33                   0.0016416         0.17423        0.027252        0.037207
v  r12                   -0.010665        0.013577     -0.00023383     -0.00030931
v  r13                   -0.045532        0.052801      9.3241e-05       0.0010138
v  r23                   -0.046714        0.051212      3.0534e-05       0.0005746
v  epsilon                0.069224          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9955e-05       0.0099177       0.0009251       0.0017427
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2771         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71351         0.85284


 TIME FOR THE TIME STEP            10756:        0.72886E+02

===============================================================


 INSTANT    0.107570000E-01   TIME STEP NUMBER           10757
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.405752140E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.206891931E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.564655087E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.408667690E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.103484358E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81140E-03   0.44986E-02 0.19867E+01 
c  Velocity[X]                                      0.13732E-03 
c  Velocity[Y]                                      0.12778E-03 
c  Velocity[Z]                                      0.42334E-02 
c  Pressure     0.36373E-04     133   0.92584E-02   0.25655E-01 0.00000E+00 
c  r11          0.10585E-01      14   0.51496E-08   0.16817E-08 0.10066E+00 
c  r22          0.10852E-01      13   0.51297E-08   0.18510E-08 0.10127E+00 
c  r33          0.21860E-01      15   0.74077E-08   0.12804E-07 0.12801E+00 
c  r12          0.93868E-03      18   0.56267E-08   0.30867E-09 0.61520E+00 
c  r13          0.46676E-02      20   0.70705E-08   0.15381E-08 0.20102E+00 
c  r23          0.39978E-02      19   0.61593E-08   0.13086E-08 0.20076E+00 
c  epsilon      0.10969E+02      11   0.37512E-08   0.10218E-01 0.16712E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.83978E-02 0.43275E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61362       0.0052575       0.0015075
v  Velocity[Y]            -0.57365         0.54427       0.0030807      0.00087328
v  Velocity[Z]              1.5653          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4391          4.3406          4.3632
v  Pressure                -36.376           360.1          87.694          169.91
v  r11                   0.0010617        0.081866        0.013075        0.018286
v  r22                   0.0011147        0.082626        0.013355        0.018646
v  r33                   0.0016416         0.17423        0.027252        0.037207
v  r12                   -0.010662        0.013581     -0.00023383     -0.00030931
v  r13                   -0.045532        0.052804      9.3241e-05       0.0010138
v  r23                   -0.046715        0.051197      3.0534e-05       0.0005746
v  epsilon                0.069225          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9955e-05       0.0099178       0.0009251       0.0017427
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2771         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71351         0.85283


 TIME FOR THE TIME STEP            10757:        0.71121E+02

===============================================================


 INSTANT    0.107580000E-01   TIME STEP NUMBER           10758
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208484969E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.990641381E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127012703E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935014E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.246422728E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.429537410E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81308E-03   0.45542E-02 0.19967E+01 
c  Velocity[X]                                      0.13800E-03 
c  Velocity[Y]                                      0.12910E-03 
c  Velocity[Z]                                      0.42871E-02 
c  Pressure     0.36453E-04     133   0.92870E-02   0.25712E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.69015E-08   0.17007E-08 0.10159E+00 
c  r22          0.10852E-01      13   0.48355E-08   0.18251E-08 0.10152E+00 
c  r33          0.21860E-01      15   0.59764E-08   0.12635E-07 0.12869E+00 
c  r12          0.93868E-03      17   0.66745E-08   0.30786E-09 0.61514E+00 
c  r13          0.46676E-02      20   0.60507E-08   0.14917E-08 0.19983E+00 
c  r23          0.39978E-02      19   0.56648E-08   0.13137E-08 0.20291E+00 
c  epsilon      0.10969E+02      11   0.34045E-08   0.94551E-02 0.16328E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84185E-02 0.43244E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61362       0.0052575       0.0015076
v  Velocity[Y]            -0.57355         0.54403       0.0030807       0.0008733
v  Velocity[Z]              1.5653          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4391          4.3406          4.3632
v  Pressure                -36.402          359.99          87.621          169.81
v  r11                   0.0010617        0.081875        0.013075        0.018286
v  r22                   0.0011147        0.082628        0.013355        0.018646
v  r33                   0.0016416         0.17422        0.027252        0.037207
v  r12                    -0.01066        0.013579     -0.00023383     -0.00030931
v  r13                    -0.04553        0.052805      9.3242e-05       0.0010138
v  r23                   -0.046714        0.051184      3.0535e-05       0.0005746
v  epsilon                0.069226          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9955e-05       0.0099179       0.0009251       0.0017427
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2776         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71351         0.85283


 TIME FOR THE TIME STEP            10758:        0.71529E+02

===============================================================


 INSTANT    0.107590000E-01   TIME STEP NUMBER           10759
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294987035E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.439005302E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.205813397E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.101790515E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.945749060E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81223E-03   0.44936E-02 0.19865E+01 
c  Velocity[X]                                      0.13766E-03 
c  Velocity[Y]                                      0.12809E-03 
c  Velocity[Z]                                      0.42278E-02 
c  Pressure     0.36097E-04     131   0.91916E-02   0.25462E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.64866E-08   0.16666E-08 0.99964E-01 
c  r22          0.10852E-01      13   0.55737E-08   0.18026E-08 0.10056E+00 
c  r33          0.21860E-01      15   0.54303E-08   0.12638E-07 0.12770E+00 
c  r12          0.93868E-03      18   0.51344E-08   0.29885E-09 0.60541E+00 
c  r13          0.46676E-02      19   0.72986E-08   0.14661E-08 0.19844E+00 
c  r23          0.39978E-02      19   0.55544E-08   0.12977E-08 0.20010E+00 
c  epsilon      0.10969E+02      11   0.33271E-08   0.10380E-01 0.17306E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.84420E-02 0.43320E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61364       0.0052576       0.0015076
v  Velocity[Y]            -0.57367         0.54412       0.0030807       0.0008733
v  Velocity[Z]              1.5652          5.4391          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4391          4.3406          4.3632
v  Pressure                -36.387          359.99          87.607          169.81
v  r11                   0.0010617        0.081885        0.013075        0.018286
v  r22                   0.0011147        0.082629        0.013355        0.018646
v  r33                   0.0016417         0.17422        0.027252        0.037207
v  r12                   -0.010664        0.013587     -0.00023383     -0.00030931
v  r13                   -0.045532        0.052803      9.3243e-05       0.0010138
v  r23                   -0.046714        0.051205      3.0535e-05       0.0005746
v  epsilon                0.069226          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9957e-05       0.0099177       0.0009251       0.0017427
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2779         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71351         0.85283


 TIME FOR THE TIME STEP            10759:        0.71502E+02

===============================================================


 INSTANT    0.107600000E-01   TIME STEP NUMBER           10760
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.124832577E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.352770254E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.171897271E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.913791523E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111440405E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81326E-03   0.45031E-02 0.19863E+01 
c  Velocity[X]                                      0.13785E-03 
c  Velocity[Y]                                      0.12773E-03 
c  Velocity[Z]                                      0.42375E-02 
c  Pressure     0.36112E-04     132   0.91833E-02   0.25471E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.67645E-08   0.16507E-08 0.99867E-01 
c  r22          0.10852E-01      13   0.59016E-08   0.18262E-08 0.10111E+00 
c  r33          0.21860E-01      15   0.57677E-08   0.12507E-07 0.12719E+00 
c  r12          0.93868E-03      18   0.57902E-08   0.30146E-09 0.60908E+00 
c  r13          0.46676E-02      20   0.59615E-08   0.14841E-08 0.19881E+00 
c  r23          0.39978E-02      19   0.64483E-08   0.12792E-08 0.19912E+00 
c  epsilon      0.10969E+02      11   0.32686E-08   0.98166E-02 0.16495E+00 
c  TempC        0.25716E+06      16   0.15184E-04   0.84222E-02 0.43317E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343          0.6136       0.0052575       0.0015076
v  Velocity[Y]            -0.57361         0.54426       0.0030807       0.0008733
v  Velocity[Z]              1.5653          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4391          4.3406          4.3632
v  Pressure                -36.423             360           87.65          169.84
v  r11                   0.0010617        0.081889        0.013075        0.018286
v  r22                   0.0011147         0.08263        0.013355        0.018646
v  r33                   0.0016417         0.17425        0.027252        0.037207
v  r12                   -0.010669        0.013586     -0.00023383     -0.00030931
v  r13                    -0.04553        0.052803      9.3244e-05       0.0010138
v  r23                   -0.046713        0.051193      3.0536e-05       0.0005746
v  epsilon                0.069227          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9956e-05       0.0099176       0.0009251       0.0017427
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017852           5.278         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71351         0.85284


 TIME FOR THE TIME STEP            10760:        0.73061E+02

===============================================================


 INSTANT    0.107610000E-01   TIME STEP NUMBER           10761
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.732276187E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.535778028E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.243900527E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.448964015E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.318248333E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81200E-03   0.45265E-02 0.19921E+01 
c  Velocity[X]                                      0.13903E-03 
c  Velocity[Y]                                      0.12853E-03 
c  Velocity[Z]                                      0.42590E-02 
c  Pressure     0.36514E-04     133   0.92954E-02   0.25754E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.64891E-08   0.16335E-08 0.99206E-01 
c  r22          0.10852E-01      13   0.57515E-08   0.18058E-08 0.10083E+00 
c  r33          0.21860E-01      15   0.59522E-08   0.12430E-07 0.12654E+00 
c  r12          0.93868E-03      18   0.55885E-08   0.29287E-09 0.60377E+00 
c  r13          0.46676E-02      19   0.74268E-08   0.14810E-08 0.19880E+00 
c  r23          0.39978E-02      19   0.62875E-08   0.12792E-08 0.19800E+00 
c  epsilon      0.10969E+02      11   0.32742E-08   0.98421E-02 0.16530E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.83694E-02 0.43157E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61362       0.0052575       0.0015075
v  Velocity[Y]            -0.57357         0.54423       0.0030808      0.00087331
v  Velocity[Z]              1.5653          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4391          4.3406          4.3632
v  Pressure                -36.379          360.06          87.658          169.88
v  r11                   0.0010617        0.081891        0.013075        0.018286
v  r22                   0.0011147        0.082631        0.013355        0.018646
v  r33                   0.0016417         0.17423        0.027252        0.037207
v  r12                   -0.010668         0.01358     -0.00023383     -0.00030931
v  r13                   -0.045531        0.052803      9.3244e-05       0.0010138
v  r23                   -0.046713        0.051182      3.0537e-05      0.00057461
v  epsilon                0.069228          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9954e-05       0.0099177       0.0009251       0.0017427
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2781         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            10761:        0.72562E+02

===============================================================


 INSTANT    0.107620000E-01   TIME STEP NUMBER           10762
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.185570924E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186488894E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.187878681E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.409067999E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.549947373E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81359E-03   0.45346E-02 0.19947E+01 
c  Velocity[X]                                      0.13735E-03 
c  Velocity[Y]                                      0.12909E-03 
c  Velocity[Z]                                      0.42681E-02 
c  Pressure     0.36114E-04     132   0.91952E-02   0.25473E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.62423E-08   0.16986E-08 0.10117E+00 
c  r22          0.10852E-01      13   0.55203E-08   0.18404E-08 0.10148E+00 
c  r33          0.21860E-01      16   0.66943E-08   0.12891E-07 0.12883E+00 
c  r12          0.93868E-03      18   0.63911E-08   0.30161E-09 0.61168E+00 
c  r13          0.46676E-02      20   0.68620E-08   0.15014E-08 0.20055E+00 
c  r23          0.39978E-02      19   0.55832E-08   0.13238E-08 0.20233E+00 
c  epsilon      0.10969E+02      11   0.35528E-08   0.10274E-01 0.16856E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.83722E-02 0.43158E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162016


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61363       0.0052574       0.0015075
v  Velocity[Y]            -0.57362         0.54416       0.0030807       0.0008733
v  Velocity[Z]              1.5653          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4391          4.3406          4.3632
v  Pressure                 -36.43          360.02          87.654          169.85
v  r11                   0.0010617        0.081881        0.013075        0.018286
v  r22                   0.0011147        0.082631        0.013355        0.018646
v  r33                   0.0016417         0.17422        0.027252        0.037207
v  r12                   -0.010662        0.013581     -0.00023383     -0.00030931
v  r13                   -0.045533        0.052803      9.3245e-05       0.0010138
v  r23                   -0.046714        0.051177      3.0537e-05      0.00057461
v  epsilon                0.069229          271.12          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05       0.0099177       0.0009251       0.0017427
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2771         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71351         0.85283


 TIME FOR THE TIME STEP            10762:        0.72410E+02

===============================================================


 INSTANT    0.107630000E-01   TIME STEP NUMBER           10763
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183179799E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.581104616E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.200102469E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188761744E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.123043703E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81196E-03   0.44942E-02 0.19846E+01 
c  Velocity[X]                                      0.13845E-03 
c  Velocity[Y]                                      0.12755E-03 
c  Velocity[Z]                                      0.42282E-02 
c  Pressure     0.36181E-04     131   0.92116E-02   0.25520E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61890E-08   0.16225E-08 0.99259E-01 
c  r22          0.10852E-01      13   0.59811E-08   0.18173E-08 0.10124E+00 
c  r33          0.21860E-01      16   0.72405E-08   0.12349E-07 0.12668E+00 
c  r12          0.93868E-03      18   0.65406E-08   0.29739E-09 0.60887E+00 
c  r13          0.46676E-02      20   0.71655E-08   0.14856E-08 0.19956E+00 
c  r23          0.39978E-02      19   0.58338E-08   0.12659E-08 0.19827E+00 
c  epsilon      0.10969E+02      11   0.37364E-08   0.96610E-02 0.16430E+00 
c  TempC        0.25716E+06      16   0.15125E-04   0.84147E-02 0.43316E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162018


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63354         0.61359       0.0052575       0.0015075
v  Velocity[Y]            -0.57378         0.54423       0.0030807      0.00087331
v  Velocity[Z]              1.5655          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4391          4.3406          4.3632
v  Pressure                -36.398          360.07          87.663          169.87
v  r11                   0.0010617        0.081877        0.013075        0.018286
v  r22                   0.0011147         0.08263        0.013355        0.018646
v  r33                   0.0016417         0.17423        0.027252        0.037207
v  r12                   -0.010661        0.013579     -0.00023383     -0.00030931
v  r13                    -0.04553        0.052802      9.3246e-05       0.0010138
v  r23                   -0.046714        0.051207      3.0538e-05      0.00057461
v  epsilon                0.069229          271.14          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099177       0.0009251       0.0017427
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2772         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71351         0.85284


 TIME FOR THE TIME STEP            10763:        0.73101E+02

===============================================================


 INSTANT    0.107640000E-01   TIME STEP NUMBER           10764
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182696088E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.149109143E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.306634970E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.346849376E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.309805971E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81269E-03   0.45104E-02 0.19885E+01 
c  Velocity[X]                                      0.13788E-03 
c  Velocity[Y]                                      0.12878E-03 
c  Velocity[Z]                                      0.42437E-02 
c  Pressure     0.36194E-04     133   0.92129E-02   0.25530E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.66279E-08   0.16575E-08 0.10028E+00 
c  r22          0.10852E-01      13   0.55781E-08   0.18349E-08 0.10140E+00 
c  r33          0.21860E-01      16   0.77030E-08   0.12636E-07 0.12779E+00 
c  r12          0.93868E-03      18   0.65834E-08   0.29474E-09 0.60537E+00 
c  r13          0.46676E-02      21   0.69071E-08   0.15104E-08 0.20029E+00 
c  r23          0.39978E-02      19   0.56490E-08   0.12910E-08 0.19956E+00 
c  epsilon      0.10969E+02      11   0.36869E-08   0.10026E-01 0.16629E+00 
c  TempC        0.25716E+06      16   0.15176E-04   0.85052E-02 0.43510E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61362       0.0052575       0.0015075
v  Velocity[Y]            -0.57361         0.54431       0.0030808       0.0008733
v  Velocity[Z]              1.5653          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4391          4.3406          4.3632
v  Pressure                -36.411          360.04          87.648          169.85
v  r11                   0.0010617        0.081874        0.013075        0.018286
v  r22                   0.0011147         0.08263        0.013355        0.018646
v  r33                   0.0016417         0.17426        0.027252        0.037207
v  r12                   -0.010661        0.013583     -0.00023383     -0.00030931
v  r13                   -0.045528        0.052803      9.3246e-05       0.0010138
v  r23                   -0.046715        0.051198      3.0538e-05      0.00057461
v  epsilon                 0.06923          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099178       0.0009251       0.0017427
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2785         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71351         0.85283


 TIME FOR THE TIME STEP            10764:        0.71810E+02

===============================================================


 INSTANT    0.107650000E-01   TIME STEP NUMBER           10765
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.284868828E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190307393E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.464446762E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181529522E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.214554195E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81218E-03   0.45103E-02 0.19875E+01 
c  Velocity[X]                                      0.13746E-03 
c  Velocity[Y]                                      0.12810E-03 
c  Velocity[Z]                                      0.42447E-02 
c  Pressure     0.36510E-04     133   0.93001E-02   0.25753E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.65840E-08   0.16737E-08 0.10080E+00 
c  r22          0.10852E-01      13   0.52277E-08   0.18530E-08 0.10200E+00 
c  r33          0.21860E-01      15   0.73899E-08   0.12860E-07 0.12897E+00 
c  r12          0.93868E-03      18   0.66048E-08   0.30470E-09 0.61085E+00 
c  r13          0.46676E-02      20   0.68292E-08   0.15412E-08 0.20204E+00 
c  r23          0.39978E-02      19   0.51683E-08   0.13227E-08 0.20213E+00 
c  epsilon      0.10969E+02      11   0.33939E-08   0.10590E-01 0.17455E+00 
c  TempC        0.25716E+06      16   0.15124E-04   0.83706E-02 0.43135E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61362       0.0052575       0.0015076
v  Velocity[Y]            -0.57374         0.54437       0.0030807      0.00087329
v  Velocity[Z]              1.5654          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4391          4.3406          4.3632
v  Pressure                -36.433          360.08          87.666          169.89
v  r11                   0.0010617        0.081872        0.013075        0.018286
v  r22                   0.0011147        0.082627        0.013355        0.018646
v  r33                   0.0016417         0.17426        0.027252        0.037207
v  r12                   -0.010658        0.013581     -0.00023383     -0.00030931
v  r13                   -0.045533        0.052803      9.3247e-05       0.0010138
v  r23                   -0.046715        0.051182      3.0538e-05      0.00057461
v  epsilon                0.069231          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099178       0.0009251       0.0017427
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2793         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8793         0.71351         0.85283


 TIME FOR THE TIME STEP            10765:        0.72918E+02

===============================================================


 INSTANT    0.107660000E-01   TIME STEP NUMBER           10766
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106026810E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.801453548E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.165580159E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.349398381E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.374253834E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81283E-03   0.45340E-02 0.19942E+01 
c  Velocity[X]                                      0.13826E-03 
c  Velocity[Y]                                      0.12880E-03 
c  Velocity[Z]                                      0.42669E-02 
c  Pressure     0.36393E-04     133   0.92670E-02   0.25670E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.62072E-08   0.16179E-08 0.99437E-01 
c  r22          0.10852E-01      13   0.50761E-08   0.18103E-08 0.10116E+00 
c  r33          0.21860E-01      16   0.58188E-08   0.12340E-07 0.12682E+00 
c  r12          0.93868E-03      18   0.65301E-08   0.29445E-09 0.60458E+00 
c  r13          0.46676E-02      20   0.61306E-08   0.14799E-08 0.19926E+00 
c  r23          0.39978E-02      19   0.61046E-08   0.12566E-08 0.19758E+00 
c  epsilon      0.10969E+02      11   0.33807E-08   0.97230E-02 0.16442E+00 
c  TempC        0.25716E+06      16   0.15169E-04   0.83945E-02 0.43253E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162018


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61359       0.0052575       0.0015076
v  Velocity[Y]            -0.57369         0.54419       0.0030807      0.00087329
v  Velocity[Z]              1.5655          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4391          4.3406          4.3632
v  Pressure                -36.437          359.98          87.655          169.83
v  r11                   0.0010617        0.081873        0.013075        0.018286
v  r22                   0.0011148        0.082629        0.013355        0.018646
v  r33                   0.0016418         0.17423        0.027252        0.037207
v  r12                   -0.010666        0.013587     -0.00023383     -0.00030931
v  r13                    -0.04553        0.052805      9.3247e-05       0.0010138
v  r23                   -0.046715        0.051214      3.0538e-05      0.00057461
v  epsilon                0.069232          271.14          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099177       0.0009251       0.0017427
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2796         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8796         0.71351         0.85283


 TIME FOR THE TIME STEP            10766:        0.71061E+02

===============================================================


 INSTANT    0.107670000E-01   TIME STEP NUMBER           10767
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.432027132E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125078848E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.694673441E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.694958873E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.336247518E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81196E-03   0.45255E-02 0.19915E+01 
c  Velocity[X]                                      0.13861E-03 
c  Velocity[Y]                                      0.12846E-03 
c  Velocity[Z]                                      0.42584E-02 
c  Pressure     0.36524E-04     133   0.92993E-02   0.25762E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58398E-08   0.16253E-08 0.99722E-01 
c  r22          0.10852E-01      13   0.51507E-08   0.18326E-08 0.10134E+00 
c  r33          0.21860E-01      15   0.70408E-08   0.12495E-07 0.12718E+00 
c  r12          0.93868E-03      18   0.67544E-08   0.30030E-09 0.60929E+00 
c  r13          0.46676E-02      19   0.73345E-08   0.15080E-08 0.20001E+00 
c  r23          0.39978E-02      19   0.66156E-08   0.12801E-08 0.19927E+00 
c  epsilon      0.10969E+02      11   0.33073E-08   0.95828E-02 0.16261E+00 
c  TempC        0.25716E+06      16   0.15120E-04   0.84598E-02 0.43374E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61362       0.0052575       0.0015076
v  Velocity[Y]            -0.57376         0.54414       0.0030808      0.00087333
v  Velocity[Z]              1.5653          5.4391          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4391          4.3406          4.3632
v  Pressure                -36.373          360.03          87.645          169.85
v  r11                   0.0010617        0.081875        0.013075        0.018286
v  r22                   0.0011148         0.08263        0.013355        0.018646
v  r33                   0.0016418         0.17425        0.027252        0.037207
v  r12                   -0.010668        0.013585     -0.00023383     -0.00030931
v  r13                   -0.045529        0.052802      9.3247e-05       0.0010138
v  r23                   -0.046715        0.051203      3.0538e-05      0.00057461
v  epsilon                0.069233          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9949e-05       0.0099175       0.0009251       0.0017427
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2788         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71351         0.85284


 TIME FOR THE TIME STEP            10767:        0.75083E+02

===============================================================


 INSTANT    0.107680000E-01   TIME STEP NUMBER           10768
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.277003887E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.718469499E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.354780073E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154290712E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.422645686E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81347E-03   0.44924E-02 0.19858E+01 
c  Velocity[X]                                      0.13759E-03 
c  Velocity[Y]                                      0.12810E-03 
c  Velocity[Z]                                      0.42267E-02 
c  Pressure     0.36160E-04     131   0.92036E-02   0.25506E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56694E-08   0.16539E-08 0.99611E-01 
c  r22          0.10852E-01      13   0.53790E-08   0.18554E-08 0.10152E+00 
c  r33          0.21860E-01      15   0.60924E-08   0.12734E-07 0.12738E+00 
c  r12          0.93868E-03      18   0.72366E-08   0.30092E-09 0.60759E+00 
c  r13          0.46676E-02      19   0.68228E-08   0.15277E-08 0.20060E+00 
c  r23          0.39978E-02      19   0.61510E-08   0.13035E-08 0.19919E+00 
c  epsilon      0.10969E+02      11   0.34153E-08   0.10341E-01 0.16838E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.83565E-02 0.43141E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61362       0.0052575       0.0015076
v  Velocity[Y]            -0.57366         0.54418       0.0030808      0.00087335
v  Velocity[Z]              1.5653          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4391          4.3406          4.3632
v  Pressure                -36.408          360.02          87.641          169.85
v  r11                   0.0010617        0.081872        0.013075        0.018286
v  r22                   0.0011148         0.08263        0.013355        0.018646
v  r33                   0.0016418         0.17429        0.027252        0.037207
v  r12                   -0.010665         0.01359     -0.00023383     -0.00030931
v  r13                   -0.045532        0.052801      9.3247e-05       0.0010138
v  r23                   -0.046715        0.051193      3.0539e-05      0.00057461
v  epsilon                0.069233          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9951e-05       0.0099175      0.00092511       0.0017427
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017852           5.279         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71351         0.85284


 TIME FOR THE TIME STEP            10768:        0.71441E+02

===============================================================


 INSTANT    0.107690000E-01   TIME STEP NUMBER           10769
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.234218385E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.966085443E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.859405549E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.325606583E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106023290E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81234E-03   0.45000E-02 0.19875E+01 
c  Velocity[X]                                      0.13756E-03 
c  Velocity[Y]                                      0.12773E-03 
c  Velocity[Z]                                      0.42347E-02 
c  Pressure     0.36545E-04     132   0.93016E-02   0.25778E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.63286E-08   0.16220E-08 0.98979E-01 
c  r22          0.10852E-01      13   0.54817E-08   0.18081E-08 0.10049E+00 
c  r33          0.21860E-01      15   0.62588E-08   0.12412E-07 0.12618E+00 
c  r12          0.93868E-03      19   0.57934E-08   0.29896E-09 0.60554E+00 
c  r13          0.46676E-02      20   0.58155E-08   0.14891E-08 0.19809E+00 
c  r23          0.39978E-02      19   0.58741E-08   0.12858E-08 0.19827E+00 
c  epsilon      0.10969E+02      11   0.36040E-08   0.97242E-02 0.16352E+00 
c  TempC        0.25716E+06      16   0.15172E-04   0.84292E-02 0.43337E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162019


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63355         0.61361       0.0052575       0.0015076
v  Velocity[Y]            -0.57359         0.54431       0.0030808      0.00087336
v  Velocity[Z]               1.565          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4391          4.3406          4.3632
v  Pressure                -36.391          360.02           87.63          169.84
v  r11                   0.0010617         0.08187        0.013075        0.018286
v  r22                   0.0011148         0.08263        0.013355        0.018646
v  r33                   0.0016418         0.17426        0.027252        0.037207
v  r12                   -0.010663          0.0136     -0.00023383     -0.00030931
v  r13                   -0.045531        0.052805      9.3247e-05       0.0010138
v  r23                   -0.046715        0.051217      3.0539e-05      0.00057461
v  epsilon                0.069234          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9954e-05       0.0099175      0.00092511       0.0017427
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2797         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8797         0.71352         0.85284


 TIME FOR THE TIME STEP            10769:        0.70384E+02

===============================================================


 INSTANT    0.107700000E-01   TIME STEP NUMBER           10770
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.882779384E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.231897498E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191152616E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.482665234E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.131262538E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81233E-03   0.45390E-02 0.19952E+01 
c  Velocity[X]                                      0.13753E-03 
c  Velocity[Y]                                      0.12845E-03 
c  Velocity[Z]                                      0.42730E-02 
c  Pressure     0.36324E-04     131   0.92499E-02   0.25622E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.64372E-08   0.15948E-08 0.98480E-01 
c  r22          0.10852E-01      13   0.55233E-08   0.17891E-08 0.10005E+00 
c  r33          0.21860E-01      15   0.58359E-08   0.12198E-07 0.12547E+00 
c  r12          0.93868E-03      18   0.69973E-08   0.29226E-09 0.60094E+00 
c  r13          0.46676E-02      20   0.64221E-08   0.14731E-08 0.19768E+00 
c  r23          0.39978E-02      19   0.53573E-08   0.12582E-08 0.19679E+00 
c  epsilon      0.10969E+02      11   0.34230E-08   0.93830E-02 0.16055E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.84199E-02 0.43279E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61364       0.0052576       0.0015076
v  Velocity[Y]            -0.57345         0.54411       0.0030808      0.00087336
v  Velocity[Z]              1.5652          5.4391          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4391          4.3406          4.3632
v  Pressure                -36.429          359.99          87.635          169.83
v  r11                   0.0010617        0.081872        0.013075        0.018286
v  r22                   0.0011148        0.082631        0.013355        0.018646
v  r33                   0.0016418         0.17424        0.027253        0.037207
v  r12                   -0.010661        0.013606     -0.00023383     -0.00030931
v  r13                    -0.04553        0.052804      9.3248e-05       0.0010138
v  r23                   -0.046714        0.051204      3.0541e-05      0.00057461
v  epsilon                0.069235          271.13          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9956e-05       0.0099174      0.00092511       0.0017427
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2796         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8796         0.71351         0.85284


 TIME FOR THE TIME STEP            10770:        0.72781E+02

===============================================================


 INSTANT    0.107710000E-01   TIME STEP NUMBER           10771
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.371602575E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.391309554E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.567585487E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.114923836E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.518652571E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81361E-03   0.45050E-02 0.19874E+01 
c  Velocity[X]                                      0.13773E-03 
c  Velocity[Y]                                      0.12819E-03 
c  Velocity[Z]                                      0.42391E-02 
c  Pressure     0.36284E-04     133   0.92398E-02   0.25592E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61859E-08   0.16448E-08 0.99645E-01 
c  r22          0.10852E-01      13   0.51943E-08   0.18170E-08 0.10074E+00 
c  r33          0.21860E-01      15   0.53457E-08   0.12595E-07 0.12727E+00 
c  r12          0.93868E-03      18   0.62168E-08   0.29642E-09 0.60493E+00 
c  r13          0.46676E-02      20   0.65997E-08   0.14952E-08 0.19933E+00 
c  r23          0.39978E-02      19   0.55127E-08   0.13091E-08 0.20104E+00 
c  epsilon      0.10969E+02      11   0.33292E-08   0.10111E-01 0.17059E+00 
c  TempC        0.25716E+06      16   0.15105E-04   0.83507E-02 0.43142E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61364       0.0052576       0.0015076
v  Velocity[Y]            -0.57366         0.54421       0.0030808      0.00087334
v  Velocity[Z]              1.5652          5.4391          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4391          4.3406          4.3632
v  Pressure                -36.382          360.01          87.632          169.84
v  r11                   0.0010617        0.081873        0.013075        0.018286
v  r22                   0.0011148        0.082631        0.013355        0.018646
v  r33                   0.0016418         0.17425        0.027253        0.037207
v  r12                   -0.010665         0.01361     -0.00023383     -0.00030931
v  r13                   -0.045532        0.052801      9.3248e-05       0.0010138
v  r23                   -0.046713        0.051193       3.054e-05      0.00057461
v  epsilon                0.069236          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9958e-05       0.0099174      0.00092511       0.0017427
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017852            5.28         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179            5.88         0.71351         0.85284


 TIME FOR THE TIME STEP            10771:        0.74120E+02

===============================================================


 INSTANT    0.107720000E-01   TIME STEP NUMBER           10772
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232552135E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.197858521E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.151524543E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.192810809E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166617940E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81243E-03   0.44972E-02 0.19869E+01 
c  Velocity[X]                                      0.13733E-03 
c  Velocity[Y]                                      0.12812E-03 
c  Velocity[Z]                                      0.42318E-02 
c  Pressure     0.36156E-04     133   0.91988E-02   0.25502E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59089E-08   0.16203E-08 0.98970E-01 
c  r22          0.10852E-01      13   0.48466E-08   0.18068E-08 0.10027E+00 
c  r33          0.21860E-01      15   0.58821E-08   0.12372E-07 0.12580E+00 
c  r12          0.93868E-03      18   0.60064E-08   0.29814E-09 0.60501E+00 
c  r13          0.46676E-02      20   0.61341E-08   0.14805E-08 0.19803E+00 
c  r23          0.39978E-02      19   0.60620E-08   0.12622E-08 0.19636E+00 
c  epsilon      0.10969E+02      11   0.33842E-08   0.99496E-02 0.16603E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.84440E-02 0.43354E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61362       0.0052576       0.0015076
v  Velocity[Y]            -0.57361         0.54433       0.0030808      0.00087333
v  Velocity[Z]              1.5652          5.4391          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4391          4.3406          4.3632
v  Pressure                -36.449          359.99          87.646          169.83
v  r11                   0.0010617        0.081872        0.013075        0.018286
v  r22                   0.0011148        0.082631        0.013355        0.018646
v  r33                   0.0016418         0.17427        0.027253        0.037207
v  r12                   -0.010669        0.013606     -0.00023383     -0.00030931
v  r13                    -0.04553        0.052804      9.3249e-05       0.0010138
v  r23                   -0.046712        0.051227      3.0542e-05      0.00057461
v  epsilon                0.069236          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9958e-05       0.0099176      0.00092511       0.0017427
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2802         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8802         0.71351         0.85283


 TIME FOR THE TIME STEP            10772:        0.66390E+02

===============================================================


 INSTANT    0.107730000E-01   TIME STEP NUMBER           10773
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.255968771E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.906925145E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.321412998E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.372894853E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.421766752E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81237E-03   0.45374E-02 0.19929E+01 
c  Velocity[X]                                      0.13871E-03 
c  Velocity[Y]                                      0.12818E-03 
c  Velocity[Z]                                      0.42705E-02 
c  Pressure     0.36465E-04     133   0.92811E-02   0.25721E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60088E-08   0.16075E-08 0.98546E-01 
c  r22          0.10852E-01      13   0.49860E-08   0.17840E-08 0.99820E-01 
c  r33          0.21860E-01      15   0.55016E-08   0.12231E-07 0.12572E+00 
c  r12          0.93868E-03      18   0.60128E-08   0.29342E-09 0.60192E+00 
c  r13          0.46676E-02      19   0.67339E-08   0.14775E-08 0.19788E+00 
c  r23          0.39978E-02      19   0.54154E-08   0.12667E-08 0.19702E+00 
c  epsilon      0.10969E+02      11   0.33138E-08   0.93792E-02 0.16117E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84214E-02 0.43280E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63355         0.61363       0.0052576       0.0015076
v  Velocity[Y]            -0.57376         0.54403       0.0030809      0.00087339
v  Velocity[Z]              1.5656          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4391          4.3406          4.3632
v  Pressure                -36.386          360.03          87.635          169.85
v  r11                   0.0010617        0.081874        0.013075        0.018286
v  r22                   0.0011148        0.082627        0.013355        0.018646
v  r33                   0.0016419         0.17425        0.027253        0.037207
v  r12                   -0.010668        0.013604     -0.00023383     -0.00030931
v  r13                   -0.045531        0.052804      9.3249e-05       0.0010138
v  r23                    -0.04671        0.051217      3.0541e-05      0.00057461
v  epsilon                0.069237          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.996e-05       0.0099176      0.00092511       0.0017427
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2799         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8799         0.71351         0.85283


 TIME FOR THE TIME STEP            10773:        0.69723E+02

===============================================================


 INSTANT    0.107740000E-01   TIME STEP NUMBER           10774
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.210138044E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.708490629E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.571916993E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.183902190E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.286012215E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81266E-03   0.45060E-02 0.19903E+01 
c  Velocity[X]                                      0.13693E-03 
c  Velocity[Y]                                      0.12871E-03 
c  Velocity[Z]                                      0.42404E-02 
c  Pressure     0.36321E-04     133   0.92454E-02   0.25619E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59089E-08   0.16248E-08 0.99051E-01 
c  r22          0.10852E-01      13   0.53359E-08   0.18239E-08 0.10079E+00 
c  r33          0.21860E-01      15   0.56925E-08   0.12534E-07 0.12687E+00 
c  r12          0.93868E-03      18   0.70780E-08   0.30135E-09 0.60574E+00 
c  r13          0.46676E-02      19   0.63278E-08   0.15051E-08 0.19952E+00 
c  r23          0.39978E-02      19   0.56263E-08   0.12870E-08 0.19887E+00 
c  epsilon      0.10969E+02      11   0.34660E-08   0.97309E-02 0.16387E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.84192E-02 0.43321E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61364       0.0052576       0.0015076
v  Velocity[Y]            -0.57365         0.54406       0.0030808      0.00087335
v  Velocity[Z]              1.5655          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4391          4.3406          4.3632
v  Pressure                 -36.41          359.99          87.626          169.81
v  r11                   0.0010617        0.081873        0.013075        0.018286
v  r22                   0.0011148        0.082628        0.013355        0.018646
v  r33                   0.0016419         0.17422        0.027253        0.037207
v  r12                   -0.010663        0.013605     -0.00023383     -0.00030931
v  r13                   -0.045533        0.052805       9.325e-05       0.0010138
v  r23                   -0.046707        0.051206      3.0542e-05      0.00057461
v  epsilon                0.069238          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.996e-05       0.0099177      0.00092511       0.0017427
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2797         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8797         0.71351         0.85284


 TIME FOR THE TIME STEP            10774:        0.66829E+02

===============================================================


 INSTANT    0.107750000E-01   TIME STEP NUMBER           10775
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.125026130E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.144444253E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.135095351E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.677111953E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.243919032E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81231E-03   0.44991E-02 0.19868E+01 
c  Velocity[X]                                      0.13755E-03 
c  Velocity[Y]                                      0.12781E-03 
c  Velocity[Z]                                      0.42337E-02 
c  Pressure     0.36236E-04     131   0.92300E-02   0.25559E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59261E-08   0.16512E-08 0.99628E-01 
c  r22          0.10852E-01      13   0.52379E-08   0.18301E-08 0.10084E+00 
c  r33          0.21860E-01      15   0.54614E-08   0.12559E-07 0.12693E+00 
c  r12          0.93868E-03      18   0.67248E-08   0.29502E-09 0.60416E+00 
c  r13          0.46676E-02      19   0.63403E-08   0.14816E-08 0.19791E+00 
c  r23          0.39978E-02      19   0.52916E-08   0.12738E-08 0.19795E+00 
c  epsilon      0.10969E+02      11   0.35466E-08   0.97746E-02 0.16380E+00 
c  TempC        0.25716E+06      16   0.15104E-04   0.84020E-02 0.43186E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61362       0.0052576       0.0015076
v  Velocity[Y]            -0.57367         0.54422       0.0030808      0.00087336
v  Velocity[Z]              1.5653          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4391          4.3406          4.3632
v  Pressure                -36.417          360.03          87.631          169.84
v  r11                   0.0010617        0.081878        0.013075        0.018286
v  r22                   0.0011148         0.08263        0.013355        0.018646
v  r33                   0.0016419         0.17422        0.027253        0.037207
v  r12                   -0.010661        0.013604     -0.00023383     -0.00030932
v  r13                   -0.045531        0.052804      9.3251e-05       0.0010138
v  r23                   -0.046705        0.051234      3.0543e-05      0.00057461
v  epsilon                0.069239          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099177      0.00092511       0.0017427
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017852           5.279         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71351         0.85284


 TIME FOR THE TIME STEP            10775:        0.70791E+02

===============================================================


 INSTANT    0.107760000E-01   TIME STEP NUMBER           10776
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.629171942E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173924079E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182732405E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.140151452E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100763617E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81292E-03   0.45009E-02 0.19864E+01 
c  Velocity[X]                                      0.13784E-03 
c  Velocity[Y]                                      0.12831E-03 
c  Velocity[Z]                                      0.42347E-02 
c  Pressure     0.36157E-04     131   0.92066E-02   0.25503E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55663E-08   0.16573E-08 0.99909E-01 
c  r22          0.10852E-01      13   0.51765E-08   0.18396E-08 0.10086E+00 
c  r33          0.21860E-01      14   0.69281E-08   0.12732E-07 0.12752E+00 
c  r12          0.93868E-03      18   0.59770E-08   0.29591E-09 0.60387E+00 
c  r13          0.46676E-02      19   0.68119E-08   0.15235E-08 0.19962E+00 
c  r23          0.39978E-02      19   0.55942E-08   0.12990E-08 0.19971E+00 
c  epsilon      0.10969E+02      11   0.34353E-08   0.10242E-01 0.16689E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.83797E-02 0.43203E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61363       0.0052575       0.0015075
v  Velocity[Y]            -0.57352         0.54438       0.0030808      0.00087338
v  Velocity[Z]              1.5651          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4391          4.3406          4.3632
v  Pressure                -36.434          360.04          87.683          169.87
v  r11                   0.0010617        0.081881        0.013075        0.018286
v  r22                   0.0011148        0.082631        0.013355        0.018646
v  r33                   0.0016419         0.17425        0.027253        0.037207
v  r12                    -0.01066        0.013606     -0.00023383     -0.00030932
v  r13                   -0.045529        0.052804      9.3251e-05       0.0010138
v  r23                   -0.046703        0.051227      3.0543e-05      0.00057461
v  epsilon                 0.06924          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9957e-05       0.0099175      0.00092511       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2779         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            10776:        0.66340E+02

===============================================================


 INSTANT    0.107770000E-01   TIME STEP NUMBER           10777
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.283710649E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.313689610E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.312883995E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.109422514E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.217480198E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81331E-03   0.45057E-02 0.19869E+01 
c  Velocity[X]                                      0.13706E-03 
c  Velocity[Y]                                      0.12868E-03 
c  Velocity[Z]                                      0.42399E-02 
c  Pressure     0.36149E-04     133   0.91968E-02   0.25497E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50684E-08   0.16600E-08 0.99705E-01 
c  r22          0.10852E-01      13   0.56354E-08   0.18280E-08 0.10093E+00 
c  r33          0.21860E-01      15   0.55023E-08   0.12661E-07 0.12759E+00 
c  r12          0.93869E-03      18   0.59002E-08   0.29987E-09 0.60761E+00 
c  r13          0.46676E-02      19   0.75938E-08   0.15006E-08 0.19905E+00 
c  r23          0.39978E-02      19   0.62576E-08   0.13146E-08 0.20177E+00 
c  epsilon      0.10969E+02      11   0.34415E-08   0.10087E-01 0.16960E+00 
c  TempC        0.25716E+06      16   0.15122E-04   0.83729E-02 0.43174E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61363       0.0052575       0.0015075
v  Velocity[Y]            -0.57363         0.54403       0.0030808      0.00087337
v  Velocity[Z]              1.5649          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5787          5.4391          4.3406          4.3632
v  Pressure                -36.403          359.97           87.61          169.81
v  r11                   0.0010617        0.081884        0.013075        0.018286
v  r22                   0.0011148        0.082632        0.013355        0.018646
v  r33                   0.0016419         0.17423        0.027253        0.037207
v  r12                   -0.010663        0.013603     -0.00023383     -0.00030932
v  r13                   -0.045534        0.052802      9.3251e-05       0.0010138
v  r23                   -0.046701        0.051213      3.0543e-05      0.00057461
v  epsilon                 0.06924          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9956e-05       0.0099174      0.00092511       0.0017428
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2772         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85285


 TIME FOR THE TIME STEP            10777:        0.66633E+02

===============================================================


 INSTANT    0.107780000E-01   TIME STEP NUMBER           10778
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.213092458E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.376575595E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.271877341E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.374891712E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.763722109E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81162E-03   0.45252E-02 0.19944E+01 
c  Velocity[X]                                      0.13832E-03 
c  Velocity[Y]                                      0.12845E-03 
c  Velocity[Z]                                      0.42584E-02 
c  Pressure     0.36396E-04     133   0.92692E-02   0.25671E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49364E-08   0.16412E-08 0.99176E-01 
c  r22          0.10852E-01      13   0.56046E-08   0.18157E-08 0.10084E+00 
c  r33          0.21860E-01      15   0.59852E-08   0.12472E-07 0.12667E+00 
c  r12          0.93869E-03      18   0.57053E-08   0.29650E-09 0.60472E+00 
c  r13          0.46676E-02      20   0.64710E-08   0.14718E-08 0.19782E+00 
c  r23          0.39978E-02      19   0.59779E-08   0.12890E-08 0.19850E+00 
c  epsilon      0.10969E+02      11   0.33720E-08   0.97190E-02 0.16353E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84223E-02 0.43286E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61359       0.0052575       0.0015075
v  Velocity[Y]             -0.5736         0.54408       0.0030808       0.0008734
v  Velocity[Z]               1.565          5.4391          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4391          4.3406          4.3632
v  Pressure                -36.429          360.06          87.676          169.89
v  r11                   0.0010617        0.081884        0.013075        0.018286
v  r22                   0.0011148        0.082632        0.013355        0.018646
v  r33                   0.0016419          0.1742        0.027253        0.037207
v  r12                   -0.010668        0.013604     -0.00023383     -0.00030932
v  r13                   -0.045531        0.052804      9.3251e-05       0.0010138
v  r23                     -0.0467        0.051206      3.0544e-05      0.00057461
v  epsilon                0.069241          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9954e-05       0.0099174      0.00092511       0.0017428
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2772         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71351         0.85284


 TIME FOR THE TIME STEP            10778:        0.64219E+02

===============================================================


 INSTANT    0.107790000E-01   TIME STEP NUMBER           10779
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.441391919E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.484704956E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.429812299E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935025E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.957118371E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.734590981E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81229E-03   0.45294E-02 0.19923E+01 
c  Velocity[X]                                      0.13850E-03 
c  Velocity[Y]                                      0.12774E-03 
c  Velocity[Z]                                      0.42632E-02 
c  Pressure     0.36038E-04     132   0.91775E-02   0.25419E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.48244E-08   0.16440E-08 0.98844E-01 
c  r22          0.10852E-01      13   0.57486E-08   0.18094E-08 0.10046E+00 
c  r33          0.21860E-01      15   0.50517E-08   0.12484E-07 0.12619E+00 
c  r12          0.93869E-03      18   0.54349E-08   0.29563E-09 0.60241E+00 
c  r13          0.46676E-02      19   0.55164E-08   0.14857E-08 0.19822E+00 
c  r23          0.39978E-02      19   0.53179E-08   0.12967E-08 0.19841E+00 
c  epsilon      0.10969E+02      11   0.33783E-08   0.97301E-02 0.16190E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.84826E-02 0.43421E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61362       0.0052575       0.0015075
v  Velocity[Y]            -0.57374         0.54421       0.0030809      0.00087341
v  Velocity[Z]              1.5652          5.4392          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4392          4.3406          4.3632
v  Pressure                 -36.39             360          87.623          169.83
v  r11                   0.0010617        0.081887        0.013075        0.018286
v  r22                   0.0011148        0.082629        0.013355        0.018646
v  r33                   0.0016419          0.1742        0.027253        0.037207
v  r12                   -0.010665        0.013607     -0.00023383     -0.00030932
v  r13                    -0.04553        0.052804      9.3251e-05       0.0010138
v  r23                     -0.0467        0.051232      3.0544e-05      0.00057461
v  epsilon                0.069242          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9954e-05       0.0099174      0.00092511       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2781         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71351         0.85284


 TIME FOR THE TIME STEP            10779:        0.65857E+02

===============================================================


 INSTANT    0.107800000E-01   TIME STEP NUMBER           10780
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.370191522E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.181218086E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.714712591E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.848488415E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.153498039E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81356E-03   0.44815E-02 0.19845E+01 
c  Velocity[X]                                      0.13710E-03 
c  Velocity[Y]                                      0.12772E-03 
c  Velocity[Z]                                      0.42166E-02 
c  Pressure     0.35759E-04     132   0.91131E-02   0.25222E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51703E-08   0.16258E-08 0.99240E-01 
c  r22          0.10852E-01      13   0.53393E-08   0.18211E-08 0.10054E+00 
c  r33          0.21860E-01      15   0.57998E-08   0.12463E-07 0.12657E+00 
c  r12          0.93869E-03      18   0.51792E-08   0.29652E-09 0.60631E+00 
c  r13          0.46676E-02      18   0.70914E-08   0.14880E-08 0.19791E+00 
c  r23          0.39978E-02      19   0.54940E-08   0.12645E-08 0.19794E+00 
c  epsilon      0.10969E+02      11   0.33801E-08   0.97606E-02 0.16446E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.83682E-02 0.43174E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162020


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61361       0.0052574       0.0015075
v  Velocity[Y]            -0.57372         0.54432       0.0030808      0.00087339
v  Velocity[Z]              1.5653          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4392          4.3406          4.3632
v  Pressure                -36.414          360.01          87.649          169.84
v  r11                   0.0010617        0.081892        0.013075        0.018286
v  r22                   0.0011148        0.082629        0.013355        0.018646
v  r33                   0.0016419         0.17423        0.027253        0.037207
v  r12                   -0.010662        0.013604     -0.00023383     -0.00030932
v  r13                   -0.045533        0.052802      9.3251e-05       0.0010138
v  r23                   -0.046699        0.051224      3.0544e-05      0.00057462
v  epsilon                0.069243          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099175      0.00092512       0.0017428
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2776         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71351         0.85284


 TIME FOR THE TIME STEP            10780:        0.65954E+02

===============================================================


 INSTANT    0.107810000E-01   TIME STEP NUMBER           10781
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.193717573E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.214004745E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.114499100E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276002329E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.654412975E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81197E-03   0.44924E-02 0.19858E+01 
c  Velocity[X]                                      0.13752E-03 
c  Velocity[Y]                                      0.12822E-03 
c  Velocity[Z]                                      0.42266E-02 
c  Pressure     0.36250E-04     133   0.92282E-02   0.25568E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52965E-08   0.15929E-08 0.97882E-01 
c  r22          0.10852E-01      13   0.50067E-08   0.18238E-08 0.10072E+00 
c  r33          0.21860E-01      15   0.57026E-08   0.12408E-07 0.12606E+00 
c  r12          0.93869E-03      18   0.52463E-08   0.29723E-09 0.60546E+00 
c  r13          0.46676E-02      19   0.55493E-08   0.15047E-08 0.19840E+00 
c  r23          0.39978E-02      19   0.59052E-08   0.12623E-08 0.19722E+00 
c  epsilon      0.10969E+02      11   0.34304E-08   0.98326E-02 0.16323E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.83806E-02 0.43250E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61358       0.0052575       0.0015075
v  Velocity[Y]            -0.57371         0.54412       0.0030809       0.0008734
v  Velocity[Z]              1.5652          5.4392          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4392          4.3406          4.3632
v  Pressure                -36.364          360.01          87.629          169.84
v  r11                   0.0010617        0.081898        0.013075        0.018286
v  r22                   0.0011148        0.082631        0.013355        0.018646
v  r33                    0.001642         0.17421        0.027253        0.037207
v  r12                   -0.010665        0.013608     -0.00023383     -0.00030932
v  r13                   -0.045532        0.052804      9.3252e-05       0.0010138
v  r23                   -0.046699        0.051215      3.0544e-05      0.00057462
v  epsilon                0.069244          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9949e-05       0.0099175      0.00092512       0.0017428
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2776         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71351         0.85284


 TIME FOR THE TIME STEP            10781:        0.68679E+02

===============================================================


 INSTANT    0.107820000E-01   TIME STEP NUMBER           10782
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.180845725E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178960479E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.298945630E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.297204838E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.432921438E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81212E-03   0.45326E-02 0.19949E+01 
c  Velocity[X]                                      0.13811E-03 
c  Velocity[Y]                                      0.12901E-03 
c  Velocity[Z]                                      0.42655E-02 
c  Pressure     0.36274E-04     132   0.92424E-02   0.25586E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52743E-08   0.16350E-08 0.98693E-01 
c  r22          0.10852E-01      13   0.50944E-08   0.18071E-08 0.10052E+00 
c  r33          0.21860E-01      14   0.69717E-08   0.12474E-07 0.12631E+00 
c  r12          0.93869E-03      18   0.59058E-08   0.30040E-09 0.60487E+00 
c  r13          0.46676E-02      19   0.58588E-08   0.14773E-08 0.19807E+00 
c  r23          0.39978E-02      19   0.62112E-08   0.12898E-08 0.19854E+00 
c  epsilon      0.10969E+02      11   0.33123E-08   0.98654E-02 0.16551E+00 
c  TempC        0.25716E+06      16   0.15124E-04   0.84342E-02 0.43301E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61361       0.0052575       0.0015075
v  Velocity[Y]             -0.5737         0.54424        0.003081      0.00087343
v  Velocity[Z]              1.5654          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4392          4.3406          4.3632
v  Pressure                -36.391          360.05          87.688          169.89
v  r11                   0.0010617          0.0819        0.013075        0.018286
v  r22                   0.0011148        0.082633        0.013355        0.018646
v  r33                    0.001642          0.1742        0.027253        0.037207
v  r12                   -0.010664        0.013603     -0.00023383     -0.00030932
v  r13                    -0.04553        0.052804      9.3253e-05       0.0010138
v  r23                   -0.046698        0.051241      3.0545e-05      0.00057462
v  epsilon                0.069244          271.14          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9949e-05       0.0099175      0.00092512       0.0017428
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2778         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85284


 TIME FOR THE TIME STEP            10782:        0.68493E+02

===============================================================


 INSTANT    0.107830000E-01   TIME STEP NUMBER           10783
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.281967897E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.774965790E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.165081706E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.294384199E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.100399127E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81355E-03   0.45009E-02 0.19881E+01 
c  Velocity[X]                                      0.13826E-03 
c  Velocity[Y]                                      0.12735E-03 
c  Velocity[Z]                                      0.42352E-02 
c  Pressure     0.36251E-04     133   0.92292E-02   0.25570E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.47998E-08   0.16541E-08 0.99791E-01 
c  r22          0.10852E-01      13   0.49225E-08   0.18129E-08 0.10058E+00 
c  r33          0.21860E-01      15   0.56484E-08   0.12547E-07 0.12689E+00 
c  r12          0.93869E-03      18   0.54971E-08   0.30035E-09 0.60659E+00 
c  r13          0.46676E-02      18   0.68018E-08   0.14870E-08 0.19842E+00 
c  r23          0.39978E-02      19   0.60958E-08   0.12957E-08 0.19981E+00 
c  epsilon      0.10969E+02      11   0.33728E-08   0.10175E-01 0.17137E+00 
c  TempC        0.25716E+06      16   0.15114E-04   0.83976E-02 0.43193E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61365       0.0052575       0.0015075
v  Velocity[Y]            -0.57368         0.54439       0.0030809      0.00087342
v  Velocity[Z]              1.5651          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4392          4.3406          4.3632
v  Pressure                -36.384          360.07          87.676           169.9
v  r11                   0.0010618        0.081909        0.013075        0.018286
v  r22                   0.0011148        0.082632        0.013355        0.018646
v  r33                    0.001642         0.17423        0.027253        0.037207
v  r12                   -0.010661        0.013608     -0.00023383     -0.00030932
v  r13                   -0.045532        0.052801      9.3253e-05       0.0010138
v  r23                   -0.046697        0.051223      3.0545e-05      0.00057462
v  epsilon                0.069245          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099177      0.00092512       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2777         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71351         0.85284


 TIME FOR THE TIME STEP            10783:        0.68169E+02

===============================================================


 INSTANT    0.107840000E-01   TIME STEP NUMBER           10784
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133977653E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.305959727E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.372652641E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.124480246E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.199693548E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81216E-03   0.44928E-02 0.19854E+01 
c  Velocity[X]                                      0.13743E-03 
c  Velocity[Y]                                      0.12760E-03 
c  Velocity[Z]                                      0.42277E-02 
c  Pressure     0.35962E-04     131   0.91503E-02   0.25365E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.48390E-08   0.15922E-08 0.97919E-01 
c  r22          0.10852E-01      13   0.49190E-08   0.17679E-08 0.99560E-01 
c  r33          0.21860E-01      14   0.68627E-08   0.12100E-07 0.12451E+00 
c  r12          0.93869E-03      18   0.50658E-08   0.29017E-09 0.59842E+00 
c  r13          0.46676E-02      18   0.71199E-08   0.14618E-08 0.19646E+00 
c  r23          0.39978E-02      19   0.59457E-08   0.12584E-08 0.19544E+00 
c  epsilon      0.10969E+02      11   0.31406E-08   0.94820E-02 0.16177E+00 
c  TempC        0.25716E+06      16   0.15190E-04   0.84249E-02 0.43298E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162016


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61361       0.0052574       0.0015075
v  Velocity[Y]            -0.57346         0.54426       0.0030809      0.00087338
v  Velocity[Z]              1.5652          5.4392          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4392          4.3406          4.3632
v  Pressure                -36.407             360          87.637          169.83
v  r11                   0.0010618         0.08191        0.013075        0.018286
v  r22                   0.0011148        0.082632        0.013355        0.018646
v  r33                    0.001642         0.17426        0.027253        0.037207
v  r12                   -0.010662        0.013611     -0.00023383     -0.00030932
v  r13                    -0.04553        0.052802      9.3253e-05       0.0010138
v  r23                   -0.046698        0.051209      3.0545e-05      0.00057462
v  epsilon                0.069246          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9949e-05       0.0099177      0.00092512       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2775         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71352         0.85284


 TIME FOR THE TIME STEP            10784:        0.67819E+02

===============================================================


 INSTANT    0.107850000E-01   TIME STEP NUMBER           10785
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.603502140E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.177186445E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.170350823E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.267554185E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.323030743E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81200E-03   0.45080E-02 0.19887E+01 
c  Velocity[X]                                      0.13729E-03 
c  Velocity[Y]                                      0.12827E-03 
c  Velocity[Z]                                      0.42424E-02 
c  Pressure     0.36082E-04     133   0.91851E-02   0.25450E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52205E-08   0.16172E-08 0.98342E-01 
c  r22          0.10852E-01      13   0.51343E-08   0.18182E-08 0.10061E+00 
c  r33          0.21860E-01      15   0.54035E-08   0.12508E-07 0.12636E+00 
c  r12          0.93869E-03      18   0.54516E-08   0.29415E-09 0.60341E+00 
c  r13          0.46676E-02      18   0.71532E-08   0.14974E-08 0.19928E+00 
c  r23          0.39978E-02      19   0.64534E-08   0.12824E-08 0.19789E+00 
c  epsilon      0.10969E+02      11   0.33562E-08   0.97870E-02 0.16393E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.83902E-02 0.43255E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162016


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61363       0.0052574       0.0015075
v  Velocity[Y]             -0.5736         0.54414       0.0030809      0.00087335
v  Velocity[Z]              1.5652          5.4392          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4392          4.3406          4.3632
v  Pressure                -36.387          360.01          87.636          169.84
v  r11                   0.0010618        0.081909        0.013075        0.018286
v  r22                   0.0011148        0.082633        0.013355        0.018646
v  r33                    0.001642          0.1743        0.027253        0.037207
v  r12                   -0.010668        0.013606     -0.00023383     -0.00030932
v  r13                   -0.045531        0.052803      9.3253e-05       0.0010138
v  r23                   -0.046699        0.051192      3.0545e-05      0.00057462
v  epsilon                0.069247           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099177      0.00092512       0.0017428
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2777         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71351         0.85283


 TIME FOR THE TIME STEP            10785:        0.67968E+02

===============================================================


 INSTANT    0.107860000E-01   TIME STEP NUMBER           10786
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.350195766E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.118293598E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.356344784E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282280469E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.252491783E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69778E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81355E-03   0.45119E-02 0.19895E+01 
c  Velocity[X]                                      0.13749E-03 
c  Velocity[Y]                                      0.12792E-03 
c  Velocity[Z]                                      0.42465E-02 
c  Pressure     0.36089E-04     133   0.91932E-02   0.25455E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50787E-08   0.16291E-08 0.99026E-01 
c  r22          0.10852E-01      13   0.51295E-08   0.18059E-08 0.10062E+00 
c  r33          0.21860E-01      14   0.70571E-08   0.12468E-07 0.12650E+00 
c  r12          0.93869E-03      18   0.58222E-08   0.29544E-09 0.60254E+00 
c  r13          0.46676E-02      18   0.65262E-08   0.14962E-08 0.19964E+00 
c  r23          0.39978E-02      19   0.59541E-08   0.12899E-08 0.19890E+00 
c  epsilon      0.10969E+02      11   0.33498E-08   0.98817E-02 0.16646E+00 
c  TempC        0.25716E+06      16   0.15172E-04   0.83314E-02 0.43045E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61363       0.0052575       0.0015075
v  Velocity[Y]            -0.57362         0.54424       0.0030809      0.00087337
v  Velocity[Z]              1.5653          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4392          4.3406          4.3632
v  Pressure                -36.417          360.03          87.678          169.87
v  r11                   0.0010618        0.081904        0.013075        0.018286
v  r22                   0.0011149        0.082634        0.013355        0.018646
v  r33                    0.001642         0.17429        0.027253        0.037207
v  r12                   -0.010668         0.01361     -0.00023383     -0.00030932
v  r13                   -0.045533        0.052803      9.3254e-05       0.0010138
v  r23                     -0.0467        0.051215      3.0545e-05      0.00057462
v  epsilon                0.069248           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099176      0.00092512       0.0017428
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2771         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71351         0.85284


 TIME FOR THE TIME STEP            10786:        0.67759E+02

===============================================================


 INSTANT    0.107870000E-01   TIME STEP NUMBER           10787
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.196588675E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153815125E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.497112148E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.309058627E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149931680E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69777E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81222E-03   0.45132E-02 0.19899E+01 
c  Velocity[X]                                      0.13790E-03 
c  Velocity[Y]                                      0.12764E-03 
c  Velocity[Z]                                      0.42477E-02 
c  Pressure     0.36611E-04     132   0.93189E-02   0.25823E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52712E-08   0.16322E-08 0.98957E-01 
c  r22          0.10852E-01      13   0.56501E-08   0.18204E-08 0.10066E+00 
c  r33          0.21860E-01      14   0.69367E-08   0.12501E-07 0.12631E+00 
c  r12          0.93869E-03      18   0.59895E-08   0.29546E-09 0.60180E+00 
c  r13          0.46676E-02      19   0.54221E-08   0.14915E-08 0.19870E+00 
c  r23          0.39978E-02      19   0.56310E-08   0.12784E-08 0.19768E+00 
c  epsilon      0.10969E+02      11   0.33643E-08   0.99250E-02 0.16573E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.84372E-02 0.43303E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61362       0.0052574       0.0015075
v  Velocity[Y]            -0.57366         0.54433       0.0030809      0.00087336
v  Velocity[Z]              1.5654          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4392          4.3406          4.3632
v  Pressure                -36.365          360.02          87.649          169.85
v  r11                   0.0010618          0.0819        0.013075        0.018286
v  r22                   0.0011149         0.08263        0.013355        0.018646
v  r33                    0.001642         0.17426        0.027253        0.037207
v  r12                   -0.010665        0.013608     -0.00023383     -0.00030932
v  r13                    -0.04553        0.052804      9.3255e-05       0.0010139
v  r23                   -0.046701         0.05121      3.0545e-05      0.00057462
v  epsilon                0.069249          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9951e-05       0.0099177      0.00092512       0.0017428
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2767         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767         0.71351         0.85284


 TIME FOR THE TIME STEP            10787:        0.66880E+02

===============================================================


 INSTANT    0.107880000E-01   TIME STEP NUMBER           10788
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116504986E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.197903673E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.337148929E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.585282024E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199025145E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81271E-03   0.45026E-02 0.19883E+01 
c  Velocity[X]                                      0.13737E-03 
c  Velocity[Y]                                      0.12813E-03 
c  Velocity[Z]                                      0.42372E-02 
c  Pressure     0.36222E-04     132   0.92197E-02   0.25549E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51310E-08   0.16343E-08 0.99097E-01 
c  r22          0.10852E-01      13   0.54132E-08   0.17906E-08 0.99960E-01 
c  r33          0.21860E-01      14   0.70750E-08   0.12533E-07 0.12665E+00 
c  r12          0.93869E-03      18   0.56086E-08   0.29723E-09 0.60299E+00 
c  r13          0.46676E-02      18   0.67963E-08   0.15068E-08 0.19939E+00 
c  r23          0.39978E-02      19   0.52682E-08   0.13052E-08 0.20045E+00 
c  epsilon      0.10969E+02      11   0.33441E-08   0.10215E-01 0.17020E+00 
c  TempC        0.25716E+06      16   0.15177E-04   0.84418E-02 0.43345E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63332         0.61366       0.0052574       0.0015075
v  Velocity[Y]            -0.57344         0.54409       0.0030809      0.00087336
v  Velocity[Z]              1.5654          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4392          4.3406          4.3632
v  Pressure                -36.397          360.06          87.685          169.89
v  r11                   0.0010618        0.081897        0.013075        0.018286
v  r22                   0.0011149        0.082631        0.013355        0.018646
v  r33                    0.001642         0.17427        0.027253        0.037207
v  r12                   -0.010666        0.013607     -0.00023383     -0.00030932
v  r13                   -0.045529        0.052804      9.3255e-05       0.0010139
v  r23                   -0.046702        0.051201      3.0545e-05      0.00057462
v  epsilon                0.069249          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9948e-05       0.0099175      0.00092512       0.0017428
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2769         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71351         0.85283


 TIME FOR THE TIME STEP            10788:        0.68612E+02

===============================================================


 INSTANT    0.107890000E-01   TIME STEP NUMBER           10789
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.720795554E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.232824863E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226175872E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.238850552E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.102898616E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69776E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81250E-03   0.44942E-02 0.19859E+01 
c  Velocity[X]                                      0.13803E-03 
c  Velocity[Y]                                      0.12863E-03 
c  Velocity[Z]                                      0.42275E-02 
c  Pressure     0.36505E-04     131   0.92931E-02   0.25748E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53573E-08   0.15988E-08 0.98471E-01 
c  r22          0.10852E-01      13   0.55815E-08   0.17808E-08 0.99785E-01 
c  r33          0.21860E-01      15   0.56153E-08   0.12155E-07 0.12541E+00 
c  r12          0.93869E-03      18   0.51638E-08   0.29238E-09 0.60278E+00 
c  r13          0.46676E-02      18   0.63478E-08   0.14669E-08 0.19758E+00 
c  r23          0.39978E-02      19   0.54844E-08   0.12534E-08 0.19736E+00 
c  epsilon      0.10969E+02      11   0.33470E-08   0.93185E-02 0.16026E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84119E-02 0.43264E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61365       0.0052574       0.0015074
v  Velocity[Y]             -0.5735         0.54406       0.0030809      0.00087333
v  Velocity[Z]              1.5655          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4392          4.3406          4.3632
v  Pressure                -36.356          360.03          87.646          169.86
v  r11                   0.0010618        0.081894        0.013075        0.018286
v  r22                   0.0011149        0.082633        0.013355        0.018646
v  r33                    0.001642         0.17431        0.027253        0.037207
v  r12                    -0.01067        0.013609     -0.00023383     -0.00030932
v  r13                   -0.045533        0.052804      9.3255e-05       0.0010139
v  r23                   -0.046703        0.051217      3.0545e-05      0.00057462
v  epsilon                 0.06925          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099173      0.00092512       0.0017428
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2773         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            10789:        0.68540E+02

===============================================================


 INSTANT    0.107900000E-01   TIME STEP NUMBER           10790
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.911447247E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122062070E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.412397136E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.243915471E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179463154E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81374E-03   0.45185E-02 0.19923E+01 
c  Velocity[X]                                      0.13801E-03 
c  Velocity[Y]                                      0.12802E-03 
c  Velocity[Z]                                      0.42525E-02 
c  Pressure     0.35666E-04     134   0.90831E-02   0.25157E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55238E-08   0.16321E-08 0.99080E-01 
c  r22          0.10852E-01      13   0.54638E-08   0.18201E-08 0.10051E+00 
c  r33          0.21860E-01      15   0.57921E-08   0.12449E-07 0.12626E+00 
c  r12          0.93869E-03      18   0.53154E-08   0.29700E-09 0.60781E+00 
c  r13          0.46676E-02      19   0.56365E-08   0.14825E-08 0.19838E+00 
c  r23          0.39978E-02      19   0.57830E-08   0.12728E-08 0.19840E+00 
c  epsilon      0.10969E+02      11   0.32506E-08   0.98028E-02 0.16477E+00 
c  TempC        0.25716E+06      16   0.15142E-04   0.84069E-02 0.43305E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63336         0.61361       0.0052573       0.0015074
v  Velocity[Y]            -0.57338         0.54417       0.0030808      0.00087328
v  Velocity[Z]              1.5652          5.4392          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4392          4.3406          4.3632
v  Pressure                -36.417          360.02          87.668          169.85
v  r11                   0.0010618        0.081891        0.013075        0.018286
v  r22                   0.0011149        0.082634        0.013355        0.018646
v  r33                    0.001642         0.17428        0.027253        0.037207
v  r12                    -0.01067        0.013607     -0.00023383     -0.00030932
v  r13                    -0.04553        0.052806      9.3256e-05       0.0010139
v  r23                   -0.046703        0.051209      3.0546e-05      0.00057462
v  epsilon                0.069251           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099174      0.00092512       0.0017428
v  CourantNb               0.44258             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2781         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            10790:        0.67995E+02

===============================================================


 INSTANT    0.107910000E-01   TIME STEP NUMBER           10791
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.119515656E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.174705897E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.312153304E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.255219534E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.287096146E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81174E-03   0.44984E-02 0.19861E+01 
c  Velocity[X]                                      0.13850E-03 
c  Velocity[Y]                                      0.12814E-03 
c  Velocity[Z]                                      0.42317E-02 
c  Pressure     0.36550E-04     131   0.92981E-02   0.25780E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57132E-08   0.16293E-08 0.99143E-01 
c  r22          0.10852E-01      13   0.53610E-08   0.18228E-08 0.10103E+00 
c  r33          0.21860E-01      15   0.56094E-08   0.12394E-07 0.12638E+00 
c  r12          0.93869E-03      18   0.51874E-08   0.29282E-09 0.60469E+00 
c  r13          0.46676E-02      20   0.62756E-08   0.15008E-08 0.19936E+00 
c  r23          0.39978E-02      19   0.54894E-08   0.12664E-08 0.19766E+00 
c  epsilon      0.10969E+02      11   0.31408E-08   0.97387E-02 0.16526E+00 
c  TempC        0.25716E+06      16   0.15112E-04   0.84665E-02 0.43430E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63333         0.61365       0.0052574       0.0015075
v  Velocity[Y]            -0.57347         0.54429       0.0030809      0.00087333
v  Velocity[Z]              1.5653          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4392          4.3406          4.3632
v  Pressure                -36.366          360.03          87.653          169.85
v  r11                   0.0010618        0.081887        0.013075        0.018286
v  r22                   0.0011149        0.082634        0.013355        0.018646
v  r33                   0.0016421         0.17426        0.027253        0.037207
v  r12                   -0.010669        0.013607     -0.00023383     -0.00030932
v  r13                    -0.04553        0.052805      9.3257e-05       0.0010139
v  r23                   -0.046702        0.051202      3.0547e-05      0.00057462
v  epsilon                0.069252          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9951e-05       0.0099175      0.00092512       0.0017428
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2785         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            10791:        0.67076E+02

===============================================================


 INSTANT    0.107920000E-01   TIME STEP NUMBER           10792
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.307462687E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.487192561E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.332302434E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.395207201E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285754428E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81326E-03   0.45140E-02 0.19895E+01 
c  Velocity[X]                                      0.13715E-03 
c  Velocity[Y]                                      0.12757E-03 
c  Velocity[Z]                                      0.42493E-02 
c  Pressure     0.36288E-04     131   0.92368E-02   0.25595E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56500E-08   0.16351E-08 0.99060E-01 
c  r22          0.10852E-01      13   0.50817E-08   0.18301E-08 0.10091E+00 
c  r33          0.21860E-01      15   0.56656E-08   0.12558E-07 0.12660E+00 
c  r12          0.93869E-03      18   0.52352E-08   0.30130E-09 0.61069E+00 
c  r13          0.46676E-02      19   0.76388E-08   0.15072E-08 0.19948E+00 
c  r23          0.39978E-02      19   0.53463E-08   0.12779E-08 0.19793E+00 
c  epsilon      0.10969E+02      11   0.33531E-08   0.10156E-01 0.16825E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.83736E-02 0.43171E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61364       0.0052574       0.0015074
v  Velocity[Y]             -0.5734         0.54408       0.0030809      0.00087334
v  Velocity[Z]              1.5655          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4392          4.3406          4.3632
v  Pressure                -36.429          360.05           87.67          169.88
v  r11                   0.0010618        0.081882        0.013075        0.018286
v  r22                   0.0011149        0.082634        0.013355        0.018646
v  r33                   0.0016421         0.17428        0.027253        0.037207
v  r12                    -0.01067         0.01361     -0.00023383     -0.00030932
v  r13                   -0.045532        0.052805      9.3257e-05       0.0010139
v  r23                   -0.046702        0.051227      3.0547e-05      0.00057462
v  epsilon                0.069253          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099173      0.00092512       0.0017428
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71351         0.85283


 TIME FOR THE TIME STEP            10792:        0.66390E+02

===============================================================


 INSTANT    0.107930000E-01   TIME STEP NUMBER           10793
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.148197018E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.814792890E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.240812288E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.323107700E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.656672184E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81191E-03   0.44966E-02 0.19861E+01 
c  Velocity[X]                                      0.13782E-03 
c  Velocity[Y]                                      0.12774E-03 
c  Velocity[Z]                                      0.42310E-02 
c  Pressure     0.36276E-04     132   0.92317E-02   0.25587E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53708E-08   0.16288E-08 0.99240E-01 
c  r22          0.10852E-01      13   0.47293E-08   0.18236E-08 0.10106E+00 
c  r33          0.21860E-01      14   0.67294E-08   0.12550E-07 0.12734E+00 
c  r12          0.93869E-03      18   0.52310E-08   0.29474E-09 0.60803E+00 
c  r13          0.46676E-02      18   0.71308E-08   0.15079E-08 0.20048E+00 
c  r23          0.39978E-02      18   0.64145E-08   0.12934E-08 0.20058E+00 
c  epsilon      0.10969E+02      11   0.33281E-08   0.10071E-01 0.17000E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.83638E-02 0.43128E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61364       0.0052574       0.0015074
v  Velocity[Y]            -0.57347         0.54419       0.0030809      0.00087329
v  Velocity[Z]              1.5654          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4392          4.3406          4.3632
v  Pressure                -36.381          359.98          87.621          169.82
v  r11                   0.0010618        0.081895        0.013075        0.018286
v  r22                   0.0011149         0.08263        0.013355        0.018646
v  r33                   0.0016421          0.1743        0.027253        0.037207
v  r12                   -0.010665        0.013607     -0.00023383     -0.00030932
v  r13                   -0.045531        0.052806      9.3259e-05       0.0010139
v  r23                   -0.046702        0.051206      3.0547e-05      0.00057462
v  epsilon                0.069254          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9949e-05       0.0099173      0.00092513       0.0017428
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017852          5.2781         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71351         0.85284


 TIME FOR THE TIME STEP            10793:        0.68189E+02

===============================================================


 INSTANT    0.107940000E-01   TIME STEP NUMBER           10794
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.326409533E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.875333940E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.125326762E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.255763563E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.266684909E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81265E-03   0.45510E-02 0.19976E+01 
c  Velocity[X]                                      0.13871E-03 
c  Velocity[Y]                                      0.12854E-03 
c  Velocity[Z]                                      0.42837E-02 
c  Pressure     0.36495E-04     132   0.92926E-02   0.25742E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54154E-08   0.16320E-08 0.99093E-01 
c  r22          0.10852E-01      13   0.48992E-08   0.18201E-08 0.10096E+00 
c  r33          0.21860E-01      15   0.51569E-08   0.12485E-07 0.12684E+00 
c  r12          0.93869E-03      18   0.53848E-08   0.29853E-09 0.60735E+00 
c  r13          0.46676E-02      19   0.53958E-08   0.14999E-08 0.19967E+00 
c  r23          0.39978E-02      19   0.52161E-08   0.12732E-08 0.19831E+00 
c  epsilon      0.10969E+02      11   0.33511E-08   0.99361E-02 0.16494E+00 
c  TempC        0.25716E+06      16   0.15174E-04   0.84704E-02 0.43365E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61365       0.0052574       0.0015074
v  Velocity[Y]            -0.57335         0.54394        0.003081      0.00087336
v  Velocity[Z]              1.5653          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4392          4.3406          4.3632
v  Pressure                -36.416           360.1          87.704          169.92
v  r11                   0.0010618        0.081897        0.013075        0.018286
v  r22                   0.0011149        0.082632        0.013355        0.018646
v  r33                   0.0016421         0.17434        0.027253        0.037207
v  r12                    -0.01067         0.01361     -0.00023383     -0.00030932
v  r13                   -0.045529        0.052808       9.326e-05       0.0010139
v  r23                   -0.046703        0.051189      3.0548e-05      0.00057462
v  epsilon                0.069255          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099173      0.00092513       0.0017428
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2783         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71351         0.85284


 TIME FOR THE TIME STEP            10794:        0.67735E+02

===============================================================


 INSTANT    0.107950000E-01   TIME STEP NUMBER           10795
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.175153555E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.316253944E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.126304945E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.166038780E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.144181003E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81308E-03   0.45012E-02 0.19888E+01 
c  Velocity[X]                                      0.13728E-03 
c  Velocity[Y]                                      0.12760E-03 
c  Velocity[Z]                                      0.42363E-02 
c  Pressure     0.36440E-04     131   0.92778E-02   0.25704E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59553E-08   0.16418E-08 0.99360E-01 
c  r22          0.10852E-01      13   0.51119E-08   0.18030E-08 0.10089E+00 
c  r33          0.21860E-01      15   0.58528E-08   0.12397E-07 0.12682E+00 
c  r12          0.93869E-03      18   0.60796E-08   0.29879E-09 0.60430E+00 
c  r13          0.46676E-02      19   0.63535E-08   0.14791E-08 0.19907E+00 
c  r23          0.39978E-02      19   0.51854E-08   0.12880E-08 0.19977E+00 
c  epsilon      0.10969E+02      11   0.34811E-08   0.97216E-02 0.16470E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.84161E-02 0.43267E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61367       0.0052573       0.0015074
v  Velocity[Y]            -0.57351         0.54402       0.0030809      0.00087334
v  Velocity[Z]              1.5652          5.4392          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4392          4.3406          4.3632
v  Pressure                -36.393          360.02          87.646          169.85
v  r11                   0.0010618        0.081898        0.013075        0.018286
v  r22                   0.0011149        0.082633        0.013355        0.018646
v  r33                   0.0016421         0.17432        0.027253        0.037207
v  r12                   -0.010668        0.013605     -0.00023383     -0.00030932
v  r13                   -0.045532        0.052803      9.3259e-05       0.0010139
v  r23                   -0.046702        0.051212      3.0547e-05      0.00057462
v  epsilon                0.069255          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099173      0.00092513       0.0017428
v  CourantNb               0.44259             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2778         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71351         0.85283


 TIME FOR THE TIME STEP            10795:        0.67554E+02

===============================================================


 INSTANT    0.107960000E-01   TIME STEP NUMBER           10796
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.521881615E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182048160E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.265484884E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.216337096E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.803085435E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81282E-03   0.45071E-02 0.19887E+01 
c  Velocity[X]                                      0.13713E-03 
c  Velocity[Y]                                      0.12815E-03 
c  Velocity[Z]                                      0.42418E-02 
c  Pressure     0.36343E-04     132   0.92526E-02   0.25635E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54728E-08   0.15953E-08 0.98110E-01 
c  r22          0.10852E-01      13   0.48905E-08   0.18123E-08 0.10073E+00 
c  r33          0.21860E-01      15   0.53605E-08   0.12264E-07 0.12578E+00 
c  r12          0.93869E-03      18   0.61411E-08   0.29666E-09 0.60512E+00 
c  r13          0.46676E-02      19   0.67601E-08   0.14760E-08 0.19839E+00 
c  r23          0.39978E-02      19   0.53779E-08   0.12561E-08 0.19764E+00 
c  epsilon      0.10969E+02      11   0.32479E-08   0.96063E-02 0.16502E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.83525E-02 0.43153E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61367       0.0052573       0.0015074
v  Velocity[Y]            -0.57358         0.54418       0.0030808       0.0008733
v  Velocity[Z]              1.5652          5.4392          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4392          4.3406          4.3632
v  Pressure                -36.415          360.02          87.664          169.85
v  r11                   0.0010618        0.081889        0.013075        0.018286
v  r22                   0.0011149        0.082634        0.013355        0.018646
v  r33                   0.0016421         0.17428        0.027253        0.037207
v  r12                   -0.010668        0.013609     -0.00023383     -0.00030932
v  r13                    -0.04553        0.052804      9.3261e-05       0.0010139
v  r23                   -0.046702        0.051208      3.0548e-05      0.00057462
v  epsilon                0.069256          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099173      0.00092513       0.0017428
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2777         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            10796:        0.68482E+02

===============================================================


 INSTANT    0.107970000E-01   TIME STEP NUMBER           10797
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.129847481E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.938126217E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.194388110E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935016E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.306526158E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.510607213E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81157E-03   0.45241E-02 0.19903E+01 
c  Velocity[X]                                      0.13796E-03 
c  Velocity[Y]                                      0.12854E-03 
c  Velocity[Z]                                      0.42576E-02 
c  Pressure     0.36369E-04     131   0.92578E-02   0.25652E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59169E-08   0.16432E-08 0.99224E-01 
c  r22          0.10852E-01      13   0.52462E-08   0.18142E-08 0.10090E+00 
c  r33          0.21860E-01      15   0.62400E-08   0.12471E-07 0.12693E+00 
c  r12          0.93869E-03      18   0.60457E-08   0.29547E-09 0.60400E+00 
c  r13          0.46676E-02      19   0.64683E-08   0.15017E-08 0.20043E+00 
c  r23          0.39978E-02      19   0.65872E-08   0.12641E-08 0.19773E+00 
c  epsilon      0.10969E+02      11   0.34152E-08   0.99267E-02 0.16690E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.84061E-02 0.43284E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6333         0.61368       0.0052574       0.0015075
v  Velocity[Y]            -0.57367         0.54435       0.0030808       0.0008733
v  Velocity[Z]              1.5654          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4392          4.3406          4.3632
v  Pressure                -36.359          360.04           87.65          169.86
v  r11                   0.0010618        0.081889        0.013075        0.018286
v  r22                   0.0011149        0.082634        0.013355        0.018646
v  r33                   0.0016421          0.1743        0.027253        0.037207
v  r12                   -0.010664        0.013604     -0.00023383     -0.00030932
v  r13                   -0.045531        0.052804      9.3262e-05       0.0010139
v  r23                   -0.046702          0.0512      3.0548e-05      0.00057462
v  epsilon                0.069257           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099173      0.00092513       0.0017428
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2781         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71351         0.85284


 TIME FOR THE TIME STEP            10797:        0.68595E+02

===============================================================


 INSTANT    0.107980000E-01   TIME STEP NUMBER           10798
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.533095975E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.723282609E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.455613907E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.457971929E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.977249275E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81330E-03   0.45025E-02 0.19877E+01 
c  Velocity[X]                                      0.13754E-03 
c  Velocity[Y]                                      0.12747E-03 
c  Velocity[Z]                                      0.42375E-02 
c  Pressure     0.36394E-04     133   0.92690E-02   0.25671E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59590E-08   0.16588E-08 0.99690E-01 
c  r22          0.10852E-01      13   0.53595E-08   0.18175E-08 0.10097E+00 
c  r33          0.21860E-01      15   0.64999E-08   0.12646E-07 0.12791E+00 
c  r12          0.93869E-03      18   0.62604E-08   0.30138E-09 0.60658E+00 
c  r13          0.46676E-02      19   0.62562E-08   0.14931E-08 0.20024E+00 
c  r23          0.39978E-02      19   0.56886E-08   0.13171E-08 0.20198E+00 
c  epsilon      0.10969E+02      11   0.33752E-08   0.10258E-01 0.17159E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.83907E-02 0.43186E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63335         0.61373       0.0052574       0.0015075
v  Velocity[Y]            -0.57362         0.54402       0.0030809      0.00087332
v  Velocity[Z]              1.5653          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4392          4.3406          4.3632
v  Pressure                -36.422          360.06           87.68          169.89
v  r11                   0.0010618        0.081892        0.013075        0.018286
v  r22                   0.0011149        0.082634        0.013355        0.018646
v  r33                   0.0016421         0.17433        0.027253        0.037207
v  r12                   -0.010662        0.013607     -0.00023383     -0.00030932
v  r13                   -0.045533        0.052804      9.3261e-05       0.0010139
v  r23                   -0.046702        0.051217      3.0548e-05      0.00057462
v  epsilon                0.069258          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099174      0.00092513       0.0017428
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2779         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            10798:        0.67439E+02

===============================================================


 INSTANT    0.107990000E-01   TIME STEP NUMBER           10799
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.460133342E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.115973379E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.410916800E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.246932599E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.685917962E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81178E-03   0.45430E-02 0.19989E+01 
c  Velocity[X]                                      0.13903E-03 
c  Velocity[Y]                                      0.12840E-03 
c  Velocity[Z]                                      0.42756E-02 
c  Pressure     0.36781E-04     133   0.93601E-02   0.25943E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60263E-08   0.16445E-08 0.99044E-01 
c  r22          0.10852E-01      13   0.55524E-08   0.18237E-08 0.10066E+00 
c  r33          0.21861E-01      15   0.66651E-08   0.12590E-07 0.12650E+00 
c  r12          0.93869E-03      19   0.53403E-08   0.29865E-09 0.60318E+00 
c  r13          0.46676E-02      19   0.71669E-08   0.15024E-08 0.19892E+00 
c  r23          0.39978E-02      19   0.57629E-08   0.12911E-08 0.19803E+00 
c  epsilon      0.10969E+02      11   0.35003E-08   0.10134E-01 0.16664E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84594E-02 0.43343E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61369       0.0052573       0.0015075
v  Velocity[Y]            -0.57359         0.54404       0.0030809      0.00087331
v  Velocity[Z]              1.5654          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4392          4.3406          4.3632
v  Pressure                -36.403          360.02          87.645          169.85
v  r11                   0.0010618        0.081903        0.013075        0.018286
v  r22                   0.0011149        0.082634        0.013355        0.018646
v  r33                   0.0016421          0.1743        0.027253        0.037207
v  r12                   -0.010661        0.013606     -0.00023383     -0.00030932
v  r13                    -0.04553        0.052802      9.3262e-05       0.0010139
v  r23                   -0.046702        0.051209      3.0548e-05      0.00057462
v  epsilon                0.069259          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099175      0.00092513       0.0017428
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2776         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71351         0.85284


 TIME FOR THE TIME STEP            10799:        0.72791E+02

===============================================================


 INSTANT    0.108000000E-01   TIME STEP NUMBER           10800
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.494031478E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107877570E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.361055125E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.420350506E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.102078207E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81271E-03   0.44965E-02 0.19860E+01 
c  Velocity[X]                                      0.13755E-03 
c  Velocity[Y]                                      0.12719E-03 
c  Velocity[Z]                                      0.42317E-02 
c  Pressure     0.35895E-04     131   0.91440E-02   0.25319E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58981E-08   0.16051E-08 0.98472E-01 
c  r22          0.10852E-01      13   0.53410E-08   0.18159E-08 0.10046E+00 
c  r33          0.21861E-01      15   0.52352E-08   0.12408E-07 0.12609E+00 
c  r12          0.93869E-03      18   0.71152E-08   0.28876E-09 0.59867E+00 
c  r13          0.46676E-02      19   0.65791E-08   0.14993E-08 0.19863E+00 
c  r23          0.39978E-02      19   0.54641E-08   0.12577E-08 0.19714E+00 
c  epsilon      0.10969E+02      11   0.34642E-08   0.10025E-01 0.16634E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.84051E-02 0.43262E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61371       0.0052574       0.0015075
v  Velocity[Y]            -0.57343         0.54416       0.0030809      0.00087335
v  Velocity[Z]              1.5656          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4392          4.3406          4.3632
v  Pressure                -36.422          359.99           87.63          169.82
v  r11                   0.0010618        0.081906        0.013075        0.018286
v  r22                   0.0011149        0.082633        0.013355        0.018646
v  r33                   0.0016421         0.17428        0.027253        0.037207
v  r12                    -0.01066        0.013614     -0.00023383     -0.00030932
v  r13                   -0.045529        0.052802      9.3263e-05       0.0010139
v  r23                   -0.046703        0.051204      3.0549e-05      0.00057462
v  epsilon                0.069259           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9943e-05       0.0099175      0.00092513       0.0017428
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2775         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71351         0.85283


 TIME FOR THE TIME STEP            10800:        0.70237E+02

===============================================================


 INSTANT    0.108010000E-01   TIME STEP NUMBER           10801
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.297128132E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.456643177E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.160730010E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.259205787E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.749019114E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81356E-03   0.45164E-02 0.19875E+01 
c  Velocity[X]                                      0.13750E-03 
c  Velocity[Y]                                      0.12828E-03 
c  Velocity[Z]                                      0.42507E-02 
c  Pressure     0.36503E-04     133   0.92969E-02   0.25747E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.63308E-08   0.16047E-08 0.98421E-01 
c  r22          0.10852E-01      13   0.48758E-08   0.17590E-08 0.99893E-01 
c  r33          0.21861E-01      15   0.52007E-08   0.12221E-07 0.12594E+00 
c  r12          0.93869E-03      18   0.60479E-08   0.29200E-09 0.60166E+00 
c  r13          0.46676E-02      20   0.60183E-08   0.14719E-08 0.19809E+00 
c  r23          0.39978E-02      19   0.59543E-08   0.12850E-08 0.19914E+00 
c  epsilon      0.10969E+02      11   0.33166E-08   0.94219E-02 0.16269E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.83621E-02 0.43187E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61372       0.0052574       0.0015075
v  Velocity[Y]            -0.57346         0.54428       0.0030809      0.00087337
v  Velocity[Z]               1.565          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4392          4.3406          4.3632
v  Pressure                -36.379          360.04          87.655          169.86
v  r11                   0.0010618        0.081917        0.013075        0.018286
v  r22                   0.0011149        0.082633        0.013355        0.018646
v  r33                   0.0016422         0.17429        0.027253        0.037207
v  r12                   -0.010658         0.01361     -0.00023383     -0.00030932
v  r13                   -0.045533        0.052801      9.3263e-05       0.0010139
v  r23                   -0.046703        0.051231      3.0548e-05      0.00057462
v  epsilon                 0.06926           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099176      0.00092513       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2777         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71351         0.85284


 TIME FOR THE TIME STEP            10801:        0.66690E+02

===============================================================


 INSTANT    0.108020000E-01   TIME STEP NUMBER           10802
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.607981164E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.969446593E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117575949E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.261981173E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200959952E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81288E-03   0.45355E-02 0.19951E+01 
c  Velocity[X]                                      0.13807E-03 
c  Velocity[Y]                                      0.12880E-03 
c  Velocity[Z]                                      0.42686E-02 
c  Pressure     0.36182E-04     133   0.92120E-02   0.25521E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.62080E-08   0.16292E-08 0.99278E-01 
c  r22          0.10852E-01      13   0.53098E-08   0.17801E-08 0.10062E+00 
c  r33          0.21861E-01      15   0.60001E-08   0.12323E-07 0.12650E+00 
c  r12          0.93869E-03      18   0.61426E-08   0.29625E-09 0.60412E+00 
c  r13          0.46677E-02      19   0.69233E-08   0.14547E-08 0.19853E+00 
c  r23          0.39978E-02      19   0.67869E-08   0.12771E-08 0.19938E+00 
c  epsilon      0.10969E+02      11   0.33532E-08   0.96669E-02 0.16383E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.84205E-02 0.43297E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61369       0.0052574       0.0015075
v  Velocity[Y]            -0.57334         0.54409       0.0030808       0.0008733
v  Velocity[Z]              1.5652          5.4392          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4392          4.3406          4.3632
v  Pressure                -36.435          360.06          87.694          169.89
v  r11                   0.0010618        0.081919        0.013075        0.018286
v  r22                   0.0011149        0.082632        0.013355        0.018646
v  r33                   0.0016422         0.17431        0.027253        0.037207
v  r12                   -0.010667        0.013611     -0.00023383     -0.00030932
v  r13                    -0.04553        0.052802      9.3263e-05       0.0010139
v  r23                   -0.046702        0.051231      3.0549e-05      0.00057462
v  epsilon                0.069261          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9939e-05       0.0099177      0.00092513       0.0017428
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2784         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71351         0.85284


 TIME FOR THE TIME STEP            10802:        0.69594E+02

===============================================================


 INSTANT    0.108030000E-01   TIME STEP NUMBER           10803
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.264443636E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.127390182E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.944708360E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.244230007E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.264754574E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81233E-03   0.45168E-02 0.19901E+01 
c  Velocity[X]                                      0.13802E-03 
c  Velocity[Y]                                      0.12822E-03 
c  Velocity[Z]                                      0.42505E-02 
c  Pressure     0.36246E-04     131   0.92334E-02   0.25566E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57031E-08   0.16351E-08 0.99473E-01 
c  r22          0.10852E-01      13   0.50075E-08   0.18230E-08 0.10089E+00 
c  r33          0.21861E-01      15   0.65485E-08   0.12475E-07 0.12673E+00 
c  r12          0.93869E-03      18   0.63216E-08   0.29221E-09 0.60171E+00 
c  r13          0.46676E-02      19   0.62248E-08   0.14985E-08 0.19975E+00 
c  r23          0.39978E-02      18   0.68744E-08   0.12749E-08 0.19817E+00 
c  epsilon      0.10969E+02      11   0.34965E-08   0.99247E-02 0.16628E+00 
c  TempC        0.25716E+06      16   0.15105E-04   0.84200E-02 0.43259E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61371       0.0052574       0.0015075
v  Velocity[Y]             -0.5734         0.54423       0.0030809      0.00087332
v  Velocity[Z]              1.5652          5.4392          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4392          4.3406          4.3632
v  Pressure                -36.394          360.03          87.652          169.86
v  r11                   0.0010618        0.081912        0.013075        0.018286
v  r22                   0.0011149        0.082631        0.013355        0.018646
v  r33                   0.0016422         0.17435        0.027253        0.037207
v  r12                   -0.010666        0.013615     -0.00023383     -0.00030932
v  r13                   -0.045529        0.052799      9.3263e-05       0.0010139
v  r23                   -0.046701        0.051219      3.0549e-05      0.00057462
v  epsilon                0.069262          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099178      0.00092513       0.0017428
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2782         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71351         0.85283


 TIME FOR THE TIME STEP            10803:        0.66709E+02

===============================================================


 INSTANT    0.108040000E-01   TIME STEP NUMBER           10804
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.504301747E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.194406680E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.322989793E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935012E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.865815675E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108805154E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81314E-03   0.44975E-02 0.19861E+01 
c  Velocity[X]                                      0.13824E-03 
c  Velocity[Y]                                      0.12748E-03 
c  Velocity[Z]                                      0.42318E-02 
c  Pressure     0.36524E-04     132   0.92904E-02   0.25762E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55481E-08   0.16529E-08 0.99812E-01 
c  r22          0.10852E-01      13   0.49379E-08   0.18111E-08 0.10106E+00 
c  r33          0.21861E-01      15   0.69172E-08   0.12573E-07 0.12763E+00 
c  r12          0.93869E-03      18   0.55476E-08   0.29858E-09 0.60862E+00 
c  r13          0.46676E-02      19   0.71721E-08   0.14900E-08 0.19982E+00 
c  r23          0.39978E-02      19   0.56048E-08   0.13066E-08 0.20123E+00 
c  epsilon      0.10969E+02      11   0.37578E-08   0.10173E-01 0.17010E+00 
c  TempC        0.25716E+06      16   0.15174E-04   0.83958E-02 0.43227E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61373       0.0052573       0.0015074
v  Velocity[Y]            -0.57338         0.54392       0.0030809      0.00087332
v  Velocity[Z]              1.5654          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4392          4.3406          4.3632
v  Pressure                -36.429          360.02          87.642          169.85
v  r11                   0.0010618        0.081909        0.013075        0.018286
v  r22                   0.0011149        0.082625        0.013355        0.018646
v  r33                   0.0016422         0.17433        0.027253        0.037207
v  r12                   -0.010665        0.013613     -0.00023383     -0.00030932
v  r13                   -0.045531        0.052801      9.3262e-05       0.0010139
v  r23                   -0.046701        0.051241      3.0549e-05      0.00057462
v  epsilon                0.069263          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099178      0.00092513       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2777         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71351         0.85283


 TIME FOR THE TIME STEP            10804:        0.68393E+02

===============================================================


 INSTANT    0.108050000E-01   TIME STEP NUMBER           10805
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125918171E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249580873E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.486540018E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.143746186E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.239691793E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81201E-03   0.45181E-02 0.19907E+01 
c  Velocity[X]                                      0.13769E-03 
c  Velocity[Y]                                      0.12762E-03 
c  Velocity[Z]                                      0.42528E-02 
c  Pressure     0.36174E-04     132   0.92098E-02   0.25516E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60462E-08   0.16439E-08 0.99308E-01 
c  r22          0.10852E-01      13   0.47406E-08   0.18459E-08 0.10123E+00 
c  r33          0.21861E-01      15   0.53249E-08   0.12648E-07 0.12713E+00 
c  r12          0.93869E-03      18   0.55383E-08   0.29984E-09 0.60848E+00 
c  r13          0.46676E-02      19   0.63777E-08   0.15202E-08 0.20021E+00 
c  r23          0.39978E-02      19   0.52667E-08   0.12878E-08 0.19833E+00 
c  epsilon      0.10969E+02      11   0.35795E-08   0.10321E-01 0.16817E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.83916E-02 0.43212E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61372       0.0052573       0.0015075
v  Velocity[Y]            -0.57347         0.54395        0.003081      0.00087335
v  Velocity[Z]              1.5657          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4392          4.3406          4.3632
v  Pressure                -36.388          359.99           87.63          169.83
v  r11                   0.0010618        0.081904        0.013075        0.018286
v  r22                   0.0011149        0.082625        0.013355        0.018646
v  r33                   0.0016422         0.17429        0.027253        0.037207
v  r12                   -0.010661        0.013607     -0.00023383     -0.00030932
v  r13                    -0.04553          0.0528      9.3264e-05       0.0010139
v  r23                   -0.046699        0.051222      3.0551e-05      0.00057462
v  epsilon                0.069264          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099178      0.00092514       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2778         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71351         0.85284


 TIME FOR THE TIME STEP            10805:        0.68726E+02

===============================================================


 INSTANT    0.108060000E-01   TIME STEP NUMBER           10806
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.427020133E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.387659846E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.165858188E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.271175078E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.207602707E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81244E-03   0.45394E-02 0.19953E+01 
c  Velocity[X]                                      0.13796E-03 
c  Velocity[Y]                                      0.12889E-03 
c  Velocity[Z]                                      0.42725E-02 
c  Pressure     0.36304E-04     132   0.92488E-02   0.25606E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56146E-08   0.16423E-08 0.99872E-01 
c  r22          0.10852E-01      13   0.44760E-08   0.18420E-08 0.10147E+00 
c  r33          0.21861E-01      15   0.51225E-08   0.12581E-07 0.12772E+00 
c  r12          0.93869E-03      17   0.65997E-08   0.30826E-09 0.61248E+00 
c  r13          0.46676E-02      19   0.57045E-08   0.15224E-08 0.20075E+00 
c  r23          0.39978E-02      19   0.54342E-08   0.13062E-08 0.20119E+00 
c  epsilon      0.10969E+02      11   0.32480E-08   0.96691E-02 0.16354E+00 
c  TempC        0.25716E+06      16   0.15172E-04   0.84397E-02 0.43359E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343          0.6137       0.0052574       0.0015075
v  Velocity[Y]            -0.57347         0.54417       0.0030809      0.00087333
v  Velocity[Z]              1.5656          5.4392          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4392          4.3406          4.3632
v  Pressure                -36.425          359.97          87.624          169.81
v  r11                   0.0010618        0.081898        0.013075        0.018286
v  r22                    0.001115        0.082627        0.013355        0.018646
v  r33                   0.0016422          0.1743        0.027253        0.037207
v  r12                    -0.01066        0.013601     -0.00023383     -0.00030932
v  r13                   -0.045529        0.052801      9.3265e-05       0.0010139
v  r23                   -0.046698         0.05121      3.0552e-05      0.00057462
v  epsilon                0.069264          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099178      0.00092514       0.0017428
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017853           5.277         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71351         0.85284


 TIME FOR THE TIME STEP            10806:        0.68984E+02

===============================================================


 INSTANT    0.108070000E-01   TIME STEP NUMBER           10807
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.286741414E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.498942179E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.456462342E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.257440149E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.666684387E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81271E-03   0.45167E-02 0.19920E+01 
c  Velocity[X]                                      0.13781E-03 
c  Velocity[Y]                                      0.12727E-03 
c  Velocity[Z]                                      0.42516E-02 
c  Pressure     0.36304E-04     133   0.92379E-02   0.25606E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57467E-08   0.17241E-08 0.10185E+00 
c  r22          0.10852E-01      13   0.45257E-08   0.18734E-08 0.10244E+00 
c  r33          0.21861E-01      14   0.70642E-08   0.13091E-07 0.13006E+00 
c  r12          0.93869E-03      18   0.51205E-08   0.30227E-09 0.61127E+00 
c  r13          0.46676E-02      19   0.59028E-08   0.15218E-08 0.20123E+00 
c  r23          0.39978E-02      19   0.53680E-08   0.13330E-08 0.20430E+00 
c  epsilon      0.10969E+02      11   0.33446E-08   0.10244E-01 0.16896E+00 
c  TempC        0.25716E+06      16   0.15107E-04   0.84166E-02 0.43300E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61371       0.0052574       0.0015075
v  Velocity[Y]            -0.57351         0.54426        0.003081      0.00087339
v  Velocity[Z]              1.5655          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4393          4.3406          4.3632
v  Pressure                -36.382          360.06          87.654          169.87
v  r11                   0.0010618        0.081889        0.013075        0.018286
v  r22                    0.001115        0.082629        0.013355        0.018646
v  r33                   0.0016422         0.17432        0.027253        0.037207
v  r12                   -0.010661        0.013595     -0.00023383     -0.00030932
v  r13                   -0.045531        0.052798      9.3265e-05       0.0010139
v  r23                   -0.046697        0.051237      3.0553e-05      0.00057462
v  epsilon                0.069265          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099177      0.00092514       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2772         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71351         0.85284


 TIME FOR THE TIME STEP            10807:        0.69566E+02

===============================================================


 INSTANT    0.108080000E-01   TIME STEP NUMBER           10808
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.493642551E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209092007E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.153187514E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188744324E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.778028373E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81259E-03   0.44813E-02 0.19824E+01 
c  Velocity[X]                                      0.13733E-03 
c  Velocity[Y]                                      0.12752E-03 
c  Velocity[Z]                                      0.42164E-02 
c  Pressure     0.36420E-04     132   0.92693E-02   0.25690E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56469E-08   0.16280E-08 0.99078E-01 
c  r22          0.10852E-01      13   0.45090E-08   0.18401E-08 0.10128E+00 
c  r33          0.21861E-01      14   0.70874E-08   0.12563E-07 0.12708E+00 
c  r12          0.93870E-03      18   0.52567E-08   0.29714E-09 0.60487E+00 
c  r13          0.46676E-02      19   0.56454E-08   0.15144E-08 0.19977E+00 
c  r23          0.39978E-02      18   0.69325E-08   0.12734E-08 0.19813E+00 
c  epsilon      0.10969E+02      11   0.34013E-08   0.10072E-01 0.16864E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.83892E-02 0.43215E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61369       0.0052574       0.0015075
v  Velocity[Y]             -0.5736          0.5441       0.0030809      0.00087336
v  Velocity[Z]              1.5652          5.4393          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4393          4.3406          4.3632
v  Pressure                -36.433          360.08          87.699           169.9
v  r11                   0.0010618        0.081891        0.013075        0.018286
v  r22                    0.001115        0.082629        0.013355        0.018646
v  r33                   0.0016422          0.1743        0.027253        0.037207
v  r12                   -0.010663        0.013589     -0.00023383     -0.00030932
v  r13                   -0.045529        0.052798      9.3265e-05       0.0010139
v  r23                   -0.046697        0.051228      3.0553e-05      0.00057462
v  epsilon                0.069266          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9933e-05       0.0099177      0.00092514       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2769         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71352         0.85284


 TIME FOR THE TIME STEP            10808:        0.68898E+02

===============================================================


 INSTANT    0.108090000E-01   TIME STEP NUMBER           10809
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.394775815E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.741795001E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161494143E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935011E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.144423616E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.216966742E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81128E-03   0.45513E-02 0.19975E+01 
c  Velocity[X]                                      0.13763E-03 
c  Velocity[Y]                                      0.12817E-03 
c  Velocity[Z]                                      0.42855E-02 
c  Pressure     0.36531E-04     133   0.92987E-02   0.25767E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58771E-08   0.16841E-08 0.10138E+00 
c  r22          0.10852E-01      13   0.46662E-08   0.18498E-08 0.10199E+00 
c  r33          0.21861E-01      15   0.60033E-08   0.12789E-07 0.12886E+00 
c  r12          0.93870E-03      18   0.57674E-08   0.30211E-09 0.61070E+00 
c  r13          0.46676E-02      19   0.59795E-08   0.15043E-08 0.20009E+00 
c  r23          0.39978E-02      19   0.56778E-08   0.13055E-08 0.20199E+00 
c  epsilon      0.10969E+02      11   0.36425E-08   0.10071E-01 0.16999E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.84422E-02 0.43313E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61371       0.0052574       0.0015075
v  Velocity[Y]            -0.57372         0.54405        0.003081      0.00087339
v  Velocity[Z]              1.5652          5.4393          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4393          4.3406          4.3632
v  Pressure                -36.374          360.02           87.63          169.84
v  r11                   0.0010618        0.081887        0.013075        0.018286
v  r22                    0.001115        0.082631        0.013355        0.018646
v  r33                   0.0016422         0.17427        0.027253        0.037207
v  r12                   -0.010662        0.013589     -0.00023383     -0.00030932
v  r13                   -0.045529        0.052799      9.3265e-05       0.0010139
v  r23                   -0.046697         0.05121      3.0553e-05      0.00057462
v  epsilon                0.069267          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099176      0.00092514       0.0017428
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2772         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71351         0.85284


 TIME FOR THE TIME STEP            10809:        0.69193E+02

===============================================================


 INSTANT    0.108100000E-01   TIME STEP NUMBER           10810
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.451974368E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.410197833E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.567828845E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.826387045E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.127033238E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81390E-03   0.44906E-02 0.19858E+01 
c  Velocity[X]                                      0.13686E-03 
c  Velocity[Y]                                      0.12810E-03 
c  Velocity[Z]                                      0.42256E-02 
c  Pressure     0.36153E-04     131   0.92041E-02   0.25500E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60595E-08   0.16428E-08 0.99139E-01 
c  r22          0.10852E-01      13   0.49531E-08   0.18448E-08 0.10130E+00 
c  r33          0.21861E-01      15   0.53132E-08   0.12697E-07 0.12711E+00 
c  r12          0.93870E-03      18   0.55328E-08   0.29789E-09 0.60481E+00 
c  r13          0.46676E-02      19   0.56464E-08   0.14957E-08 0.19902E+00 
c  r23          0.39978E-02      18   0.65946E-08   0.12885E-08 0.19850E+00 
c  epsilon      0.10969E+02      11   0.35780E-08   0.10207E-01 0.16679E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.83336E-02 0.43033E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61371       0.0052574       0.0015075
v  Velocity[Y]            -0.57374         0.54413        0.003081      0.00087339
v  Velocity[Z]              1.5652          5.4392          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4392          4.3406          4.3632
v  Pressure                -36.407          359.99          87.628          169.82
v  r11                   0.0010618        0.081887        0.013075        0.018286
v  r22                    0.001115        0.082633        0.013355        0.018646
v  r33                   0.0016423         0.17428        0.027253        0.037207
v  r12                   -0.010661        0.013591     -0.00023383     -0.00030932
v  r13                   -0.045531        0.052799      9.3265e-05       0.0010139
v  r23                   -0.046697        0.051233      3.0554e-05      0.00057462
v  epsilon                0.069268           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099176      0.00092514       0.0017428
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            10810:        0.70381E+02

===============================================================


 INSTANT    0.108110000E-01   TIME STEP NUMBER           10811
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.148028916E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.165604993E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.956432645E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.155660160E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.142481806E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81223E-03   0.45148E-02 0.19892E+01 
c  Velocity[X]                                      0.13793E-03 
c  Velocity[Y]                                      0.12853E-03 
c  Velocity[Z]                                      0.42483E-02 
c  Pressure     0.36266E-04     132   0.92315E-02   0.25578E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58281E-08   0.16280E-08 0.99106E-01 
c  r22          0.10852E-01      13   0.48788E-08   0.18191E-08 0.10090E+00 
c  r33          0.21861E-01      14   0.70748E-08   0.12419E-07 0.12644E+00 
c  r12          0.93870E-03      18   0.54706E-08   0.30397E-09 0.60685E+00 
c  r13          0.46676E-02      19   0.62933E-08   0.14914E-08 0.19861E+00 
c  r23          0.39978E-02      18   0.65734E-08   0.12851E-08 0.19805E+00 
c  epsilon      0.10969E+02      11   0.33324E-08   0.96843E-02 0.16286E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.83687E-02 0.43189E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349          0.6137       0.0052574       0.0015075
v  Velocity[Y]            -0.57385         0.54423        0.003081      0.00087338
v  Velocity[Z]              1.5653          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4393          4.3406          4.3632
v  Pressure                -36.409          360.04          87.662          169.87
v  r11                   0.0010618        0.081897        0.013075        0.018286
v  r22                    0.001115        0.082629        0.013355        0.018646
v  r33                   0.0016423         0.17431        0.027253        0.037207
v  r12                   -0.010665        0.013587     -0.00023383     -0.00030932
v  r13                   -0.045529          0.0528      9.3265e-05       0.0010139
v  r23                   -0.046696        0.051226      3.0555e-05      0.00057463
v  epsilon                0.069269          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099176      0.00092514       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2785         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71351         0.85284


 TIME FOR THE TIME STEP            10811:        0.69085E+02

===============================================================


 INSTANT    0.108120000E-01   TIME STEP NUMBER           10812
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.537766185E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.348241054E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.339200652E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.148229590E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.362242661E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81196E-03   0.45121E-02 0.19914E+01 
c  Velocity[X]                                      0.13814E-03 
c  Velocity[Y]                                      0.12712E-03 
c  Velocity[Z]                                      0.42468E-02 
c  Pressure     0.36441E-04     133   0.92808E-02   0.25704E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55895E-08   0.16244E-08 0.99547E-01 
c  r22          0.10852E-01      13   0.47518E-08   0.18295E-08 0.10176E+00 
c  r33          0.21861E-01      15   0.59374E-08   0.12516E-07 0.12743E+00 
c  r12          0.93870E-03      18   0.53780E-08   0.30424E-09 0.60811E+00 
c  r13          0.46676E-02      19   0.61300E-08   0.15087E-08 0.20075E+00 
c  r23          0.39978E-02      18   0.67303E-08   0.12711E-08 0.19807E+00 
c  epsilon      0.10969E+02      11   0.33694E-08   0.99408E-02 0.16642E+00 
c  TempC        0.25716E+06      16   0.15164E-04   0.84445E-02 0.43382E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63335         0.61374       0.0052574       0.0015075
v  Velocity[Y]            -0.57374         0.54408        0.003081      0.00087338
v  Velocity[Z]              1.5652          5.4393          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4393          4.3406          4.3632
v  Pressure                -36.435          360.07          87.681          169.89
v  r11                   0.0010618        0.081905        0.013075        0.018286
v  r22                    0.001115        0.082631        0.013355        0.018646
v  r33                   0.0016423         0.17434        0.027253        0.037207
v  r12                   -0.010666        0.013582     -0.00023383     -0.00030932
v  r13                   -0.045528        0.052801      9.3264e-05       0.0010139
v  r23                   -0.046696        0.051215      3.0555e-05      0.00057462
v  epsilon                 0.06927          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099176      0.00092514       0.0017428
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71351         0.85284


 TIME FOR THE TIME STEP            10812:        0.70173E+02

===============================================================


 INSTANT    0.108130000E-01   TIME STEP NUMBER           10813
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.143938601E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69752E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117945712E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69752E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.213877100E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69752E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.362066357E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69752E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.765502119E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69752E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81286E-03   0.44956E-02 0.19857E+01 
c  Velocity[X]                                      0.13824E-03 
c  Velocity[Y]                                      0.12777E-03 
c  Velocity[Z]                                      0.42296E-02 
c  Pressure     0.36154E-04     132   0.92052E-02   0.25501E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55806E-08   0.16449E-08 0.10026E+00 
c  r22          0.10852E-01      13   0.47691E-08   0.18265E-08 0.10163E+00 
c  r33          0.21861E-01      14   0.67891E-08   0.12532E-07 0.12792E+00 
c  r12          0.93870E-03      18   0.58084E-08   0.29373E-09 0.60411E+00 
c  r13          0.46676E-02      19   0.57971E-08   0.14970E-08 0.20040E+00 
c  r23          0.39978E-02      19   0.53179E-08   0.12763E-08 0.19988E+00 
c  epsilon      0.10969E+02      11   0.32414E-08   0.98188E-02 0.16540E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.83725E-02 0.43192E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61374       0.0052574       0.0015075
v  Velocity[Y]            -0.57369         0.54406        0.003081      0.00087338
v  Velocity[Z]              1.5654          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4393          4.3406          4.3632
v  Pressure                -36.378          360.04          87.645          169.85
v  r11                   0.0010618        0.081913        0.013075        0.018286
v  r22                    0.001115        0.082633        0.013355        0.018646
v  r33                   0.0016423         0.17433        0.027253        0.037207
v  r12                   -0.010667        0.013585     -0.00023384     -0.00030932
v  r13                   -0.045532        0.052801      9.3264e-05       0.0010139
v  r23                   -0.046695        0.051227      3.0555e-05      0.00057462
v  epsilon                 0.06927          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099176      0.00092514       0.0017428
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71351         0.85283


 TIME FOR THE TIME STEP            10813:        0.68557E+02

===============================================================


 INSTANT    0.108140000E-01   TIME STEP NUMBER           10814
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.253815323E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.725414257E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184351668E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.103626749E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.580337918E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81234E-03   0.45139E-02 0.19904E+01 
c  Velocity[X]                                      0.13759E-03 
c  Velocity[Y]                                      0.12846E-03 
c  Velocity[Z]                                      0.42478E-02 
c  Pressure     0.36102E-04     132   0.91958E-02   0.25465E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53843E-08   0.16196E-08 0.99016E-01 
c  r22          0.10852E-01      13   0.49714E-08   0.18346E-08 0.10139E+00 
c  r33          0.21861E-01      14   0.67082E-08   0.12499E-07 0.12700E+00 
c  r12          0.93870E-03      18   0.52275E-08   0.29266E-09 0.60275E+00 
c  r13          0.46676E-02      19   0.57191E-08   0.15111E-08 0.19971E+00 
c  r23          0.39978E-02      18   0.65741E-08   0.12778E-08 0.19897E+00 
c  epsilon      0.10969E+02      11   0.32452E-08   0.99201E-02 0.16651E+00 
c  TempC        0.25716E+06      16   0.15178E-04   0.84420E-02 0.43298E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61371       0.0052574       0.0015075
v  Velocity[Y]             -0.5736         0.54414       0.0030809      0.00087332
v  Velocity[Z]              1.5652          5.4393          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4393          4.3406          4.3632
v  Pressure                -36.453          360.02          87.644          169.84
v  r11                   0.0010618         0.08191        0.013075        0.018286
v  r22                    0.001115        0.082634        0.013355        0.018646
v  r33                   0.0016423         0.17428        0.027253        0.037207
v  r12                   -0.010666        0.013584     -0.00023384     -0.00030932
v  r13                   -0.045529        0.052804      9.3264e-05       0.0010139
v  r23                   -0.046695        0.051214      3.0556e-05      0.00057462
v  epsilon                0.069271           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099177      0.00092514       0.0017428
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71351         0.85284


 TIME FOR THE TIME STEP            10814:        0.68562E+02

===============================================================


 INSTANT    0.108150000E-01   TIME STEP NUMBER           10815
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.305460848E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.549725489E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.176917046E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.234735674E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.961671914E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81255E-03   0.45252E-02 0.19911E+01 
c  Velocity[X]                                      0.13765E-03 
c  Velocity[Y]                                      0.12774E-03 
c  Velocity[Z]                                      0.42598E-02 
c  Pressure     0.36344E-04     133   0.92506E-02   0.25634E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50383E-08   0.16341E-08 0.99706E-01 
c  r22          0.10852E-01      13   0.47819E-08   0.18213E-08 0.10100E+00 
c  r33          0.21861E-01      15   0.50826E-08   0.12523E-07 0.12729E+00 
c  r12          0.93870E-03      18   0.49229E-08   0.29193E-09 0.60031E+00 
c  r13          0.46676E-02      19   0.58101E-08   0.14892E-08 0.19921E+00 
c  r23          0.39978E-02      19   0.55687E-08   0.12798E-08 0.20035E+00 
c  epsilon      0.10969E+02      11   0.32505E-08   0.10008E-01 0.16936E+00 
c  TempC        0.25716E+06      16   0.15101E-04   0.84563E-02 0.43359E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162021


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61373       0.0052574       0.0015075
v  Velocity[Y]            -0.57372          0.5443       0.0030809      0.00087335
v  Velocity[Z]              1.5653          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4393          4.3406          4.3632
v  Pressure                -36.387          360.05          87.658          169.87
v  r11                   0.0010618        0.081917        0.013075        0.018286
v  r22                    0.001115        0.082635        0.013355        0.018646
v  r33                   0.0016423         0.17429        0.027253        0.037207
v  r12                   -0.010663         0.01358     -0.00023383     -0.00030932
v  r13                   -0.045528        0.052802      9.3264e-05       0.0010139
v  r23                   -0.046695        0.051206      3.0557e-05      0.00057463
v  epsilon                0.069272           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099179      0.00092514       0.0017428
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2777         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            10815:        0.69650E+02

===============================================================


 INSTANT    0.108160000E-01   TIME STEP NUMBER           10816
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.376706314E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108737204E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.335375353E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.398654206E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.368984531E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81259E-03   0.44817E-02 0.19836E+01 
c  Velocity[X]                                      0.13692E-03 
c  Velocity[Y]                                      0.12681E-03 
c  Velocity[Z]                                      0.42180E-02 
c  Pressure     0.36515E-04     133   0.92994E-02   0.25755E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52900E-08   0.16261E-08 0.99135E-01 
c  r22          0.10852E-01      13   0.51099E-08   0.18322E-08 0.10150E+00 
c  r33          0.21861E-01      15   0.52853E-08   0.12539E-07 0.12719E+00 
c  r12          0.93870E-03      18   0.57369E-08   0.29617E-09 0.60277E+00 
c  r13          0.46676E-02      19   0.65271E-08   0.14883E-08 0.19933E+00 
c  r23          0.39978E-02      18   0.69527E-08   0.12781E-08 0.19928E+00 
c  epsilon      0.10969E+02      11   0.34970E-08   0.98887E-02 0.16522E+00 
c  TempC        0.25716E+06      16   0.15178E-04   0.84151E-02 0.43324E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162015


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61373       0.0052574       0.0015075
v  Velocity[Y]             -0.5735         0.54412       0.0030809      0.00087331
v  Velocity[Z]              1.5653          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4393          4.3406          4.3632
v  Pressure                -36.416          360.01          87.641          169.83
v  r11                   0.0010618        0.081915        0.013075        0.018286
v  r22                    0.001115        0.082635        0.013355        0.018646
v  r33                   0.0016423         0.17432        0.027253        0.037207
v  r12                   -0.010664        0.013576     -0.00023384     -0.00030932
v  r13                   -0.045531        0.052804      9.3264e-05       0.0010139
v  r23                   -0.046695        0.051197      3.0556e-05      0.00057462
v  epsilon                0.069273          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05        0.009918      0.00092514       0.0017428
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017853          5.2774         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71351         0.85283


 TIME FOR THE TIME STEP            10816:        0.71597E+02

===============================================================


 INSTANT    0.108170000E-01   TIME STEP NUMBER           10817
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.706331884E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.898191007E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.992915608E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.433829511E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.744270724E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81170E-03   0.45114E-02 0.19904E+01 
c  Velocity[X]                                      0.13705E-03 
c  Velocity[Y]                                      0.12801E-03 
c  Velocity[Z]                                      0.42463E-02 
c  Pressure     0.35996E-04     133   0.91625E-02   0.25390E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51383E-08   0.16415E-08 0.99215E-01 
c  r22          0.10852E-01      13   0.53980E-08   0.18257E-08 0.10105E+00 
c  r33          0.21861E-01      15   0.57471E-08   0.12560E-07 0.12678E+00 
c  r12          0.93870E-03      18   0.51138E-08   0.30772E-09 0.60678E+00 
c  r13          0.46677E-02      19   0.57406E-08   0.15110E-08 0.19967E+00 
c  r23          0.39978E-02      19   0.58512E-08   0.12995E-08 0.19942E+00 
c  epsilon      0.10969E+02      11   0.35788E-08   0.10004E-01 0.16557E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.83648E-02 0.43168E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61372       0.0052574       0.0015075
v  Velocity[Y]             -0.5736         0.54405       0.0030809      0.00087329
v  Velocity[Z]              1.5653          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4393          4.3406          4.3632
v  Pressure                -36.385          359.98          87.627          169.82
v  r11                   0.0010618        0.081916        0.013075        0.018286
v  r22                    0.001115        0.082636        0.013355        0.018646
v  r33                   0.0016423          0.1743        0.027253        0.037207
v  r12                   -0.010662        0.013577     -0.00023384     -0.00030932
v  r13                    -0.04553        0.052804      9.3264e-05       0.0010139
v  r23                   -0.046695        0.051227      3.0556e-05      0.00057462
v  epsilon                0.069274          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099181      0.00092514       0.0017428
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2777         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71351         0.85283


 TIME FOR THE TIME STEP            10817:        0.69954E+02

===============================================================


 INSTANT    0.108180000E-01   TIME STEP NUMBER           10818
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.394496211E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.241835688E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150447621E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.405224642E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.963325870E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81280E-03   0.45235E-02 0.19925E+01 
c  Velocity[X]                                      0.13794E-03 
c  Velocity[Y]                                      0.12832E-03 
c  Velocity[Z]                                      0.42572E-02 
c  Pressure     0.36379E-04     134   0.92595E-02   0.25660E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56789E-08   0.16315E-08 0.98751E-01 
c  r22          0.10852E-01      13   0.57239E-08   0.18256E-08 0.10068E+00 
c  r33          0.21861E-01      15   0.69765E-08   0.12577E-07 0.12631E+00 
c  r12          0.93870E-03      18   0.60230E-08   0.29932E-09 0.60123E+00 
c  r13          0.46676E-02      19   0.61461E-08   0.14988E-08 0.19889E+00 
c  r23          0.39978E-02      19   0.65337E-08   0.12784E-08 0.19717E+00 
c  epsilon      0.10969E+02      11   0.36002E-08   0.10284E-01 0.16845E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84225E-02 0.43297E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61373       0.0052574       0.0015075
v  Velocity[Y]            -0.57348         0.54417       0.0030809      0.00087332
v  Velocity[Z]              1.5655          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4393          4.3406          4.3632
v  Pressure                -36.408          360.05          87.688          169.89
v  r11                   0.0010618        0.081918        0.013075        0.018286
v  r22                    0.001115        0.082636        0.013355        0.018646
v  r33                   0.0016423         0.17427        0.027253        0.037207
v  r12                   -0.010662        0.013578     -0.00023384     -0.00030932
v  r13                   -0.045528        0.052805      9.3265e-05       0.0010139
v  r23                   -0.046695        0.051211      3.0557e-05      0.00057462
v  epsilon                0.069275          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099181      0.00092515       0.0017428
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2779         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71351         0.85283


 TIME FOR THE TIME STEP            10818:        0.70167E+02

===============================================================


 INSTANT    0.108190000E-01   TIME STEP NUMBER           10819
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.978517270E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119855037E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.376961707E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.948275750E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.496839778E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81293E-03   0.45117E-02 0.19885E+01 
c  Velocity[X]                                      0.13790E-03 
c  Velocity[Y]                                      0.12737E-03 
c  Velocity[Z]                                      0.42464E-02 
c  Pressure     0.36215E-04     136   0.92252E-02   0.25544E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55940E-08   0.16120E-08 0.98644E-01 
c  r22          0.10852E-01      13   0.58463E-08   0.18011E-08 0.10094E+00 
c  r33          0.21861E-01      16   0.61684E-08   0.12268E-07 0.12611E+00 
c  r12          0.93870E-03      18   0.71379E-08   0.29480E-09 0.59991E+00 
c  r13          0.46677E-02      19   0.63105E-08   0.14824E-08 0.19920E+00 
c  r23          0.39978E-02      19   0.74079E-08   0.12616E-08 0.19726E+00 
c  epsilon      0.10969E+02      11   0.35998E-08   0.97025E-02 0.16483E+00 
c  TempC        0.25716E+06      16   0.15124E-04   0.84198E-02 0.43268E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63336         0.61373       0.0052574       0.0015075
v  Velocity[Y]            -0.57361         0.54424       0.0030809      0.00087332
v  Velocity[Z]              1.5651          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4393          4.3406          4.3632
v  Pressure                -36.388             360          87.631          169.84
v  r11                   0.0010618        0.081915        0.013075        0.018286
v  r22                    0.001115         0.08263        0.013355        0.018646
v  r33                   0.0016423         0.17428        0.027253        0.037207
v  r12                   -0.010662        0.013576     -0.00023384     -0.00030932
v  r13                   -0.045531        0.052803      9.3264e-05       0.0010139
v  r23                   -0.046695        0.051201      3.0557e-05      0.00057462
v  epsilon                0.069276          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099178      0.00092515       0.0017428
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2777         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            10819:        0.69738E+02

===============================================================


 INSTANT    0.108200000E-01   TIME STEP NUMBER           10820
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.747631851E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.175546507E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.310901850E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.147087979E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.262594521E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81148E-03   0.44874E-02 0.19860E+01 
c  Velocity[X]                                      0.13753E-03 
c  Velocity[Y]                                      0.12727E-03 
c  Velocity[Z]                                      0.42226E-02 
c  Pressure     0.36133E-04     134   0.91978E-02   0.25487E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56312E-08   0.16149E-08 0.98832E-01 
c  r22          0.10852E-01      13   0.57214E-08   0.18280E-08 0.10122E+00 
c  r33          0.21861E-01      15   0.57650E-08   0.12433E-07 0.12657E+00 
c  r12          0.93870E-03      18   0.66060E-08   0.29654E-09 0.60254E+00 
c  r13          0.46677E-02      19   0.59657E-08   0.15097E-08 0.20002E+00 
c  r23          0.39978E-02      19   0.67374E-08   0.12682E-08 0.19778E+00 
c  epsilon      0.10969E+02      11   0.32679E-08   0.10066E-01 0.16816E+00 
c  TempC        0.25716E+06      16   0.15155E-04   0.84123E-02 0.43303E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63335         0.61372       0.0052574       0.0015075
v  Velocity[Y]            -0.57362         0.54434       0.0030809      0.00087329
v  Velocity[Z]              1.5652          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4393          4.3406          4.3632
v  Pressure                -36.417             360          87.653          169.84
v  r11                   0.0010618        0.081919        0.013075        0.018286
v  r22                    0.001115         0.08263        0.013355        0.018646
v  r33                   0.0016423         0.17429        0.027253        0.037207
v  r12                   -0.010662        0.013574     -0.00023384     -0.00030932
v  r13                   -0.045529        0.052803      9.3265e-05       0.0010139
v  r23                   -0.046695         0.05122      3.0558e-05      0.00057463
v  epsilon                0.069277          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099179      0.00092515       0.0017428
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2786         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            10820:        0.69340E+02

===============================================================


 INSTANT    0.108210000E-01   TIME STEP NUMBER           10821
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.278282739E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.983719882E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.266315400E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.112040379E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.109870978E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81253E-03   0.45154E-02 0.19917E+01 
c  Velocity[X]                                      0.13766E-03 
c  Velocity[Y]                                      0.12843E-03 
c  Velocity[Z]                                      0.42493E-02 
c  Pressure     0.36301E-04     133   0.92422E-02   0.25604E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58408E-08   0.16407E-08 0.99817E-01 
c  r22          0.10852E-01      13   0.57286E-08   0.17700E-08 0.10044E+00 
c  r33          0.21861E-01      15   0.55951E-08   0.12322E-07 0.12660E+00 
c  r12          0.93870E-03      18   0.68965E-08   0.29464E-09 0.60327E+00 
c  r13          0.46677E-02      19   0.59048E-08   0.14750E-08 0.19897E+00 
c  r23          0.39978E-02      20   0.61684E-08   0.12837E-08 0.19936E+00 
c  epsilon      0.10969E+02      11   0.33680E-08   0.99405E-02 0.16966E+00 
c  TempC        0.25716E+06      16   0.15155E-04   0.83872E-02 0.43273E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61374       0.0052575       0.0015075
v  Velocity[Y]            -0.57364         0.54414        0.003081      0.00087334
v  Velocity[Z]              1.5652          5.4393          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4393          4.3406          4.3632
v  Pressure                -36.367          360.05          87.658          169.87
v  r11                   0.0010618         0.08192        0.013075        0.018286
v  r22                    0.001115        0.082631        0.013355        0.018646
v  r33                   0.0016424         0.17433        0.027253        0.037207
v  r12                   -0.010663        0.013577     -0.00023384     -0.00030932
v  r13                   -0.045529        0.052803      9.3266e-05       0.0010139
v  r23                   -0.046695        0.051208      3.0559e-05      0.00057463
v  epsilon                0.069278          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9929e-05        0.009918      0.00092515       0.0017428
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2792         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8792         0.71352         0.85284


 TIME FOR THE TIME STEP            10821:        0.71408E+02

===============================================================


 INSTANT    0.108220000E-01   TIME STEP NUMBER           10822
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.925260114E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.921356923E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169543768E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.378496892E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.107466815E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81365E-03   0.44962E-02 0.19872E+01 
c  Velocity[X]                                      0.13761E-03 
c  Velocity[Y]                                      0.12786E-03 
c  Velocity[Z]                                      0.42307E-02 
c  Pressure     0.36471E-04     131   0.92812E-02   0.25723E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59647E-08   0.16185E-08 0.98932E-01 
c  r22          0.10852E-01      13   0.58222E-08   0.18321E-08 0.10160E+00 
c  r33          0.21861E-01      15   0.62483E-08   0.12378E-07 0.12672E+00 
c  r12          0.93870E-03      19   0.58221E-08   0.29596E-09 0.60281E+00 
c  r13          0.46677E-02      19   0.56112E-08   0.14787E-08 0.19987E+00 
c  r23          0.39978E-02      19   0.61072E-08   0.12558E-08 0.19731E+00 
c  epsilon      0.10969E+02      11   0.34820E-08   0.98816E-02 0.16550E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.84153E-02 0.43280E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61374       0.0052574       0.0015075
v  Velocity[Y]            -0.57353         0.54423       0.0030809      0.00087329
v  Velocity[Z]              1.5653          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4393          4.3406          4.3632
v  Pressure                -36.421          360.07          87.683          169.89
v  r11                   0.0010618         0.08192        0.013075        0.018286
v  r22                    0.001115        0.082632        0.013355        0.018646
v  r33                   0.0016424         0.17432        0.027253        0.037207
v  r12                   -0.010663        0.013577     -0.00023384     -0.00030932
v  r13                   -0.045531        0.052802      9.3265e-05       0.0010139
v  r23                   -0.046696        0.051195       3.056e-05      0.00057463
v  epsilon                0.069279          271.25          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05        0.009918      0.00092515       0.0017428
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2795         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8795         0.71351         0.85284


 TIME FOR THE TIME STEP            10822:        0.70754E+02

===============================================================


 INSTANT    0.108230000E-01   TIME STEP NUMBER           10823
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.139161062E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.121190921E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157647024E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.180352530E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.202744457E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81209E-03   0.45145E-02 0.19881E+01 
c  Velocity[X]                                      0.13804E-03 
c  Velocity[Y]                                      0.12759E-03 
c  Velocity[Z]                                      0.42489E-02 
c  Pressure     0.35963E-04     133   0.91632E-02   0.25367E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61964E-08   0.16176E-08 0.98426E-01 
c  r22          0.10852E-01      13   0.57153E-08   0.18281E-08 0.10067E+00 
c  r33          0.21861E-01      15   0.67252E-08   0.12418E-07 0.12608E+00 
c  r12          0.93870E-03      19   0.53630E-08   0.29744E-09 0.60310E+00 
c  r13          0.46677E-02      19   0.56196E-08   0.14941E-08 0.19911E+00 
c  r23          0.39978E-02      19   0.69105E-08   0.12626E-08 0.19740E+00 
c  epsilon      0.10969E+02      11   0.35931E-08   0.10058E-01 0.16625E+00 
c  TempC        0.25716E+06      16   0.15121E-04   0.84275E-02 0.43302E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63354         0.61374       0.0052573       0.0015075
v  Velocity[Y]            -0.57364         0.54439       0.0030809       0.0008733
v  Velocity[Z]              1.5652          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4393          4.3406          4.3632
v  Pressure                -36.381          360.02           87.66          169.85
v  r11                   0.0010618        0.081919        0.013075        0.018286
v  r22                    0.001115        0.082631        0.013355        0.018646
v  r33                   0.0016424         0.17428        0.027253        0.037207
v  r12                   -0.010668        0.013574     -0.00023384     -0.00030932
v  r13                   -0.045529        0.052799      9.3265e-05       0.0010139
v  r23                   -0.046696         0.05121       3.056e-05      0.00057463
v  epsilon                 0.06928           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099179      0.00092515       0.0017428
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2786         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            10823:        0.68313E+02

===============================================================


 INSTANT    0.108240000E-01   TIME STEP NUMBER           10824
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.163435789E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.290355495E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.348949035E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935012E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129342726E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169286686E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81232E-03   0.44859E-02 0.19858E+01 
c  Velocity[X]                                      0.13703E-03 
c  Velocity[Y]                                      0.12776E-03 
c  Velocity[Z]                                      0.42211E-02 
c  Pressure     0.36287E-04     131   0.92286E-02   0.25594E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58087E-08   0.16210E-08 0.98491E-01 
c  r22          0.10852E-01      13   0.53205E-08   0.18195E-08 0.10056E+00 
c  r33          0.21861E-01      15   0.62572E-08   0.12482E-07 0.12622E+00 
c  r12          0.93870E-03      18   0.69244E-08   0.29591E-09 0.59894E+00 
c  r13          0.46677E-02      19   0.62764E-08   0.15262E-08 0.20023E+00 
c  r23          0.39978E-02      20   0.65094E-08   0.12822E-08 0.19780E+00 
c  epsilon      0.10969E+02      11   0.35305E-08   0.10105E-01 0.16786E+00 
c  TempC        0.25716E+06      16   0.15181E-04   0.84022E-02 0.43235E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61374       0.0052574       0.0015074
v  Velocity[Y]            -0.57353         0.54426        0.003081      0.00087334
v  Velocity[Z]              1.5651          5.4393          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4393          4.3406          4.3632
v  Pressure                -36.399             360          87.642          169.84
v  r11                   0.0010618        0.081915        0.013075        0.018286
v  r22                    0.001115        0.082631        0.013355        0.018646
v  r33                   0.0016424         0.17429        0.027253        0.037207
v  r12                    -0.01067        0.013583     -0.00023384     -0.00030932
v  r13                   -0.045528        0.052798      9.3265e-05       0.0010139
v  r23                   -0.046696        0.051194       3.056e-05      0.00057463
v  epsilon                0.069281           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099179      0.00092515       0.0017428
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2779         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71351         0.85283


 TIME FOR THE TIME STEP            10824:        0.69486E+02

===============================================================


 INSTANT    0.108250000E-01   TIME STEP NUMBER           10825
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.489234511E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.262221629E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.217609410E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.371070677E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.480385608E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81302E-03   0.45233E-02 0.19914E+01 
c  Velocity[X]                                      0.13793E-03 
c  Velocity[Y]                                      0.12834E-03 
c  Velocity[Z]                                      0.42570E-02 
c  Pressure     0.36279E-04     132   0.92387E-02   0.25589E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51519E-08   0.16259E-08 0.98530E-01 
c  r22          0.10852E-01      13   0.56663E-08   0.18067E-08 0.10053E+00 
c  r33          0.21861E-01      15   0.55497E-08   0.12365E-07 0.12592E+00 
c  r12          0.93870E-03      18   0.70362E-08   0.29120E-09 0.59569E+00 
c  r13          0.46677E-02      19   0.66777E-08   0.14708E-08 0.19794E+00 
c  r23          0.39978E-02      20   0.69527E-08   0.12793E-08 0.19771E+00 
c  epsilon      0.10969E+02      11   0.33421E-08   0.98558E-02 0.16608E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83538E-02 0.43110E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61375       0.0052573       0.0015075
v  Velocity[Y]            -0.57367         0.54418        0.003081      0.00087333
v  Velocity[Z]              1.5653          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4393          4.3406          4.3632
v  Pressure                -36.371          360.09          87.687          169.91
v  r11                   0.0010618        0.081912        0.013075        0.018286
v  r22                    0.001115        0.082626        0.013355        0.018646
v  r33                   0.0016424         0.17432        0.027253        0.037207
v  r12                   -0.010669        0.013584     -0.00023384     -0.00030932
v  r13                   -0.045532        0.052799      9.3266e-05       0.0010139
v  r23                   -0.046696        0.051186      3.0561e-05      0.00057463
v  epsilon                0.069281          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099178      0.00092515       0.0017428
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2773         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            10825:        0.71138E+02

===============================================================


 INSTANT    0.108260000E-01   TIME STEP NUMBER           10826
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122292781E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.709687814E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161302940E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.299084498E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.684071804E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81282E-03   0.45186E-02 0.19905E+01 
c  Velocity[X]                                      0.13746E-03 
c  Velocity[Y]                                      0.12782E-03 
c  Velocity[Z]                                      0.42534E-02 
c  Pressure     0.36194E-04     134   0.92147E-02   0.25530E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50620E-08   0.16228E-08 0.98433E-01 
c  r22          0.10852E-01      13   0.55405E-08   0.18358E-08 0.10079E+00 
c  r33          0.21861E-01      15   0.58104E-08   0.12452E-07 0.12582E+00 
c  r12          0.93870E-03      18   0.65609E-08   0.29603E-09 0.60169E+00 
c  r13          0.46677E-02      19   0.66652E-08   0.15045E-08 0.19913E+00 
c  r23          0.39978E-02      20   0.57790E-08   0.12753E-08 0.19728E+00 
c  epsilon      0.10969E+02      10   0.53992E-08   0.10023E-01 0.16513E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.83896E-02 0.43228E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61373       0.0052574       0.0015075
v  Velocity[Y]             -0.5737          0.5443       0.0030809      0.00087331
v  Velocity[Z]              1.5653          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4393          4.3406          4.3632
v  Pressure                 -36.43          360.01          87.644          169.84
v  r11                   0.0010618         0.08191        0.013075        0.018286
v  r22                   0.0011151        0.082626        0.013355        0.018646
v  r33                   0.0016424         0.17429        0.027253        0.037207
v  r12                   -0.010669        0.013585     -0.00023384     -0.00030932
v  r13                   -0.045528        0.052798      9.3266e-05       0.0010139
v  r23                   -0.046696        0.051212      3.0561e-05      0.00057463
v  epsilon                0.069282          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.991e-05       0.0099178      0.00092515       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2777         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71351         0.85284


 TIME FOR THE TIME STEP            10826:        0.71329E+02

===============================================================


 INSTANT    0.108270000E-01   TIME STEP NUMBER           10827
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120085786E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69745E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.123392116E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69745E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.525049225E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69745E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.665282794E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69745E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.128771929E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69745E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81202E-03   0.45272E-02 0.19914E+01 
c  Velocity[X]                                      0.13869E-03 
c  Velocity[Y]                                      0.12735E-03 
c  Velocity[Z]                                      0.42612E-02 
c  Pressure     0.36403E-04     133   0.92709E-02   0.25675E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55389E-08   0.16364E-08 0.99153E-01 
c  r22          0.10852E-01      13   0.57585E-08   0.18078E-08 0.10068E+00 
c  r33          0.21861E-01      15   0.51690E-08   0.12469E-07 0.12667E+00 
c  r12          0.93870E-03      18   0.68280E-08   0.29055E-09 0.59986E+00 
c  r13          0.46677E-02      19   0.62418E-08   0.14867E-08 0.19882E+00 
c  r23          0.39978E-02      20   0.57477E-08   0.12897E-08 0.19996E+00 
c  epsilon      0.10969E+02      11   0.32057E-08   0.10093E-01 0.17122E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.84510E-02 0.43382E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61376       0.0052574       0.0015075
v  Velocity[Y]            -0.57378         0.54441       0.0030809      0.00087331
v  Velocity[Z]              1.5654          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4393          4.3406          4.3632
v  Pressure                -36.393          360.01          87.638          169.84
v  r11                   0.0010618        0.081911        0.013075        0.018286
v  r22                   0.0011151        0.082626        0.013355        0.018646
v  r33                   0.0016424         0.17427        0.027253        0.037207
v  r12                   -0.010668        0.013591     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052796      9.3266e-05       0.0010139
v  r23                   -0.046696        0.051201      3.0561e-05      0.00057463
v  epsilon                0.069283          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9908e-05       0.0099179      0.00092515       0.0017428
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017854           5.278         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71351         0.85283


 TIME FOR THE TIME STEP            10827:        0.73103E+02

===============================================================


 INSTANT    0.108280000E-01   TIME STEP NUMBER           10828
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.182557897E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69744E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.331593874E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69744E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.218662138E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69744E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226670093E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69744E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.307812949E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69744E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81338E-03   0.44915E-02 0.19849E+01 
c  Velocity[X]                                      0.13706E-03 
c  Velocity[Y]                                      0.12870E-03 
c  Velocity[Z]                                      0.42257E-02 
c  Pressure     0.36200E-04     133   0.92150E-02   0.25533E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58984E-08   0.16340E-08 0.98911E-01 
c  r22          0.10852E-01      13   0.58294E-08   0.18122E-08 0.10070E+00 
c  r33          0.21861E-01      15   0.53473E-08   0.12551E-07 0.12687E+00 
c  r12          0.93870E-03      19   0.53311E-08   0.29560E-09 0.60248E+00 
c  r13          0.46677E-02      19   0.67490E-08   0.14884E-08 0.19969E+00 
c  r23          0.39978E-02      20   0.58777E-08   0.12883E-08 0.19916E+00 
c  epsilon      0.10969E+02      11   0.33590E-08   0.10109E-01 0.16780E+00 
c  TempC        0.25716E+06      16   0.15179E-04   0.83683E-02 0.43161E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63355         0.61377       0.0052573       0.0015075
v  Velocity[Y]            -0.57376         0.54449       0.0030809      0.00087331
v  Velocity[Z]              1.5655          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4393          4.3406          4.3632
v  Pressure                -36.415          360.06          87.692           169.9
v  r11                   0.0010618         0.08191        0.013075        0.018286
v  r22                   0.0011151        0.082625        0.013355        0.018646
v  r33                   0.0016424         0.17429        0.027253        0.037207
v  r12                   -0.010668        0.013589     -0.00023384     -0.00030932
v  r13                    -0.04553        0.052795      9.3266e-05       0.0010138
v  r23                   -0.046696         0.05119      3.0562e-05      0.00057463
v  epsilon                0.069284          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9906e-05       0.0099179      0.00092515       0.0017428
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71351         0.85284


 TIME FOR THE TIME STEP            10828:        0.74166E+02

===============================================================


 INSTANT    0.108290000E-01   TIME STEP NUMBER           10829
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.198860004E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69743E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285830098E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69743E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.171865436E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69743E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.299460983E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69743E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.809139477E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69743E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81180E-03   0.45114E-02 0.19896E+01 
c  Velocity[X]                                      0.13742E-03 
c  Velocity[Y]                                      0.12821E-03 
c  Velocity[Z]                                      0.42458E-02 
c  Pressure     0.36350E-04     133   0.92508E-02   0.25639E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54473E-08   0.16277E-08 0.98378E-01 
c  r22          0.10852E-01      13   0.58605E-08   0.18290E-08 0.10085E+00 
c  r33          0.21861E-01      15   0.55890E-08   0.12536E-07 0.12626E+00 
c  r12          0.93870E-03      19   0.54569E-08   0.30332E-09 0.60545E+00 
c  r13          0.46677E-02      19   0.69760E-08   0.15101E-08 0.19974E+00 
c  r23          0.39978E-02      19   0.68806E-08   0.12955E-08 0.19825E+00 
c  epsilon      0.10969E+02      11   0.34678E-08   0.99537E-02 0.16436E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.84123E-02 0.43259E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63359         0.61377       0.0052573       0.0015074
v  Velocity[Y]            -0.57394         0.54425        0.003081      0.00087332
v  Velocity[Z]              1.5651          5.4393          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4393          4.3406          4.3632
v  Pressure                -36.389          360.02          87.634          169.84
v  r11                   0.0010619        0.081911        0.013075        0.018286
v  r22                   0.0011151        0.082625        0.013355        0.018646
v  r33                   0.0016424         0.17431        0.027253        0.037207
v  r12                   -0.010663        0.013587     -0.00023384     -0.00030932
v  r13                    -0.04553        0.052795      9.3266e-05       0.0010139
v  r23                   -0.046696        0.051202      3.0562e-05      0.00057463
v  epsilon                0.069285          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9905e-05       0.0099179      0.00092515       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017854          5.2787         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71351         0.85284


 TIME FOR THE TIME STEP            10829:        0.73557E+02

===============================================================


 INSTANT    0.108300000E-01   TIME STEP NUMBER           10830
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.237615503E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69743E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.823418657E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69743E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116342382E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69743E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.407821884E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69743E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.207724515E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69743E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81259E-03   0.45148E-02 0.19916E+01 
c  Velocity[X]                                      0.13808E-03 
c  Velocity[Y]                                      0.12831E-03 
c  Velocity[Z]                                      0.42484E-02 
c  Pressure     0.36235E-04     132   0.92194E-02   0.25558E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56669E-08   0.16008E-08 0.98341E-01 
c  r22          0.10852E-01      13   0.58301E-08   0.18042E-08 0.10077E+00 
c  r33          0.21861E-01      15   0.54568E-08   0.12269E-07 0.12616E+00 
c  r12          0.93870E-03      18   0.65556E-08   0.29738E-09 0.60134E+00 
c  r13          0.46677E-02      19   0.67125E-08   0.14864E-08 0.19913E+00 
c  r23          0.39978E-02      19   0.62429E-08   0.12475E-08 0.19678E+00 
c  epsilon      0.10969E+02      11   0.32901E-08   0.95704E-02 0.16290E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84408E-02 0.43387E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61377       0.0052574       0.0015075
v  Velocity[Y]            -0.57381         0.54427       0.0030809      0.00087332
v  Velocity[Z]              1.5652          5.4393          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4393          4.3406          4.3632
v  Pressure                -36.423          360.04          87.659          169.86
v  r11                   0.0010619        0.081908        0.013075        0.018286
v  r22                   0.0011151        0.082624        0.013355        0.018646
v  r33                   0.0016424         0.17435        0.027253        0.037207
v  r12                   -0.010663        0.013584     -0.00023384     -0.00030932
v  r13                   -0.045528        0.052796      9.3267e-05       0.0010138
v  r23                   -0.046696        0.051186      3.0562e-05      0.00057463
v  epsilon                0.069286          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9904e-05       0.0099175      0.00092515       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2787         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85284


 TIME FOR THE TIME STEP            10830:        0.70915E+02

===============================================================


 INSTANT    0.108310000E-01   TIME STEP NUMBER           10831
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.111209027E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69745E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.144129005E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69745E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.160548252E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69745E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.315368407E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69745E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.230698894E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21881E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69745E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81356E-03   0.45151E-02 0.19911E+01 
c  Velocity[X]                                      0.13788E-03 
c  Velocity[Y]                                      0.12728E-03 
c  Velocity[Z]                                      0.42499E-02 
c  Pressure     0.36442E-04     131   0.92733E-02   0.25705E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56966E-08   0.16455E-08 0.98933E-01 
c  r22          0.10852E-01      13   0.57118E-08   0.18074E-08 0.10050E+00 
c  r33          0.21861E-01      15   0.58754E-08   0.12631E-07 0.12679E+00 
c  r12          0.93870E-03      18   0.65854E-08   0.29004E-09 0.59684E+00 
c  r13          0.46677E-02      19   0.65147E-08   0.14970E-08 0.19920E+00 
c  r23          0.39978E-02      19   0.61608E-08   0.12938E-08 0.19859E+00 
c  epsilon      0.10969E+02      11   0.33570E-08   0.10239E-01 0.16884E+00 
c  TempC        0.25716E+06      16   0.15103E-04   0.83478E-02 0.43118E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61378       0.0052574       0.0015075
v  Velocity[Y]            -0.57378         0.54429        0.003081      0.00087335
v  Velocity[Z]              1.5651          5.4394          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4394          4.3406          4.3632
v  Pressure                -36.374          359.99          87.629          169.83
v  r11                   0.0010619        0.081904        0.013075        0.018286
v  r22                   0.0011151        0.082624        0.013355        0.018646
v  r33                   0.0016424         0.17433        0.027253        0.037207
v  r12                    -0.01066        0.013589     -0.00023384     -0.00030932
v  r13                    -0.04553        0.052794      9.3266e-05       0.0010138
v  r23                   -0.046695        0.051171      3.0562e-05      0.00057463
v  epsilon                0.069287          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9902e-05       0.0099174      0.00092515       0.0017428
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71351         0.85283


 TIME FOR THE TIME STEP            10831:        0.70157E+02

===============================================================


 INSTANT    0.108320000E-01   TIME STEP NUMBER           10832
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.307899297E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.176359750E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.197248800E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229249253E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.172035182E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81259E-03   0.45261E-02 0.19930E+01 
c  Velocity[X]                                      0.13794E-03 
c  Velocity[Y]                                      0.12803E-03 
c  Velocity[Z]                                      0.42601E-02 
c  Pressure     0.36357E-04     132   0.92572E-02   0.25644E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52802E-08   0.16098E-08 0.97960E-01 
c  r22          0.10852E-01      13   0.54768E-08   0.18342E-08 0.10092E+00 
c  r33          0.21861E-01      15   0.59859E-08   0.12428E-07 0.12603E+00 
c  r12          0.93870E-03      18   0.61552E-08   0.29568E-09 0.59958E+00 
c  r13          0.46677E-02      19   0.64931E-08   0.15065E-08 0.19975E+00 
c  r23          0.39978E-02      19   0.63166E-08   0.12787E-08 0.19731E+00 
c  epsilon      0.10969E+02      11   0.33343E-08   0.98460E-02 0.16490E+00 
c  TempC        0.25716E+06      16   0.15169E-04   0.83705E-02 0.43162E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61373       0.0052574       0.0015074
v  Velocity[Y]            -0.57361         0.54436       0.0030809      0.00087331
v  Velocity[Z]              1.5651          5.4394          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4394          4.3406          4.3632
v  Pressure                -36.439          359.97          87.629          169.81
v  r11                   0.0010619        0.081906        0.013075        0.018286
v  r22                   0.0011151        0.082623        0.013355        0.018646
v  r33                   0.0016424         0.17429        0.027253        0.037207
v  r12                   -0.010659         0.01359     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052794      9.3266e-05       0.0010138
v  r23                   -0.046695        0.051201      3.0563e-05      0.00057463
v  epsilon                0.069288           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc               5.99e-05       0.0099175      0.00092516       0.0017428
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71351         0.85283


 TIME FOR THE TIME STEP            10832:        0.69374E+02

===============================================================


 INSTANT    0.108330000E-01   TIME STEP NUMBER           10833
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.552672011E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69745E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.113904240E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69745E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.749248000E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69745E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.774591740E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69745E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150147049E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69745E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81184E-03   0.44989E-02 0.19876E+01 
c  Velocity[X]                                      0.13854E-03 
c  Velocity[Y]                                      0.12821E-03 
c  Velocity[Z]                                      0.42321E-02 
c  Pressure     0.36226E-04     132   0.92244E-02   0.25552E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55127E-08   0.16544E-08 0.99582E-01 
c  r22          0.10852E-01      13   0.54619E-08   0.17934E-08 0.10055E+00 
c  r33          0.21861E-01      15   0.57823E-08   0.12499E-07 0.12699E+00 
c  r12          0.93870E-03      18   0.64887E-08   0.29680E-09 0.60289E+00 
c  r13          0.46677E-02      19   0.73795E-08   0.14946E-08 0.19971E+00 
c  r23          0.39978E-02      19   0.60488E-08   0.13005E-08 0.19965E+00 
c  epsilon      0.10969E+02      11   0.33904E-08   0.99477E-02 0.16899E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.84326E-02 0.43328E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61376       0.0052574       0.0015075
v  Velocity[Y]            -0.57369         0.54417        0.003081      0.00087335
v  Velocity[Z]              1.5653          5.4394          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4394          4.3406          4.3632
v  Pressure                 -36.38          360.08          87.672           169.9
v  r11                   0.0010619          0.0819        0.013075        0.018286
v  r22                   0.0011151        0.082619        0.013355        0.018646
v  r33                   0.0016425          0.1743        0.027253        0.037207
v  r12                   -0.010657         0.01359     -0.00023384     -0.00030932
v  r13                   -0.045528        0.052795      9.3267e-05       0.0010139
v  r23                   -0.046695        0.051185      3.0564e-05      0.00057463
v  epsilon                0.069289          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9901e-05       0.0099175      0.00092516       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71351         0.85284


 TIME FOR THE TIME STEP            10833:        0.70457E+02

===============================================================


 INSTANT    0.108340000E-01   TIME STEP NUMBER           10834
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.249716681E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.258586203E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.620081932E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935011E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.605455642E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.222557470E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81356E-03   0.45257E-02 0.19925E+01 
c  Velocity[X]                                      0.13665E-03 
c  Velocity[Y]                                      0.12805E-03 
c  Velocity[Z]                                      0.42610E-02 
c  Pressure     0.36462E-04     132   0.92733E-02   0.25718E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55035E-08   0.16231E-08 0.98527E-01 
c  r22          0.10852E-01      13   0.56947E-08   0.17909E-08 0.99817E-01 
c  r33          0.21861E-01      15   0.61661E-08   0.12392E-07 0.12551E+00 
c  r12          0.93870E-03      18   0.66635E-08   0.29290E-09 0.59772E+00 
c  r13          0.46677E-02      19   0.69187E-08   0.14760E-08 0.19729E+00 
c  r23          0.39978E-02      19   0.58097E-08   0.12716E-08 0.19706E+00 
c  epsilon      0.10969E+02      11   0.34293E-08   0.97257E-02 0.16306E+00 
c  TempC        0.25716E+06      16   0.15181E-04   0.83955E-02 0.43213E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61376       0.0052573       0.0015074
v  Velocity[Y]            -0.57365         0.54428        0.003081      0.00087334
v  Velocity[Z]              1.5652          5.4394          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4394          4.3406          4.3632
v  Pressure                -36.434          359.99          87.632          169.83
v  r11                   0.0010619        0.081893        0.013075        0.018286
v  r22                   0.0011151         0.08262        0.013355        0.018646
v  r33                   0.0016425         0.17432        0.027253        0.037207
v  r12                   -0.010665        0.013589     -0.00023384     -0.00030932
v  r13                    -0.04553        0.052795      9.3267e-05       0.0010139
v  r23                   -0.046695        0.051175      3.0564e-05      0.00057463
v  epsilon                 0.06929          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9901e-05       0.0099176      0.00092516       0.0017428
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2779         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            10834:        0.72268E+02

===============================================================


 INSTANT    0.108350000E-01   TIME STEP NUMBER           10835
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.117188969E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.168562938E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.526790525E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.423903534E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.298202489E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81249E-03   0.45085E-02 0.19911E+01 
c  Velocity[X]                                      0.13796E-03 
c  Velocity[Y]                                      0.12757E-03 
c  Velocity[Z]                                      0.42430E-02 
c  Pressure     0.36562E-04     131   0.93151E-02   0.25789E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55857E-08   0.16207E-08 0.98508E-01 
c  r22          0.10852E-01      13   0.55981E-08   0.18090E-08 0.10051E+00 
c  r33          0.21861E-01      15   0.63011E-08   0.12464E-07 0.12603E+00 
c  r12          0.93870E-03      18   0.58969E-08   0.29017E-09 0.59995E+00 
c  r13          0.46677E-02      19   0.71573E-08   0.14900E-08 0.19805E+00 
c  r23          0.39978E-02      19   0.56706E-08   0.12902E-08 0.19860E+00 
c  epsilon      0.10969E+02      11   0.34501E-08   0.97096E-02 0.16207E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.84152E-02 0.43232E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61375       0.0052574       0.0015074
v  Velocity[Y]            -0.57381         0.54441        0.003081      0.00087337
v  Velocity[Z]              1.5652          5.4394          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4394          4.3406          4.3632
v  Pressure                -36.415          359.99          87.605          169.81
v  r11                   0.0010619        0.081889        0.013075        0.018286
v  r22                   0.0011151        0.082621        0.013355        0.018646
v  r33                   0.0016425          0.1743        0.027253        0.037207
v  r12                   -0.010667         0.01359     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052794      9.3267e-05       0.0010139
v  r23                   -0.046694        0.051194      3.0565e-05      0.00057463
v  epsilon                 0.06929          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9904e-05       0.0099176      0.00092516       0.0017428
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2774         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            10835:        0.70972E+02

===============================================================


 INSTANT    0.108360000E-01   TIME STEP NUMBER           10836
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282186012E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.613446326E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.904205868E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.136737245E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239211961E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81320E-03   0.45003E-02 0.19849E+01 
c  Velocity[X]                                      0.13784E-03 
c  Velocity[Y]                                      0.12770E-03 
c  Velocity[Z]                                      0.42348E-02 
c  Pressure     0.36584E-04     133   0.93140E-02   0.25804E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56116E-08   0.16264E-08 0.98546E-01 
c  r22          0.10852E-01      13   0.57517E-08   0.18034E-08 0.10041E+00 
c  r33          0.21861E-01      15   0.58915E-08   0.12409E-07 0.12604E+00 
c  r12          0.93871E-03      18   0.64254E-08   0.29191E-09 0.60009E+00 
c  r13          0.46677E-02      19   0.56003E-08   0.14841E-08 0.19846E+00 
c  r23          0.39978E-02      19   0.64735E-08   0.12821E-08 0.19806E+00 
c  epsilon      0.10969E+02      11   0.32673E-08   0.96568E-02 0.16400E+00 
c  TempC        0.25716E+06      16   0.15175E-04   0.84512E-02 0.43396E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61378       0.0052574       0.0015074
v  Velocity[Y]            -0.57383         0.54407        0.003081      0.00087337
v  Velocity[Z]              1.5651          5.4394          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4394          4.3406          4.3632
v  Pressure                -36.418          360.08          87.695           169.9
v  r11                   0.0010619        0.081882        0.013075        0.018286
v  r22                   0.0011151        0.082622        0.013355        0.018646
v  r33                   0.0016425         0.17427        0.027253        0.037207
v  r12                    -0.01067        0.013593     -0.00023384     -0.00030932
v  r13                   -0.045525        0.052794      9.3268e-05       0.0010139
v  r23                   -0.046694         0.05118      3.0566e-05      0.00057463
v  epsilon                0.069291          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9906e-05       0.0099176      0.00092516       0.0017428
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2769         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71351         0.85284


 TIME FOR THE TIME STEP            10836:        0.69903E+02

===============================================================


 INSTANT    0.108370000E-01   TIME STEP NUMBER           10837
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200362404E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.161862679E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.203505342E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935020E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.573281645E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203458525E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81263E-03   0.45243E-02 0.19914E+01 
c  Velocity[X]                                      0.13838E-03 
c  Velocity[Y]                                      0.12815E-03 
c  Velocity[Z]                                      0.42578E-02 
c  Pressure     0.36095E-04     133   0.91862E-02   0.25459E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57878E-08   0.16184E-08 0.98267E-01 
c  r22          0.10852E-01      13   0.58000E-08   0.17971E-08 0.10012E+00 
c  r33          0.21861E-01      16   0.56765E-08   0.12416E-07 0.12584E+00 
c  r12          0.93871E-03      18   0.67642E-08   0.29183E-09 0.60081E+00 
c  r13          0.46677E-02      19   0.69461E-08   0.14953E-08 0.19876E+00 
c  r23          0.39978E-02      20   0.61536E-08   0.12809E-08 0.19719E+00 
c  epsilon      0.10969E+02      11   0.34625E-08   0.99443E-02 0.16666E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.84009E-02 0.43255E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61376       0.0052573       0.0015074
v  Velocity[Y]             -0.5739         0.54408        0.003081      0.00087335
v  Velocity[Z]              1.5653          5.4394          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4394          4.3406          4.3632
v  Pressure                -36.368          360.07           87.68           169.9
v  r11                   0.0010619        0.081877        0.013075        0.018286
v  r22                   0.0011151        0.082623        0.013355        0.018646
v  r33                   0.0016425         0.17429        0.027253        0.037207
v  r12                   -0.010668        0.013592     -0.00023384     -0.00030932
v  r13                   -0.045529        0.052795      9.3268e-05       0.0010139
v  r23                   -0.046694        0.051174      3.0565e-05      0.00057463
v  epsilon                0.069292          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.991e-05       0.0099176      0.00092516       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2769         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71352         0.85284


 TIME FOR THE TIME STEP            10837:        0.70459E+02

===============================================================


 INSTANT    0.108380000E-01   TIME STEP NUMBER           10838
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.799803390E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.407493374E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.683379588E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.396762025E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.364969526E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81252E-03   0.45083E-02 0.19889E+01 
c  Velocity[X]                                      0.13712E-03 
c  Velocity[Y]                                      0.12816E-03 
c  Velocity[Z]                                      0.42431E-02 
c  Pressure     0.36381E-04     132   0.92646E-02   0.25661E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57967E-08   0.16513E-08 0.99134E-01 
c  r22          0.10852E-01      13   0.60310E-08   0.18197E-08 0.10046E+00 
c  r33          0.21861E-01      15   0.60125E-08   0.12612E-07 0.12659E+00 
c  r12          0.93871E-03      18   0.72350E-08   0.29584E-09 0.60265E+00 
c  r13          0.46677E-02      19   0.65100E-08   0.15080E-08 0.19889E+00 
c  r23          0.39978E-02      20   0.61575E-08   0.13116E-08 0.19971E+00 
c  epsilon      0.10969E+02      11   0.34483E-08   0.10330E-01 0.17215E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.83611E-02 0.43154E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61378       0.0052574       0.0015075
v  Velocity[Y]            -0.57375         0.54422        0.003081      0.00087335
v  Velocity[Z]              1.5655          5.4394          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4394          4.3406          4.3632
v  Pressure                -36.417          359.95          87.623           169.8
v  r11                   0.0010619        0.081866        0.013075        0.018286
v  r22                   0.0011151        0.082624        0.013355        0.018646
v  r33                   0.0016425         0.17431        0.027253        0.037207
v  r12                   -0.010669        0.013592     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052797      9.3267e-05       0.0010139
v  r23                   -0.046694        0.051175      3.0565e-05      0.00057463
v  epsilon                0.069293           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9911e-05       0.0099175      0.00092516       0.0017428
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2774         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            10838:        0.71509E+02

===============================================================


 INSTANT    0.108390000E-01   TIME STEP NUMBER           10839
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237173998E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191953442E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.621049088E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.104427666E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.213083112E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81228E-03   0.45297E-02 0.19938E+01 
c  Velocity[X]                                      0.13753E-03 
c  Velocity[Y]                                      0.12902E-03 
c  Velocity[Z]                                      0.42632E-02 
c  Pressure     0.36265E-04     132   0.92307E-02   0.25580E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58108E-08   0.16059E-08 0.98024E-01 
c  r22          0.10852E-01      13   0.62704E-08   0.17904E-08 0.99904E-01 
c  r33          0.21861E-01      15   0.66484E-08   0.12276E-07 0.12513E+00 
c  r12          0.93871E-03      18   0.70389E-08   0.29381E-09 0.60085E+00 
c  r13          0.46677E-02      19   0.58944E-08   0.14728E-08 0.19719E+00 
c  r23          0.39978E-02      20   0.60889E-08   0.12561E-08 0.19537E+00 
c  epsilon      0.10969E+02      11   0.36767E-08   0.98439E-02 0.16430E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.85123E-02 0.43501E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61377       0.0052574       0.0015075
v  Velocity[Y]            -0.57377         0.54439        0.003081      0.00087337
v  Velocity[Z]              1.5654          5.4394          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4394          4.3406          4.3632
v  Pressure                -36.386             360          87.622          169.83
v  r11                   0.0010619        0.081855        0.013075        0.018286
v  r22                   0.0011151        0.082624        0.013355        0.018646
v  r33                   0.0016425          0.1743        0.027253        0.037207
v  r12                   -0.010667         0.01359     -0.00023384     -0.00030932
v  r13                   -0.045526        0.052796      9.3268e-05       0.0010139
v  r23                   -0.046694         0.05121      3.0565e-05      0.00057463
v  epsilon                0.069294          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099174      0.00092516       0.0017428
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017855           5.278         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            10839:        0.71168E+02

===============================================================


 INSTANT    0.108400000E-01   TIME STEP NUMBER           10840
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.168653519E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.390078184E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.376964533E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172411551E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.789782575E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81394E-03   0.45040E-02 0.19865E+01 
c  Velocity[X]                                      0.13831E-03 
c  Velocity[Y]                                      0.12786E-03 
c  Velocity[Z]                                      0.42378E-02 
c  Pressure     0.35945E-04     133   0.91527E-02   0.25353E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57612E-08   0.16032E-08 0.98054E-01 
c  r22          0.10852E-01      13   0.60649E-08   0.18185E-08 0.10061E+00 
c  r33          0.21861E-01      15   0.65380E-08   0.12395E-07 0.12595E+00 
c  r12          0.93871E-03      18   0.66121E-08   0.29122E-09 0.59905E+00 
c  r13          0.46677E-02      19   0.56131E-08   0.14924E-08 0.19938E+00 
c  r23          0.39978E-02      20   0.56341E-08   0.12530E-08 0.19563E+00 
c  epsilon      0.10969E+02      11   0.35195E-08   0.99271E-02 0.16584E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.83908E-02 0.43273E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61373       0.0052573       0.0015074
v  Velocity[Y]            -0.57364         0.54408        0.003081      0.00087334
v  Velocity[Z]              1.5655          5.4394          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4394          4.3406          4.3632
v  Pressure                -36.485          360.03          87.639          169.85
v  r11                   0.0010619        0.081849        0.013075        0.018286
v  r22                   0.0011151        0.082625        0.013355        0.018646
v  r33                   0.0016425         0.17428        0.027253        0.037207
v  r12                   -0.010664        0.013594     -0.00023384     -0.00030932
v  r13                   -0.045529        0.052797      9.3268e-05       0.0010139
v  r23                   -0.046694        0.051196      3.0565e-05      0.00057463
v  epsilon                0.069295          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099173      0.00092516       0.0017428
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2782         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            10840:        0.72100E+02

===============================================================


 INSTANT    0.108410000E-01   TIME STEP NUMBER           10841
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.450126078E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.247496530E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.372706277E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.645177244E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.234558421E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81266E-03   0.44935E-02 0.19837E+01 
c  Velocity[X]                                      0.13801E-03 
c  Velocity[Y]                                      0.12730E-03 
c  Velocity[Z]                                      0.42282E-02 
c  Pressure     0.36504E-04     133   0.92968E-02   0.25748E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58956E-08   0.16538E-08 0.99462E-01 
c  r22          0.10852E-01      13   0.63316E-08   0.18411E-08 0.10106E+00 
c  r33          0.21861E-01      15   0.60061E-08   0.12644E-07 0.12683E+00 
c  r12          0.93871E-03      19   0.55852E-08   0.29616E-09 0.60218E+00 
c  r13          0.46677E-02      19   0.57701E-08   0.15246E-08 0.20008E+00 
c  r23          0.39978E-02      19   0.71868E-08   0.12977E-08 0.19859E+00 
c  epsilon      0.10969E+02      11   0.33944E-08   0.10239E-01 0.16729E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.83873E-02 0.43200E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61377       0.0052574       0.0015075
v  Velocity[Y]            -0.57372         0.54411        0.003081      0.00087333
v  Velocity[Z]              1.5652          5.4394          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4394          4.3406          4.3632
v  Pressure                -36.424          360.06          87.678          169.88
v  r11                   0.0010619        0.081849        0.013075        0.018286
v  r22                   0.0011151        0.082625        0.013355        0.018646
v  r33                   0.0016425         0.17429        0.027253        0.037207
v  r12                   -0.010665        0.013599     -0.00023384     -0.00030932
v  r13                   -0.045528        0.052798      9.3268e-05       0.0010139
v  r23                   -0.046694        0.051186      3.0565e-05      0.00057463
v  epsilon                0.069296          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099174      0.00092516       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017855          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            10841:        0.70546E+02

===============================================================


 INSTANT    0.108420000E-01   TIME STEP NUMBER           10842
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.143230662E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123743111E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.552288053E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161621211E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.676706458E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81260E-03   0.45353E-02 0.19937E+01 
c  Velocity[X]                                      0.13808E-03 
c  Velocity[Y]                                      0.12877E-03 
c  Velocity[Z]                                      0.42684E-02 
c  Pressure     0.36177E-04     131   0.92158E-02   0.25517E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58057E-08   0.16282E-08 0.98691E-01 
c  r22          0.10852E-01      13   0.57958E-08   0.18064E-08 0.10092E+00 
c  r33          0.21861E-01      15   0.56686E-08   0.12367E-07 0.12615E+00 
c  r12          0.93871E-03      18   0.66105E-08   0.29482E-09 0.60045E+00 
c  r13          0.46677E-02      19   0.68821E-08   0.14874E-08 0.19929E+00 
c  r23          0.39978E-02      20   0.54425E-08   0.12867E-08 0.19769E+00 
c  epsilon      0.10969E+02      11   0.35590E-08   0.97007E-02 0.16466E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.83938E-02 0.43181E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61375       0.0052575       0.0015075
v  Velocity[Y]            -0.57376         0.54429       0.0030811      0.00087338
v  Velocity[Z]              1.5654          5.4394          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4394          4.3406          4.3632
v  Pressure                -36.497          360.07          87.681          169.89
v  r11                   0.0010619        0.081862        0.013075        0.018286
v  r22                   0.0011151        0.082622        0.013355        0.018646
v  r33                   0.0016425         0.17431        0.027253        0.037207
v  r12                   -0.010664        0.013598     -0.00023384     -0.00030932
v  r13                   -0.045526        0.052802      9.3268e-05       0.0010139
v  r23                   -0.046695        0.051214      3.0566e-05      0.00057463
v  epsilon                0.069297          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099176      0.00092516       0.0017428
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2784         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85284


 TIME FOR THE TIME STEP            10842:        0.73020E+02

===============================================================


 INSTANT    0.108430000E-01   TIME STEP NUMBER           10843
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.134037335E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.956770201E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.148310737E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935024E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.912979714E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.152504906E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81323E-03   0.45212E-02 0.19917E+01 
c  Velocity[X]                                      0.13801E-03 
c  Velocity[Y]                                      0.12849E-03 
c  Velocity[Z]                                      0.42547E-02 
c  Pressure     0.36078E-04     133   0.91894E-02   0.25448E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57422E-08   0.16494E-08 0.99338E-01 
c  r22          0.10852E-01      13   0.58067E-08   0.18367E-08 0.10113E+00 
c  r33          0.21861E-01      15   0.70170E-08   0.12661E-07 0.12710E+00 
c  r12          0.93871E-03      19   0.53569E-08   0.29251E-09 0.60031E+00 
c  r13          0.46677E-02      19   0.58553E-08   0.15066E-08 0.19934E+00 
c  r23          0.39978E-02      19   0.65287E-08   0.13052E-08 0.19951E+00 
c  epsilon      0.10969E+02      11   0.35607E-08   0.10351E-01 0.17167E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.83724E-02 0.43182E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61372       0.0052575       0.0015075
v  Velocity[Y]            -0.57386         0.54445       0.0030811      0.00087337
v  Velocity[Z]              1.5652          5.4395          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4395          4.3406          4.3632
v  Pressure                -36.405          359.99          87.602          169.81
v  r11                   0.0010619        0.081877        0.013075        0.018286
v  r22                   0.0011151        0.082623        0.013355        0.018646
v  r33                   0.0016425          0.1743        0.027253        0.037207
v  r12                   -0.010664        0.013594     -0.00023384     -0.00030932
v  r13                   -0.045528          0.0528      9.3268e-05       0.0010139
v  r23                   -0.046694        0.051209      3.0565e-05      0.00057463
v  epsilon                0.069298          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099178      0.00092516       0.0017428
v  CourantNb               0.44256             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71351         0.85284


 TIME FOR THE TIME STEP            10843:        0.70214E+02

===============================================================


 INSTANT    0.108440000E-01   TIME STEP NUMBER           10844
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.322654500E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.427332819E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.299712594E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.635135362E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.524852134E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12292E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81312E-03   0.44982E-02 0.19845E+01 
c  Velocity[X]                                      0.13711E-03 
c  Velocity[Y]                                      0.12721E-03 
c  Velocity[Z]                                      0.42339E-02 
c  Pressure     0.36282E-04     132   0.92427E-02   0.25591E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57773E-08   0.16248E-08 0.98449E-01 
c  r22          0.10852E-01      13   0.55962E-08   0.18758E-08 0.10165E+00 
c  r33          0.21861E-01      15   0.59977E-08   0.12735E-07 0.12699E+00 
c  r12          0.93871E-03      18   0.66092E-08   0.29725E-09 0.60231E+00 
c  r13          0.46677E-02      19   0.69179E-08   0.15494E-08 0.20124E+00 
c  r23          0.39978E-02      19   0.64007E-08   0.12858E-08 0.19768E+00 
c  epsilon      0.10969E+02      11   0.34373E-08   0.10337E-01 0.16947E+00 
c  TempC        0.25716E+06      16   0.15177E-04   0.84564E-02 0.43413E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61377       0.0052574       0.0015075
v  Velocity[Y]            -0.57367         0.54411        0.003081      0.00087334
v  Velocity[Z]              1.5652          5.4395          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4395          4.3406          4.3632
v  Pressure                -36.445          359.98          87.604           169.8
v  r11                   0.0010619        0.081888        0.013075        0.018286
v  r22                   0.0011151        0.082624        0.013355        0.018646
v  r33                   0.0016425         0.17426        0.027253        0.037207
v  r12                   -0.010664        0.013596     -0.00023384     -0.00030932
v  r13                   -0.045525        0.052801      9.3268e-05       0.0010139
v  r23                   -0.046695        0.051195      3.0565e-05      0.00057463
v  epsilon                0.069299          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099177      0.00092516       0.0017428
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2782         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            10844:        0.68126E+02

===============================================================


 INSTANT    0.108450000E-01   TIME STEP NUMBER           10845
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.722626667E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.202951178E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.197855911E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.430676379E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.365917836E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81222E-03   0.45240E-02 0.19904E+01 
c  Velocity[X]                                      0.13782E-03 
c  Velocity[Y]                                      0.12753E-03 
c  Velocity[Z]                                      0.42587E-02 
c  Pressure     0.36137E-04     131   0.91999E-02   0.25490E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60970E-08   0.16547E-08 0.98796E-01 
c  r22          0.10852E-01      13   0.60307E-08   0.18249E-08 0.10119E+00 
c  r33          0.21861E-01      15   0.62793E-08   0.12546E-07 0.12646E+00 
c  r12          0.93871E-03      19   0.55583E-08   0.29317E-09 0.59920E+00 
c  r13          0.46677E-02      19   0.66356E-08   0.14785E-08 0.19875E+00 
c  r23          0.39978E-02      19   0.65592E-08   0.12825E-08 0.19726E+00 
c  epsilon      0.10969E+02      11   0.34576E-08   0.99952E-02 0.16621E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84015E-02 0.43269E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162017


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6333         0.61374       0.0052576       0.0015076
v  Velocity[Y]            -0.57362         0.54415       0.0030811       0.0008734
v  Velocity[Z]              1.5653          5.4395          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4395          4.3406          4.3632
v  Pressure                -36.393          360.02          87.629          169.84
v  r11                   0.0010619        0.081893        0.013075        0.018286
v  r22                   0.0011151        0.082627        0.013355        0.018646
v  r33                   0.0016426         0.17428        0.027253        0.037207
v  r12                   -0.010665        0.013594     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052802      9.3269e-05       0.0010139
v  r23                   -0.046695         0.05121      3.0566e-05      0.00057463
v  epsilon                  0.0693          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099175      0.00092517       0.0017428
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2778         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85284


 TIME FOR THE TIME STEP            10845:        0.66556E+02

===============================================================


 INSTANT    0.108460000E-01   TIME STEP NUMBER           10846
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.576116980E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.278114934E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.482366150E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267391729E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.406020219E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81446E-03   0.44999E-02 0.19868E+01 
c  Velocity[X]                                      0.13684E-03 
c  Velocity[Y]                                      0.12830E-03 
c  Velocity[Z]                                      0.42348E-02 
c  Pressure     0.35989E-04     132   0.91577E-02   0.25385E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60777E-08   0.16613E-08 0.99485E-01 
c  r22          0.10852E-01      13   0.56506E-08   0.18483E-08 0.10188E+00 
c  r33          0.21861E-01      15   0.55652E-08   0.12703E-07 0.12746E+00 
c  r12          0.93871E-03      18   0.70034E-08   0.30421E-09 0.60652E+00 
c  r13          0.46677E-02      19   0.53636E-08   0.15036E-08 0.20021E+00 
c  r23          0.39978E-02      19   0.59704E-08   0.13071E-08 0.19945E+00 
c  epsilon      0.10969E+02      11   0.35472E-08   0.10030E-01 0.16756E+00 
c  TempC        0.25716E+06      16   0.15167E-04   0.83636E-02 0.43146E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162021


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63331         0.61371       0.0052576       0.0015076
v  Velocity[Y]            -0.57358         0.54426       0.0030811      0.00087341
v  Velocity[Z]               1.565          5.4395          4.3387          4.3625
v  ǁVelocityǁ               1.5788          5.4395          4.3406          4.3632
v  Pressure                -36.436          359.97          87.621          169.81
v  r11                   0.0010619        0.081895        0.013075        0.018286
v  r22                   0.0011151        0.082629        0.013355        0.018646
v  r33                   0.0016426         0.17431        0.027253        0.037207
v  r12                   -0.010663        0.013591     -0.00023384     -0.00030932
v  r13                   -0.045529        0.052801       9.327e-05       0.0010139
v  r23                   -0.046695        0.051199      3.0566e-05      0.00057463
v  epsilon                0.069301           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099176      0.00092517       0.0017428
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2779         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            10846:        0.67328E+02

===============================================================


 INSTANT    0.108470000E-01   TIME STEP NUMBER           10847
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.269634800E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.203878204E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.258631706E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.393867063E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.626702921E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81108E-03   0.45325E-02 0.19934E+01 
c  Velocity[X]                                      0.13774E-03 
c  Velocity[Y]                                      0.12839E-03 
c  Velocity[Z]                                      0.42663E-02 
c  Pressure     0.36386E-04     134   0.92650E-02   0.25665E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53938E-08   0.16177E-08 0.98630E-01 
c  r22          0.10852E-01      13   0.55280E-08   0.18370E-08 0.10113E+00 
c  r33          0.21861E-01      15   0.61872E-08   0.12458E-07 0.12636E+00 
c  r12          0.93871E-03      18   0.61681E-08   0.29208E-09 0.59854E+00 
c  r13          0.46677E-02      19   0.54071E-08   0.15003E-08 0.19906E+00 
c  r23          0.39978E-02      19   0.58893E-08   0.12677E-08 0.19681E+00 
c  epsilon      0.10969E+02      11   0.34318E-08   0.98088E-02 0.16544E+00 
c  TempC        0.25716E+06      16   0.15127E-04   0.84048E-02 0.43213E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61377       0.0052576       0.0015076
v  Velocity[Y]             -0.5737         0.54437       0.0030811       0.0008734
v  Velocity[Z]              1.5652          5.4395          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4395          4.3406          4.3632
v  Pressure                -36.372          359.99          87.631          169.83
v  r11                   0.0010619        0.081893        0.013075        0.018286
v  r22                   0.0011151         0.08263        0.013355        0.018646
v  r33                   0.0016426         0.17429        0.027253        0.037207
v  r12                   -0.010662         0.01359     -0.00023384     -0.00030932
v  r13                   -0.045526        0.052801       9.327e-05       0.0010139
v  r23                   -0.046695        0.051193      3.0566e-05      0.00057463
v  epsilon                0.069302          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099176      0.00092517       0.0017428
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2772         0.11443         0.25443
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71351         0.85283


 TIME FOR THE TIME STEP            10847:        0.68632E+02

===============================================================


 INSTANT    0.108480000E-01   TIME STEP NUMBER           10848
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110450505E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.800312823E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.198759695E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.239687346E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.662458130E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81286E-03   0.44964E-02 0.19857E+01 
c  Velocity[X]                                      0.13835E-03 
c  Velocity[Y]                                      0.12842E-03 
c  Velocity[Z]                                      0.42296E-02 
c  Pressure     0.36224E-04     133   0.92203E-02   0.25551E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53665E-08   0.16744E-08 0.10007E+00 
c  r22          0.10852E-01      13   0.53407E-08   0.18307E-08 0.10131E+00 
c  r33          0.21861E-01      15   0.60293E-08   0.12714E-07 0.12772E+00 
c  r12          0.93871E-03      18   0.61243E-08   0.30160E-09 0.60903E+00 
c  r13          0.46677E-02      19   0.60967E-08   0.15067E-08 0.20063E+00 
c  r23          0.39979E-02      19   0.62940E-08   0.13196E-08 0.20108E+00 
c  epsilon      0.10969E+02      11   0.34642E-08   0.10245E-01 0.17117E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.84315E-02 0.43355E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61372       0.0052575       0.0015076
v  Velocity[Y]             -0.5736         0.54421        0.003081      0.00087339
v  Velocity[Z]              1.5654          5.4395          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4395          4.3406          4.3632
v  Pressure                -36.426          360.06          87.682          169.89
v  r11                   0.0010619        0.081902        0.013075        0.018286
v  r22                   0.0011151         0.08263        0.013355        0.018646
v  r33                   0.0016426         0.17427        0.027253        0.037207
v  r12                   -0.010661        0.013594     -0.00023384     -0.00030932
v  r13                   -0.045525          0.0528       9.327e-05       0.0010139
v  r23                   -0.046696        0.051213      3.0566e-05      0.00057463
v  epsilon                0.069303          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099177      0.00092517       0.0017428
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2766         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71352         0.85284


 TIME FOR THE TIME STEP            10848:        0.68309E+02

===============================================================


 INSTANT    0.108490000E-01   TIME STEP NUMBER           10849
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.223107394E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149115510E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195292057E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935018E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.324775686E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120696943E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81283E-03   0.44886E-02 0.19841E+01 
c  Velocity[X]                                      0.13797E-03 
c  Velocity[Y]                                      0.12710E-03 
c  Velocity[Z]                                      0.42236E-02 
c  Pressure     0.36012E-04     133   0.91669E-02   0.25400E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54937E-08   0.16410E-08 0.99130E-01 
c  r22          0.10852E-01      13   0.59084E-08   0.17977E-08 0.10042E+00 
c  r33          0.21861E-01      15   0.67826E-08   0.12344E-07 0.12586E+00 
c  r12          0.93871E-03      18   0.62717E-08   0.29921E-09 0.60436E+00 
c  r13          0.46677E-02      20   0.63326E-08   0.14715E-08 0.19849E+00 
c  r23          0.39979E-02      19   0.66168E-08   0.12794E-08 0.19787E+00 
c  epsilon      0.10969E+02      11   0.35165E-08   0.95392E-02 0.16165E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.84278E-02 0.43306E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63333          0.6137       0.0052575       0.0015076
v  Velocity[Y]            -0.57376         0.54429        0.003081      0.00087338
v  Velocity[Z]              1.5653          5.4395          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4395          4.3406          4.3632
v  Pressure                -36.395          360.06          87.649          169.88
v  r11                   0.0010619        0.081901        0.013075        0.018286
v  r22                   0.0011151         0.08263        0.013355        0.018646
v  r33                   0.0016426         0.17428        0.027253        0.037207
v  r12                   -0.010665        0.013594     -0.00023384     -0.00030932
v  r13                   -0.045528        0.052801       9.327e-05       0.0010139
v  r23                   -0.046696        0.051196      3.0566e-05      0.00057463
v  epsilon                0.069304          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05       0.0099179      0.00092517       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2759         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8759         0.71351         0.85283


 TIME FOR THE TIME STEP            10849:        0.69761E+02

===============================================================


 INSTANT    0.108500000E-01   TIME STEP NUMBER           10850
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.402539548E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.631138279E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.465644515E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.738652565E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.598480113E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81224E-03   0.45285E-02 0.19928E+01 
c  Velocity[X]                                      0.13782E-03 
c  Velocity[Y]                                      0.12868E-03 
c  Velocity[Z]                                      0.42620E-02 
c  Pressure     0.36530E-04     132   0.92997E-02   0.25766E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58360E-08   0.16689E-08 0.10005E+00 
c  r22          0.10852E-01      13   0.61333E-08   0.18339E-08 0.10110E+00 
c  r33          0.21861E-01      15   0.64938E-08   0.12671E-07 0.12728E+00 
c  r12          0.93871E-03      18   0.61102E-08   0.30148E-09 0.60737E+00 
c  r13          0.46677E-02      20   0.60548E-08   0.15025E-08 0.19946E+00 
c  r23          0.39979E-02      19   0.71759E-08   0.13114E-08 0.20036E+00 
c  epsilon      0.10969E+02      11   0.34545E-08   0.97654E-02 0.16424E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.83835E-02 0.43189E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63329         0.61375       0.0052575       0.0015076
v  Velocity[Y]            -0.57364         0.54402        0.003081      0.00087336
v  Velocity[Z]              1.5655          5.4395          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4395          4.3406          4.3632
v  Pressure                -36.422          359.98          87.637          169.82
v  r11                   0.0010619        0.081901        0.013075        0.018286
v  r22                   0.0011151         0.08263        0.013355        0.018646
v  r33                   0.0016426          0.1743        0.027253        0.037207
v  r12                   -0.010665        0.013589     -0.00023384     -0.00030932
v  r13                   -0.045526        0.052802      9.3272e-05       0.0010139
v  r23                   -0.046697        0.051175      3.0567e-05      0.00057463
v  epsilon                0.069305          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05        0.009918      0.00092517       0.0017428
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2759         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8759         0.71352         0.85284


 TIME FOR THE TIME STEP            10850:        0.68087E+02

===============================================================


 INSTANT    0.108510000E-01   TIME STEP NUMBER           10851
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.259829105E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.171606104E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934902E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111286231E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.245502523E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100772609E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81315E-03   0.45206E-02 0.19916E+01 
c  Velocity[X]                                      0.13735E-03 
c  Velocity[Y]                                      0.12814E-03 
c  Velocity[Z]                                      0.42551E-02 
c  Pressure     0.35896E-04     133   0.91441E-02   0.25320E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55628E-08   0.17109E-08 0.10184E+00 
c  r22          0.10852E-01      13   0.55232E-08   0.18541E-08 0.10249E+00 
c  r33          0.21861E-01      15   0.52412E-08   0.12811E-07 0.12940E+00 
c  r12          0.93871E-03      18   0.51638E-08   0.30677E-09 0.61384E+00 
c  r13          0.46677E-02      19   0.61304E-08   0.15001E-08 0.20120E+00 
c  r23          0.39979E-02      19   0.68532E-08   0.13043E-08 0.20222E+00 
c  epsilon      0.10969E+02      11   0.32659E-08   0.95605E-02 0.16392E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.84039E-02 0.43229E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61373       0.0052576       0.0015076
v  Velocity[Y]            -0.57375         0.54407        0.003081      0.00087335
v  Velocity[Z]              1.5654          5.4395          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4395          4.3406          4.3632
v  Pressure                -36.417          360.06          87.671          169.88
v  r11                   0.0010619        0.081893        0.013075        0.018286
v  r22                   0.0011151        0.082624        0.013355        0.018646
v  r33                   0.0016426         0.17428        0.027253        0.037207
v  r12                   -0.010664        0.013589     -0.00023384     -0.00030932
v  r13                   -0.045525        0.052801      9.3273e-05       0.0010139
v  r23                   -0.046697        0.051204      3.0569e-05      0.00057463
v  epsilon                0.069306          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05        0.009918      0.00092517       0.0017428
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2769         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71351         0.85284


 TIME FOR THE TIME STEP            10851:        0.67543E+02

===============================================================


 INSTANT    0.108520000E-01   TIME STEP NUMBER           10852
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.358266800E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.234648869E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.442796759E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935012E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283447183E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.482799600E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81266E-03   0.44654E-02 0.19810E+01 
c  Velocity[X]                                      0.13683E-03 
c  Velocity[Y]                                      0.12794E-03 
c  Velocity[Z]                                      0.42006E-02 
c  Pressure     0.36346E-04     133   0.92491E-02   0.25636E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54610E-08   0.16669E-08 0.99741E-01 
c  r22          0.10852E-01      13   0.58807E-08   0.18732E-08 0.10174E+00 
c  r33          0.21861E-01      15   0.54206E-08   0.12788E-07 0.12742E+00 
c  r12          0.93871E-03      18   0.51337E-08   0.29887E-09 0.60590E+00 
c  r13          0.46677E-02      19   0.64647E-08   0.15226E-08 0.20011E+00 
c  r23          0.39979E-02      20   0.56969E-08   0.12869E-08 0.19884E+00 
c  epsilon      0.10969E+02      11   0.33813E-08   0.10506E-01 0.17145E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.84030E-02 0.43293E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61369       0.0052576       0.0015076
v  Velocity[Y]            -0.57368         0.54426        0.003081      0.00087336
v  Velocity[Z]              1.5653          5.4395          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4395          4.3406          4.3632
v  Pressure                -36.437             360          87.629          169.82
v  r11                   0.0010619        0.081895        0.013075        0.018286
v  r22                   0.0011151        0.082624        0.013355        0.018646
v  r33                   0.0016426         0.17426        0.027253        0.037207
v  r12                   -0.010662        0.013591     -0.00023384     -0.00030932
v  r13                   -0.045528        0.052802      9.3274e-05       0.0010139
v  r23                   -0.046698          0.0512      3.0569e-05      0.00057463
v  epsilon                0.069307          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05        0.009918      0.00092517       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2776         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            10852:        0.69084E+02

===============================================================


 INSTANT    0.108530000E-01   TIME STEP NUMBER           10853
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.452163741E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.127290916E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.376085112E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.193805148E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.679785414E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81213E-03   0.45190E-02 0.19904E+01 
c  Velocity[X]                                      0.13808E-03 
c  Velocity[Y]                                      0.12807E-03 
c  Velocity[Z]                                      0.42529E-02 
c  Pressure     0.36087E-04     132   0.91892E-02   0.25453E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54025E-08   0.16666E-08 0.10013E+00 
c  r22          0.10852E-01      13   0.61583E-08   0.18366E-08 0.10158E+00 
c  r33          0.21861E-01      14   0.69666E-08   0.12668E-07 0.12787E+00 
c  r12          0.93871E-03      18   0.58334E-08   0.30697E-09 0.61172E+00 
c  r13          0.46677E-02      19   0.60086E-08   0.14964E-08 0.19983E+00 
c  r23          0.39979E-02      19   0.64687E-08   0.13025E-08 0.20027E+00 
c  epsilon      0.10969E+02      11   0.34305E-08   0.10130E-01 0.17059E+00 
c  TempC        0.25716E+06      16   0.15184E-04   0.83717E-02 0.43215E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63326         0.61374       0.0052575       0.0015076
v  Velocity[Y]            -0.57372         0.54433       0.0030811      0.00087336
v  Velocity[Z]              1.5653          5.4395          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4395          4.3406          4.3632
v  Pressure                 -36.36          360.02          87.645          169.84
v  r11                   0.0010619        0.081894        0.013075        0.018286
v  r22                   0.0011152        0.082625        0.013355        0.018646
v  r33                   0.0016426         0.17427        0.027253        0.037207
v  r12                   -0.010659         0.01359     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052803      9.3274e-05       0.0010139
v  r23                   -0.046698        0.051187       3.057e-05      0.00057463
v  epsilon                0.069308          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099179      0.00092517       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017856          5.2775         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71352         0.85284


 TIME FOR THE TIME STEP            10853:        0.69301E+02

===============================================================


 INSTANT    0.108540000E-01   TIME STEP NUMBER           10854
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.289667931E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.176998832E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108275723E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.148948378E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.109148203E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81271E-03   0.45245E-02 0.19933E+01 
c  Velocity[X]                                      0.13751E-03 
c  Velocity[Y]                                      0.12819E-03 
c  Velocity[Z]                                      0.42588E-02 
c  Pressure     0.36308E-04     133   0.92411E-02   0.25609E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54250E-08   0.16346E-08 0.99649E-01 
c  r22          0.10852E-01      13   0.65653E-08   0.18376E-08 0.10166E+00 
c  r33          0.21861E-01      15   0.58215E-08   0.12537E-07 0.12756E+00 
c  r12          0.93871E-03      18   0.55807E-08   0.29699E-09 0.60504E+00 
c  r13          0.46677E-02      19   0.61435E-08   0.15203E-08 0.20144E+00 
c  r23          0.39979E-02      19   0.64826E-08   0.12850E-08 0.19931E+00 
c  epsilon      0.10969E+02      11   0.33325E-08   0.97070E-02 0.16396E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.84476E-02 0.43350E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63328         0.61371       0.0052575       0.0015076
v  Velocity[Y]            -0.57371         0.54423        0.003081      0.00087333
v  Velocity[Z]              1.5652          5.4395          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4395          4.3406          4.3632
v  Pressure                -36.423          360.06           87.66          169.87
v  r11                   0.0010619        0.081892        0.013075        0.018286
v  r22                   0.0011152        0.082627        0.013355        0.018646
v  r33                   0.0016426          0.1743        0.027253        0.037207
v  r12                    -0.01066        0.013589     -0.00023384     -0.00030932
v  r13                   -0.045526        0.052802      9.3275e-05       0.0010139
v  r23                   -0.046699         0.05121       3.057e-05      0.00057463
v  epsilon                0.069309          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099178      0.00092517       0.0017428
v  CourantNb                0.4426             0.6         0.59908         0.59839
v  FourierNb             0.0017857          5.2773         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71351         0.85283


 TIME FOR THE TIME STEP            10854:        0.68351E+02

===============================================================


 INSTANT    0.108550000E-01   TIME STEP NUMBER           10855
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158851576E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.432061807E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.612094485E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.118109250E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.133111598E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81330E-03   0.45240E-02 0.19910E+01 
c  Velocity[X]                                      0.13740E-03 
c  Velocity[Y]                                      0.12710E-03 
c  Velocity[Z]                                      0.42595E-02 
c  Pressure     0.36270E-04     133   0.92270E-02   0.25583E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56684E-08   0.16350E-08 0.98977E-01 
c  r22          0.10852E-01      13   0.63036E-08   0.18300E-08 0.10121E+00 
c  r33          0.21861E-01      15   0.55459E-08   0.12572E-07 0.12706E+00 
c  r12          0.93871E-03      18   0.60044E-08   0.29441E-09 0.60166E+00 
c  r13          0.46677E-02      19   0.67667E-08   0.15159E-08 0.20048E+00 
c  r23          0.39979E-02      19   0.54271E-08   0.12751E-08 0.19809E+00 
c  epsilon      0.10969E+02      11   0.32579E-08   0.97730E-02 0.16406E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.84417E-02 0.43344E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161986


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63333         0.61369       0.0052575       0.0015075
v  Velocity[Y]            -0.57394         0.54414        0.003081      0.00087331
v  Velocity[Z]              1.5653          5.4396          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4396          4.3406          4.3632
v  Pressure                -36.392          360.03          87.623          169.84
v  r11                   0.0010619        0.081901        0.013075        0.018286
v  r22                   0.0011152        0.082627        0.013355        0.018646
v  r33                   0.0016426         0.17429        0.027253        0.037207
v  r12                   -0.010667        0.013597     -0.00023384     -0.00030932
v  r13                   -0.045528          0.0528      9.3275e-05       0.0010139
v  r23                   -0.046699        0.051195      3.0571e-05      0.00057463
v  epsilon                 0.06931          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099177      0.00092517       0.0017428
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017857          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            10855:        0.66411E+02

===============================================================


 INSTANT    0.108560000E-01   TIME STEP NUMBER           10856
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.157168059E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.387457885E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.390515078E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.119764787E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.266376321E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81240E-03   0.44986E-02 0.19868E+01 
c  Velocity[X]                                      0.13786E-03 
c  Velocity[Y]                                      0.12872E-03 
c  Velocity[Z]                                      0.42320E-02 
c  Pressure     0.36197E-04     131   0.92094E-02   0.25532E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54709E-08   0.16177E-08 0.99076E-01 
c  r22          0.10852E-01      13   0.59230E-08   0.17963E-08 0.10060E+00 
c  r33          0.21861E-01      15   0.61193E-08   0.12237E-07 0.12602E+00 
c  r12          0.93871E-03      18   0.63221E-08   0.29241E-09 0.60296E+00 
c  r13          0.46677E-02      19   0.52568E-08   0.14668E-08 0.19839E+00 
c  r23          0.39979E-02      18   0.69773E-08   0.12498E-08 0.19688E+00 
c  epsilon      0.10969E+02      11   0.33577E-08   0.94886E-02 0.16229E+00 
c  TempC        0.25716E+06      16   0.15186E-04   0.83334E-02 0.43105E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61372       0.0052576       0.0015076
v  Velocity[Y]            -0.57391         0.54418        0.003081      0.00087331
v  Velocity[Z]              1.5652          5.4396          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4396          4.3406          4.3632
v  Pressure                -36.452          359.97          87.635          169.82
v  r11                   0.0010619        0.081896        0.013075        0.018286
v  r22                   0.0011152        0.082626        0.013355        0.018646
v  r33                   0.0016427         0.17426        0.027253        0.037207
v  r12                   -0.010666        0.013597     -0.00023384     -0.00030932
v  r13                   -0.045526        0.052799      9.3275e-05       0.0010139
v  r23                   -0.046699        0.051182      3.0571e-05      0.00057463
v  epsilon                0.069311          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099176      0.00092517       0.0017428
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017857          5.2777         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71351         0.85283


 TIME FOR THE TIME STEP            10856:        0.71020E+02

===============================================================


 INSTANT    0.108570000E-01   TIME STEP NUMBER           10857
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.193878879E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.128965936E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141381368E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.565861631E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209598552E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81188E-03   0.45038E-02 0.19883E+01 
c  Velocity[X]                                      0.13821E-03 
c  Velocity[Y]                                      0.12861E-03 
c  Velocity[Z]                                      0.42369E-02 
c  Pressure     0.36146E-04     133   0.92055E-02   0.25494E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53745E-08   0.16309E-08 0.98870E-01 
c  r22          0.10852E-01      13   0.57001E-08   0.18355E-08 0.10112E+00 
c  r33          0.21861E-01      15   0.62968E-08   0.12587E-07 0.12696E+00 
c  r12          0.93871E-03      18   0.51080E-08   0.28922E-09 0.59951E+00 
c  r13          0.46677E-02      19   0.55056E-08   0.15032E-08 0.19974E+00 
c  r23          0.39979E-02      18   0.69892E-08   0.12651E-08 0.19735E+00 
c  epsilon      0.10969E+02      11   0.34056E-08   0.10012E-01 0.16521E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.83975E-02 0.43239E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63332          0.6137       0.0052576       0.0015076
v  Velocity[Y]            -0.57396         0.54431       0.0030811      0.00087334
v  Velocity[Z]              1.5653          5.4396          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4396          4.3406          4.3632
v  Pressure                -36.395          360.03          87.661          169.87
v  r11                   0.0010619        0.081898        0.013075        0.018286
v  r22                   0.0011152        0.082626        0.013355        0.018646
v  r33                   0.0016427         0.17428        0.027253        0.037207
v  r12                   -0.010664        0.013592     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052799      9.3277e-05       0.0010139
v  r23                   -0.046699        0.051171      3.0572e-05      0.00057463
v  epsilon                0.069311          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099176      0.00092517       0.0017428
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017857          5.2778         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71351         0.85284


 TIME FOR THE TIME STEP            10857:        0.70906E+02

===============================================================


 INSTANT    0.108580000E-01   TIME STEP NUMBER           10858
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.519406265E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249767343E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.290828757E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.237953486E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200807398E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81345E-03   0.45129E-02 0.19908E+01 
c  Velocity[X]                                      0.13757E-03 
c  Velocity[Y]                                      0.12807E-03 
c  Velocity[Z]                                      0.42473E-02 
c  Pressure     0.36366E-04     133   0.92653E-02   0.25649E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54983E-08   0.16355E-08 0.99480E-01 
c  r22          0.10852E-01      13   0.54846E-08   0.18166E-08 0.10116E+00 
c  r33          0.21861E-01      15   0.62219E-08   0.12445E-07 0.12680E+00 
c  r12          0.93871E-03      18   0.51184E-08   0.29769E-09 0.60366E+00 
c  r13          0.46677E-02      18   0.67592E-08   0.14712E-08 0.19921E+00 
c  r23          0.39979E-02      19   0.52737E-08   0.12749E-08 0.19847E+00 
c  epsilon      0.10969E+02      11   0.35004E-08   0.97376E-02 0.16452E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.84038E-02 0.43220E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61368       0.0052575       0.0015076
v  Velocity[Y]            -0.57377         0.54414        0.003081      0.00087331
v  Velocity[Z]              1.5654          5.4396          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4396          4.3406          4.3632
v  Pressure                -36.454          360.01          87.654          169.85
v  r11                   0.0010619        0.081899        0.013075        0.018286
v  r22                   0.0011152        0.082626        0.013355        0.018646
v  r33                   0.0016427          0.1743        0.027253        0.037207
v  r12                   -0.010663        0.013597     -0.00023384     -0.00030932
v  r13                   -0.045529        0.052799      9.3277e-05       0.0010139
v  r23                     -0.0467        0.051202      3.0573e-05      0.00057463
v  epsilon                0.069312          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099175      0.00092517       0.0017428
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017857          5.2775         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71352         0.85284


 TIME FOR THE TIME STEP            10858:        0.70324E+02

===============================================================


 INSTANT    0.108590000E-01   TIME STEP NUMBER           10859
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.476051908E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.828664108E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169368529E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195066176E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.604151736E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81262E-03   0.45218E-02 0.19927E+01 
c  Velocity[X]                                      0.13693E-03 
c  Velocity[Y]                                      0.12787E-03 
c  Velocity[Z]                                      0.42570E-02 
c  Pressure     0.36421E-04     133   0.92727E-02   0.25690E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56544E-08   0.16787E-08 0.10053E+00 
c  r22          0.10852E-01      13   0.53579E-08   0.18543E-08 0.10189E+00 
c  r33          0.21861E-01      15   0.52984E-08   0.12837E-07 0.12846E+00 
c  r12          0.93871E-03      18   0.54912E-08   0.30122E-09 0.60784E+00 
c  r13          0.46677E-02      18   0.70025E-08   0.15109E-08 0.20145E+00 
c  r23          0.39979E-02      18   0.67293E-08   0.13055E-08 0.20128E+00 
c  epsilon      0.10969E+02      11   0.32730E-08   0.10533E-01 0.17206E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.84556E-02 0.43363E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61373       0.0052576       0.0015076
v  Velocity[Y]            -0.57378         0.54409        0.003081      0.00087331
v  Velocity[Z]              1.5652          5.4396          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4396          4.3406          4.3632
v  Pressure                -36.396          360.07           87.66          169.88
v  r11                   0.0010619        0.081897        0.013075        0.018286
v  r22                   0.0011152        0.082621        0.013355        0.018646
v  r33                   0.0016427         0.17428        0.027253        0.037207
v  r12                   -0.010662        0.013594     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052799      9.3277e-05       0.0010139
v  r23                     -0.0467        0.051206      3.0573e-05      0.00057463
v  epsilon                0.069313          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099174      0.00092518       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017857          5.2779         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71351         0.85284


 TIME FOR THE TIME STEP            10859:        0.69930E+02

===============================================================


 INSTANT    0.108600000E-01   TIME STEP NUMBER           10860
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.172015727E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.682907678E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.611189262E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173991107E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.240987679E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81264E-03   0.45017E-02 0.19865E+01 
c  Velocity[X]                                      0.13815E-03 
c  Velocity[Y]                                      0.12737E-03 
c  Velocity[Z]                                      0.42362E-02 
c  Pressure     0.35604E-04     132   0.90719E-02   0.25113E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57346E-08   0.16479E-08 0.99771E-01 
c  r22          0.10852E-01      13   0.55507E-08   0.18530E-08 0.10164E+00 
c  r33          0.21861E-01      15   0.52416E-08   0.12654E-07 0.12771E+00 
c  r12          0.93871E-03      18   0.52760E-08   0.30172E-09 0.60829E+00 
c  r13          0.46677E-02      19   0.57106E-08   0.15095E-08 0.20068E+00 
c  r23          0.39979E-02      19   0.51073E-08   0.12765E-08 0.19964E+00 
c  epsilon      0.10969E+02      11   0.33032E-08   0.99971E-02 0.16634E+00 
c  TempC        0.25716E+06      16   0.15188E-04   0.83968E-02 0.43338E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63326         0.61371       0.0052575       0.0015076
v  Velocity[Y]            -0.57366         0.54416        0.003081      0.00087331
v  Velocity[Z]              1.5653          5.4396          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4396          4.3406          4.3632
v  Pressure                -36.424          360.03          87.646          169.85
v  r11                   0.0010619        0.081896        0.013075        0.018286
v  r22                   0.0011152        0.082621        0.013355        0.018646
v  r33                   0.0016427         0.17426        0.027253        0.037207
v  r12                   -0.010661        0.013591     -0.00023384     -0.00030932
v  r13                   -0.045525        0.052799      9.3278e-05       0.0010139
v  r23                     -0.0467        0.051188      3.0573e-05      0.00057463
v  epsilon                0.069314          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9911e-05       0.0099176      0.00092518       0.0017428
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017857          5.2779         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            10860:        0.67370E+02

===============================================================


 INSTANT    0.108610000E-01   TIME STEP NUMBER           10861
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201425679E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.135402071E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221977034E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191590327E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162706076E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81352E-03   0.45013E-02 0.19868E+01 
c  Velocity[X]                                      0.13839E-03 
c  Velocity[Y]                                      0.12760E-03 
c  Velocity[Z]                                      0.42353E-02 
c  Pressure     0.36416E-04     133   0.92702E-02   0.25685E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57896E-08   0.16227E-08 0.98885E-01 
c  r22          0.10852E-01      13   0.53266E-08   0.18550E-08 0.10171E+00 
c  r33          0.21861E-01      15   0.59076E-08   0.12614E-07 0.12733E+00 
c  r12          0.93871E-03      18   0.50969E-08   0.29415E-09 0.60161E+00 
c  r13          0.46677E-02      19   0.54720E-08   0.15212E-08 0.20055E+00 
c  r23          0.39979E-02      19   0.54743E-08   0.12798E-08 0.19819E+00 
c  epsilon      0.10969E+02      11   0.35217E-08   0.99739E-02 0.16501E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.83159E-02 0.43049E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63329         0.61368       0.0052575       0.0015075
v  Velocity[Y]            -0.57366         0.54424        0.003081      0.00087328
v  Velocity[Z]              1.5651          5.4396          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4396          4.3406          4.3632
v  Pressure                -36.422          360.01          87.634          169.84
v  r11                   0.0010619        0.081889        0.013075        0.018286
v  r22                   0.0011152        0.082622        0.013355        0.018646
v  r33                   0.0016427         0.17427        0.027253        0.037207
v  r12                   -0.010656        0.013597     -0.00023384     -0.00030932
v  r13                    -0.04553        0.052796      9.3278e-05       0.0010139
v  r23                     -0.0467        0.051215      3.0573e-05      0.00057463
v  epsilon                0.069315          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9909e-05       0.0099178      0.00092518       0.0017428
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017857          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            10861:        0.70833E+02

===============================================================


 INSTANT    0.108620000E-01   TIME STEP NUMBER           10862
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.314806787E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.256918486E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.207062969E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.147720170E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.226195347E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81267E-03   0.45129E-02 0.19895E+01 
c  Velocity[X]                                      0.13673E-03 
c  Velocity[Y]                                      0.12804E-03 
c  Velocity[Z]                                      0.42482E-02 
c  Pressure     0.36251E-04     131   0.92231E-02   0.25570E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55678E-08   0.16435E-08 0.99213E-01 
c  r22          0.10852E-01      13   0.51252E-08   0.18334E-08 0.10111E+00 
c  r33          0.21861E-01      15   0.59435E-08   0.12501E-07 0.12698E+00 
c  r12          0.93871E-03      18   0.51890E-08   0.29699E-09 0.60439E+00 
c  r13          0.46677E-02      18   0.72579E-08   0.14835E-08 0.19845E+00 
c  r23          0.39979E-02      18   0.71056E-08   0.12840E-08 0.19931E+00 
c  epsilon      0.10969E+02      11   0.36034E-08   0.96943E-02 0.16324E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83946E-02 0.43163E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61371       0.0052576       0.0015076
v  Velocity[Y]            -0.57373         0.54403        0.003081      0.00087329
v  Velocity[Z]              1.5651          5.4396          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4396          4.3406          4.3632
v  Pressure                -36.412          359.97          87.634          169.81
v  r11                   0.0010619        0.081892        0.013075        0.018286
v  r22                   0.0011152        0.082622        0.013355        0.018646
v  r33                   0.0016427         0.17429        0.027253        0.037207
v  r12                   -0.010656        0.013596     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052798      9.3278e-05       0.0010139
v  r23                     -0.0467        0.051203      3.0574e-05      0.00057463
v  epsilon                0.069316          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9906e-05       0.0099179      0.00092518       0.0017428
v  CourantNb               0.44259             0.6         0.59908         0.59839
v  FourierNb             0.0017857          5.2783         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71352         0.85284


 TIME FOR THE TIME STEP            10862:        0.72137E+02

===============================================================


 INSTANT    0.108630000E-01   TIME STEP NUMBER           10863
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.475266125E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.147383541E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.433369165E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133879567E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.303063230E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40349E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81239E-03   0.44890E-02 0.19840E+01 
c  Velocity[X]                                      0.13806E-03 
c  Velocity[Y]                                      0.12823E-03 
c  Velocity[Z]                                      0.42227E-02 
c  Pressure     0.36284E-04     133   0.92369E-02   0.25593E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52865E-08   0.16092E-08 0.98313E-01 
c  r22          0.10852E-01      13   0.50982E-08   0.17940E-08 0.10034E+00 
c  r33          0.21861E-01      15   0.59286E-08   0.12277E-07 0.12583E+00 
c  r12          0.93871E-03      18   0.48667E-08   0.28505E-09 0.59632E+00 
c  r13          0.46677E-02      19   0.54572E-08   0.14650E-08 0.19822E+00 
c  r23          0.39979E-02      18   0.69751E-08   0.12470E-08 0.19595E+00 
c  epsilon      0.10969E+02      11   0.35407E-08   0.95133E-02 0.16271E+00 
c  TempC        0.25716E+06      16   0.15110E-04   0.84708E-02 0.43412E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61371       0.0052577       0.0015076
v  Velocity[Y]            -0.57389         0.54415       0.0030811      0.00087336
v  Velocity[Z]              1.5652          5.4396          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4396          4.3406          4.3632
v  Pressure                -36.392          360.03          87.657          169.86
v  r11                   0.0010619        0.081904        0.013075        0.018286
v  r22                   0.0011152        0.082623        0.013355        0.018646
v  r33                   0.0016427         0.17433        0.027253        0.037207
v  r12                   -0.010657        0.013591     -0.00023384     -0.00030932
v  r13                   -0.045526        0.052796      9.3278e-05       0.0010139
v  r23                     -0.0467        0.051197      3.0575e-05      0.00057463
v  epsilon                0.069317          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9903e-05        0.009918      0.00092518       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017857          5.2784         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71351         0.85283


 TIME FOR THE TIME STEP            10863:        0.71830E+02

===============================================================


 INSTANT    0.108640000E-01   TIME STEP NUMBER           10864
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.314940083E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.470195661E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.149629592E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935011E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.328269294E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.395707254E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81312E-03   0.44888E-02 0.19847E+01 
c  Velocity[X]                                      0.13753E-03 
c  Velocity[Y]                                      0.12812E-03 
c  Velocity[Z]                                      0.42231E-02 
c  Pressure     0.36425E-04     132   0.92711E-02   0.25692E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50746E-08   0.16605E-08 0.99210E-01 
c  r22          0.10852E-01      13   0.50070E-08   0.18379E-08 0.10085E+00 
c  r33          0.21861E-01      15   0.58971E-08   0.12790E-07 0.12741E+00 
c  r12          0.93871E-03      18   0.52515E-08   0.29836E-09 0.60253E+00 
c  r13          0.46677E-02      18   0.63149E-08   0.15058E-08 0.19973E+00 
c  r23          0.39979E-02      18   0.70555E-08   0.13083E-08 0.20032E+00 
c  epsilon      0.10969E+02      11   0.34422E-08   0.10465E-01 0.17128E+00 
c  TempC        0.25716E+06      16   0.15192E-04   0.83934E-02 0.43222E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63322         0.61366       0.0052575       0.0015075
v  Velocity[Y]            -0.57387         0.54434        0.003081      0.00087332
v  Velocity[Z]              1.5651          5.4396          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4396          4.3406          4.3632
v  Pressure                -36.484          359.99          87.622          169.82
v  r11                   0.0010619        0.081903        0.013075        0.018286
v  r22                   0.0011152        0.082622        0.013355        0.018646
v  r33                   0.0016427         0.17431        0.027253        0.037207
v  r12                   -0.010656        0.013588     -0.00023384     -0.00030932
v  r13                   -0.045528        0.052795      9.3278e-05       0.0010139
v  r23                   -0.046701        0.051223      3.0575e-05      0.00057463
v  epsilon                0.069318          271.26          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc               5.99e-05       0.0099182      0.00092518       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017857          5.2777         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            10864:        0.70512E+02

===============================================================


 INSTANT    0.108650000E-01   TIME STEP NUMBER           10865
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.663411897E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.248213089E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.712537611E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161055670E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205351845E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81263E-03   0.45212E-02 0.19918E+01 
c  Velocity[X]                                      0.13739E-03 
c  Velocity[Y]                                      0.12772E-03 
c  Velocity[Z]                                      0.42561E-02 
c  Pressure     0.36274E-04     131   0.92351E-02   0.25586E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53995E-08   0.16402E-08 0.98451E-01 
c  r22          0.10852E-01      13   0.51488E-08   0.18406E-08 0.10100E+00 
c  r33          0.21861E-01      14   0.70408E-08   0.12577E-07 0.12624E+00 
c  r12          0.93871E-03      18   0.52373E-08   0.30151E-09 0.60485E+00 
c  r13          0.46677E-02      18   0.63206E-08   0.14931E-08 0.19885E+00 
c  r23          0.39979E-02      19   0.54910E-08   0.12916E-08 0.19794E+00 
c  epsilon      0.10969E+02      11   0.34809E-08   0.10071E-01 0.16566E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84199E-02 0.43269E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63328         0.61372       0.0052575       0.0015076
v  Velocity[Y]             -0.5738         0.54403        0.003081      0.00087332
v  Velocity[Z]              1.5654          5.4396          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4396          4.3406          4.3632
v  Pressure                -36.387          360.04          87.646          169.85
v  r11                   0.0010619        0.081901        0.013075        0.018286
v  r22                   0.0011152        0.082622        0.013355        0.018646
v  r33                   0.0016427         0.17428        0.027253        0.037207
v  r12                   -0.010656        0.013583     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052795      9.3278e-05       0.0010139
v  r23                   -0.046701        0.051209      3.0575e-05      0.00057463
v  epsilon                0.069319          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9898e-05       0.0099184      0.00092518       0.0017428
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017857          5.2778         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71351         0.85284


 TIME FOR THE TIME STEP            10865:        0.68230E+02

===============================================================


 INSTANT    0.108660000E-01   TIME STEP NUMBER           10866
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.642450030E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171147274E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.175363777E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108447619E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.557938940E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81308E-03   0.45439E-02 0.19982E+01 
c  Velocity[X]                                      0.13844E-03 
c  Velocity[Y]                                      0.12811E-03 
c  Velocity[Z]                                      0.42773E-02 
c  Pressure     0.36497E-04     133   0.92885E-02   0.25743E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54340E-08   0.16353E-08 0.98764E-01 
c  r22          0.10852E-01      13   0.52421E-08   0.18392E-08 0.10121E+00 
c  r33          0.21861E-01      14   0.67896E-08   0.12533E-07 0.12660E+00 
c  r12          0.93871E-03      18   0.48350E-08   0.29356E-09 0.59788E+00 
c  r13          0.46677E-02      18   0.66596E-08   0.15138E-08 0.20017E+00 
c  r23          0.39979E-02      18   0.71877E-08   0.12860E-08 0.19809E+00 
c  epsilon      0.10969E+02      11   0.32741E-08   0.97990E-02 0.16372E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.83916E-02 0.43278E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61371       0.0052576       0.0015076
v  Velocity[Y]            -0.57384         0.54406        0.003081      0.00087331
v  Velocity[Z]              1.5654          5.4396          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4396          4.3406          4.3632
v  Pressure                -36.447          359.98           87.62          169.81
v  r11                   0.0010619        0.081897        0.013075        0.018286
v  r22                   0.0011152        0.082622        0.013355        0.018646
v  r33                   0.0016427          0.1743        0.027253        0.037207
v  r12                   -0.010656        0.013585     -0.00023384     -0.00030932
v  r13                   -0.045526        0.052795      9.3279e-05       0.0010139
v  r23                   -0.046702        0.051188      3.0575e-05      0.00057463
v  epsilon                 0.06932          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9894e-05       0.0099184      0.00092518       0.0017428
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2787         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85284


 TIME FOR THE TIME STEP            10866:        0.69664E+02

===============================================================


 INSTANT    0.108670000E-01   TIME STEP NUMBER           10867
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.549700984E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.193261051E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.213659929E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.281608768E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.314635277E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81269E-03   0.45069E-02 0.19881E+01 
c  Velocity[X]                                      0.13704E-03 
c  Velocity[Y]                                      0.12772E-03 
c  Velocity[Z]                                      0.42422E-02 
c  Pressure     0.36153E-04     132   0.92040E-02   0.25500E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55021E-08   0.16629E-08 0.99587E-01 
c  r22          0.10852E-01      13   0.51107E-08   0.18571E-08 0.10182E+00 
c  r33          0.21861E-01      15   0.52620E-08   0.12710E-07 0.12759E+00 
c  r12          0.93871E-03      18   0.50037E-08   0.29556E-09 0.60079E+00 
c  r13          0.46677E-02      18   0.61191E-08   0.14996E-08 0.20052E+00 
c  r23          0.39979E-02      18   0.69098E-08   0.12881E-08 0.19903E+00 
c  epsilon      0.10969E+02      11   0.33316E-08   0.10283E-01 0.16944E+00 
c  TempC        0.25716E+06      16   0.15124E-04   0.83846E-02 0.43178E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161988


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63335         0.61368       0.0052576       0.0015076
v  Velocity[Y]            -0.57386         0.54417       0.0030809       0.0008733
v  Velocity[Z]              1.5651          5.4396          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4396          4.3406          4.3632
v  Pressure                -36.407          360.04          87.649          169.86
v  r11                   0.0010619        0.081895        0.013075        0.018286
v  r22                   0.0011153        0.082617        0.013355        0.018646
v  r33                   0.0016428         0.17432        0.027253        0.037207
v  r12                   -0.010655         0.01358     -0.00023384     -0.00030932
v  r13                   -0.045529        0.052795      9.3279e-05       0.0010139
v  r23                   -0.046702        0.051213      3.0575e-05      0.00057463
v  epsilon                0.069321          271.25          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9892e-05       0.0099182      0.00092518       0.0017428
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            10867:        0.74599E+02

===============================================================


 INSTANT    0.108680000E-01   TIME STEP NUMBER           10868
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.373837891E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.237090334E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.213127034E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.477069314E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.160444350E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12293E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81308E-03   0.45144E-02 0.19857E+01 
c  Velocity[X]                                      0.13780E-03 
c  Velocity[Y]                                      0.12838E-03 
c  Velocity[Z]                                      0.42482E-02 
c  Pressure     0.36262E-04     133   0.92238E-02   0.25577E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.61027E-08   0.16585E-08 0.99527E-01 
c  r22          0.10852E-01      13   0.54570E-08   0.18534E-08 0.10133E+00 
c  r33          0.21861E-01      15   0.53114E-08   0.12692E-07 0.12727E+00 
c  r12          0.93871E-03      18   0.64282E-08   0.29912E-09 0.60485E+00 
c  r13          0.46677E-02      18   0.67708E-08   0.15080E-08 0.19971E+00 
c  r23          0.39979E-02      19   0.55865E-08   0.13016E-08 0.20024E+00 
c  epsilon      0.10969E+02      11   0.35776E-08   0.10154E-01 0.16889E+00 
c  TempC        0.25716E+06      16   0.15164E-04   0.83992E-02 0.43253E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61374       0.0052576       0.0015076
v  Velocity[Y]            -0.57377         0.54429        0.003081      0.00087331
v  Velocity[Z]              1.5652          5.4396          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4396          4.3406          4.3632
v  Pressure                -36.429          359.99          87.631          169.82
v  r11                   0.0010619         0.08189        0.013075        0.018286
v  r22                   0.0011153        0.082616        0.013355        0.018646
v  r33                   0.0016428         0.17429        0.027254        0.037207
v  r12                   -0.010658        0.013582     -0.00023384     -0.00030932
v  r13                   -0.045526        0.052797      9.3278e-05       0.0010139
v  r23                   -0.046702        0.051207      3.0576e-05      0.00057463
v  epsilon                0.069322          271.26          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9888e-05       0.0099182      0.00092518       0.0017428
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2786         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            10868:        0.74256E+02

===============================================================


 INSTANT    0.108690000E-01   TIME STEP NUMBER           10869
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.174254871E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.125515231E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.960150025E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.231456632E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.372498794E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69749E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81204E-03   0.45053E-02 0.19873E+01 
c  Velocity[X]                                      0.13803E-03 
c  Velocity[Y]                                      0.12713E-03 
c  Velocity[Z]                                      0.42401E-02 
c  Pressure     0.36371E-04     132   0.92590E-02   0.25655E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58924E-08   0.16354E-08 0.99292E-01 
c  r22          0.10852E-01      13   0.53498E-08   0.18396E-08 0.10140E+00 
c  r33          0.21861E-01      15   0.61019E-08   0.12517E-07 0.12709E+00 
c  r12          0.93871E-03      18   0.66425E-08   0.29419E-09 0.60269E+00 
c  r13          0.46677E-02      19   0.59788E-08   0.15181E-08 0.20116E+00 
c  r23          0.39979E-02      19   0.65701E-08   0.12768E-08 0.19902E+00 
c  epsilon      0.10969E+02      11   0.34182E-08   0.98436E-02 0.16490E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.84101E-02 0.43291E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343          0.6137       0.0052576       0.0015076
v  Velocity[Y]            -0.57383         0.54422       0.0030811      0.00087336
v  Velocity[Z]              1.5648          5.4397          4.3387          4.3625
v  ǁVelocityǁ               1.5786          5.4397          4.3406          4.3632
v  Pressure                -36.373          360.05          87.648          169.86
v  r11                   0.0010619        0.081889        0.013075        0.018286
v  r22                   0.0011153        0.082618        0.013355        0.018646
v  r33                   0.0016428         0.17427        0.027254        0.037207
v  r12                    -0.01066        0.013579     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052797      9.3278e-05       0.0010139
v  r23                   -0.046702        0.051187      3.0576e-05      0.00057463
v  epsilon                0.069323          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9885e-05       0.0099183      0.00092518       0.0017428
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            10869:        0.74592E+02

===============================================================


 INSTANT    0.108700000E-01   TIME STEP NUMBER           10870
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.286123792E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.236904961E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178895601E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.396175823E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.177557199E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81277E-03   0.45157E-02 0.19920E+01 
c  Velocity[X]                                      0.13777E-03 
c  Velocity[Y]                                      0.12773E-03 
c  Velocity[Z]                                      0.42502E-02 
c  Pressure     0.36459E-04     133   0.92806E-02   0.25716E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57618E-08   0.16518E-08 0.99608E-01 
c  r22          0.10852E-01      13   0.50408E-08   0.18267E-08 0.10135E+00 
c  r33          0.21861E-01      15   0.61363E-08   0.12617E-07 0.12775E+00 
c  r12          0.93871E-03      18   0.57746E-08   0.29465E-09 0.60359E+00 
c  r13          0.46677E-02      19   0.69837E-08   0.14811E-08 0.19975E+00 
c  r23          0.39979E-02      18   0.70246E-08   0.12910E-08 0.20027E+00 
c  epsilon      0.10969E+02      11   0.32313E-08   0.10101E-01 0.17050E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.83634E-02 0.43139E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63328         0.61366       0.0052575       0.0015076
v  Velocity[Y]            -0.57383          0.5441       0.0030809      0.00087328
v  Velocity[Z]              1.5651          5.4397          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4397          4.3406          4.3632
v  Pressure                -36.473             360          87.647          169.84
v  r11                   0.0010619        0.081884        0.013075        0.018286
v  r22                   0.0011153        0.082618        0.013355        0.018646
v  r33                   0.0016428         0.17429        0.027254        0.037207
v  r12                    -0.01066        0.013586     -0.00023384     -0.00030932
v  r13                   -0.045529        0.052797      9.3278e-05       0.0010139
v  r23                   -0.046703        0.051207      3.0576e-05      0.00057463
v  epsilon                0.069324          271.27          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9882e-05       0.0099181      0.00092518       0.0017428
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2788         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71351         0.85283


 TIME FOR THE TIME STEP            10870:        0.76808E+02

===============================================================


 INSTANT    0.108710000E-01   TIME STEP NUMBER           10871
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.197732051E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.454108888E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.556946675E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.161370959E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172067840E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69747E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81272E-03   0.45298E-02 0.19936E+01 
c  Velocity[X]                                      0.13831E-03 
c  Velocity[Y]                                      0.12902E-03 
c  Velocity[Z]                                      0.42624E-02 
c  Pressure     0.36314E-04     131   0.92443E-02   0.25614E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55778E-08   0.16550E-08 0.99952E-01 
c  r22          0.10852E-01      13   0.48670E-08   0.18557E-08 0.10177E+00 
c  r33          0.21861E-01      15   0.71433E-08   0.12659E-07 0.12773E+00 
c  r12          0.93872E-03      18   0.53232E-08   0.29716E-09 0.60623E+00 
c  r13          0.46677E-02      19   0.73961E-08   0.15088E-08 0.20039E+00 
c  r23          0.39979E-02      19   0.64517E-08   0.12839E-08 0.19969E+00 
c  epsilon      0.10969E+02      11   0.33377E-08   0.99778E-02 0.16594E+00 
c  TempC        0.25716E+06      16   0.15127E-04   0.84029E-02 0.43256E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63327          0.6137       0.0052576       0.0015076
v  Velocity[Y]            -0.57388         0.54416       0.0030809       0.0008733
v  Velocity[Z]              1.5654          5.4397          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4397          4.3406          4.3632
v  Pressure                  -36.4          360.03          87.649          169.85
v  r11                   0.0010619        0.081885        0.013075        0.018286
v  r22                   0.0011153        0.082617        0.013355        0.018646
v  r33                   0.0016428         0.17431        0.027254        0.037207
v  r12                    -0.01066        0.013583     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052796      9.3277e-05       0.0010139
v  r23                   -0.046703        0.051186      3.0575e-05      0.00057463
v  epsilon                0.069325          271.29          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9879e-05        0.009918      0.00092518       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2782         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            10871:        0.77641E+02

===============================================================


 INSTANT    0.108720000E-01   TIME STEP NUMBER           10872
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.912518824E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.385516299E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.348171554E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.450995772E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.432178378E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81330E-03   0.44906E-02 0.19844E+01 
c  Velocity[X]                                      0.13767E-03 
c  Velocity[Y]                                      0.12797E-03 
c  Velocity[Z]                                      0.42250E-02 
c  Pressure     0.36091E-04     133   0.91901E-02   0.25457E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57162E-08   0.16688E-08 0.99933E-01 
c  r22          0.10852E-01      13   0.53896E-08   0.18552E-08 0.10174E+00 
c  r33          0.21861E-01      15   0.72897E-08   0.12779E-07 0.12801E+00 
c  r12          0.93872E-03      18   0.65140E-08   0.29785E-09 0.60415E+00 
c  r13          0.46677E-02      20   0.57346E-08   0.15230E-08 0.20050E+00 
c  r23          0.39979E-02      19   0.65381E-08   0.13161E-08 0.20149E+00 
c  epsilon      0.10969E+02      11   0.33924E-08   0.99678E-02 0.16579E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.84885E-02 0.43494E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61367       0.0052575       0.0015075
v  Velocity[Y]            -0.57384         0.54429       0.0030809       0.0008733
v  Velocity[Z]              1.5653          5.4397          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4397          4.3406          4.3632
v  Pressure                -36.456          360.06          87.684          169.89
v  r11                   0.0010619        0.081876        0.013075        0.018286
v  r22                   0.0011153        0.082617        0.013355        0.018646
v  r33                   0.0016428         0.17435        0.027254        0.037207
v  r12                   -0.010659        0.013578     -0.00023384     -0.00030932
v  r13                   -0.045525        0.052797      9.3277e-05       0.0010139
v  r23                   -0.046703        0.051171      3.0575e-05      0.00057463
v  epsilon                0.069326          271.29          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9876e-05       0.0099181      0.00092518       0.0017428
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2782         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            10872:        0.72444E+02

===============================================================


 INSTANT    0.108730000E-01   TIME STEP NUMBER           10873
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267049608E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136254530E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.289946314E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935023E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.340936013E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.103884481E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81226E-03   0.44986E-02 0.19865E+01 
c  Velocity[X]                                      0.13736E-03 
c  Velocity[Y]                                      0.12792E-03 
c  Velocity[Z]                                      0.42333E-02 
c  Pressure     0.35983E-04     132   0.91564E-02   0.25380E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56719E-08   0.16336E-08 0.99088E-01 
c  r22          0.10852E-01      13   0.53425E-08   0.18427E-08 0.10115E+00 
c  r33          0.21861E-01      15   0.62174E-08   0.12556E-07 0.12674E+00 
c  r12          0.93872E-03      18   0.69524E-08   0.29570E-09 0.60143E+00 
c  r13          0.46677E-02      19   0.67365E-08   0.14864E-08 0.19870E+00 
c  r23          0.39979E-02      19   0.59808E-08   0.12746E-08 0.19845E+00 
c  epsilon      0.10969E+02      11   0.33680E-08   0.99785E-02 0.16536E+00 
c  TempC        0.25716E+06      16   0.15142E-04   0.83578E-02 0.43095E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61365       0.0052575       0.0015075
v  Velocity[Y]            -0.57395         0.54408       0.0030809      0.00087331
v  Velocity[Z]              1.5654          5.4397          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4397          4.3406          4.3632
v  Pressure                -36.396          360.04          87.628          169.85
v  r11                   0.0010619        0.081867        0.013075        0.018286
v  r22                   0.0011153        0.082617        0.013355        0.018646
v  r33                   0.0016428         0.17433        0.027254        0.037207
v  r12                   -0.010656        0.013576     -0.00023384     -0.00030932
v  r13                    -0.04553        0.052798      9.3277e-05       0.0010139
v  r23                   -0.046703        0.051158      3.0575e-05      0.00057463
v  epsilon                0.069327          271.32          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9876e-05       0.0099181      0.00092519       0.0017428
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2779         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            10873:        0.73885E+02

===============================================================


 INSTANT    0.108740000E-01   TIME STEP NUMBER           10874
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.185097889E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.276406581E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.315095253E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.735935169E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.371399799E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81266E-03   0.45174E-02 0.19910E+01 
c  Velocity[X]                                      0.13796E-03 
c  Velocity[Y]                                      0.12826E-03 
c  Velocity[Z]                                      0.42512E-02 
c  Pressure     0.36377E-04     132   0.92647E-02   0.25659E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56904E-08   0.16469E-08 0.99435E-01 
c  r22          0.10852E-01      13   0.54939E-08   0.18195E-08 0.10127E+00 
c  r33          0.21861E-01      15   0.74449E-08   0.12471E-07 0.12702E+00 
c  r12          0.93872E-03      18   0.71905E-08   0.29495E-09 0.60032E+00 
c  r13          0.46677E-02      19   0.67662E-08   0.14791E-08 0.19913E+00 
c  r23          0.39979E-02      19   0.72780E-08   0.12765E-08 0.19893E+00 
c  epsilon      0.10969E+02      11   0.35408E-08   0.98961E-02 0.16617E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.84153E-02 0.43245E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63324         0.61372       0.0052576       0.0015076
v  Velocity[Y]            -0.57388          0.5442       0.0030809      0.00087332
v  Velocity[Z]              1.5653          5.4397          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4397          4.3406          4.3632
v  Pressure                -36.428          359.96          87.624          169.81
v  r11                   0.0010619         0.08186        0.013075        0.018286
v  r22                   0.0011153        0.082617        0.013355        0.018646
v  r33                   0.0016428         0.17429        0.027254        0.037207
v  r12                   -0.010656        0.013579     -0.00023384     -0.00030932
v  r13                   -0.045528        0.052798      9.3277e-05       0.0010139
v  r23                   -0.046703        0.051178      3.0575e-05      0.00057463
v  epsilon                0.069328          271.29          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9874e-05        0.009918      0.00092519       0.0017428
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2777         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            10874:        0.74682E+02

===============================================================


 INSTANT    0.108750000E-01   TIME STEP NUMBER           10875
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.424807113E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.156474849E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.210210304E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.420878084E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150107000E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69746E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81309E-03   0.45137E-02 0.19884E+01 
c  Velocity[X]                                      0.13845E-03 
c  Velocity[Y]                                      0.12795E-03 
c  Velocity[Z]                                      0.42473E-02 
c  Pressure     0.36088E-04     133   0.91968E-02   0.25454E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56893E-08   0.16142E-08 0.98992E-01 
c  r22          0.10852E-01      13   0.55413E-08   0.17988E-08 0.10054E+00 
c  r33          0.21861E-01      15   0.68286E-08   0.12293E-07 0.12619E+00 
c  r12          0.93872E-03      19   0.59111E-08   0.29630E-09 0.60140E+00 
c  r13          0.46677E-02      19   0.71596E-08   0.14767E-08 0.19886E+00 
c  r23          0.39979E-02      20   0.60320E-08   0.12546E-08 0.19697E+00 
c  epsilon      0.10969E+02      11   0.35283E-08   0.96391E-02 0.16402E+00 
c  TempC        0.25716E+06      16   0.15114E-04   0.84598E-02 0.43369E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63328         0.61369       0.0052576       0.0015075
v  Velocity[Y]            -0.57397         0.54433        0.003081      0.00087333
v  Velocity[Z]              1.5653          5.4397          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4397          4.3406          4.3632
v  Pressure                -36.373          360.01          87.643          169.85
v  r11                   0.0010619        0.081867        0.013075        0.018286
v  r22                   0.0011153        0.082617        0.013355        0.018646
v  r33                   0.0016428         0.17431        0.027254        0.037207
v  r12                   -0.010657        0.013578     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052796      9.3277e-05       0.0010139
v  r23                   -0.046703        0.051173      3.0575e-05      0.00057463
v  epsilon                0.069329          271.29          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9874e-05       0.0099177      0.00092519       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2777         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            10875:        0.73731E+02

===============================================================


 INSTANT    0.108760000E-01   TIME STEP NUMBER           10876
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.549701307E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.193921476E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.147391952E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.129550299E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.753857520E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69748E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81406E-03   0.45135E-02 0.19873E+01 
c  Velocity[X]                                      0.13792E-03 
c  Velocity[Y]                                      0.12791E-03 
c  Velocity[Z]                                      0.42476E-02 
c  Pressure     0.36337E-04     133   0.92555E-02   0.25630E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55070E-08   0.16449E-08 0.99906E-01 
c  r22          0.10852E-01      13   0.57599E-08   0.18419E-08 0.10172E+00 
c  r33          0.21861E-01      15   0.65803E-08   0.12527E-07 0.12728E+00 
c  r12          0.93872E-03      19   0.54295E-08   0.29753E-09 0.60536E+00 
c  r13          0.46677E-02      19   0.60999E-08   0.15050E-08 0.20047E+00 
c  r23          0.39979E-02      20   0.62690E-08   0.12704E-08 0.19852E+00 
c  epsilon      0.10969E+02      11   0.36004E-08   0.99953E-02 0.16770E+00 
c  TempC        0.25716E+06      16   0.15165E-04   0.83820E-02 0.43247E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61365       0.0052575       0.0015075
v  Velocity[Y]            -0.57394         0.54439        0.003081      0.00087332
v  Velocity[Z]              1.5654          5.4397          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4397          4.3406          4.3632
v  Pressure                -36.438          360.07          87.679          169.89
v  r11                   0.0010619        0.081866        0.013075        0.018286
v  r22                   0.0011153        0.082616        0.013355        0.018646
v  r33                   0.0016428         0.17434        0.027254        0.037207
v  r12                   -0.010657        0.013584     -0.00023384     -0.00030932
v  r13                   -0.045529        0.052796      9.3277e-05       0.0010139
v  r23                   -0.046704        0.051167      3.0576e-05      0.00057463
v  epsilon                 0.06933          271.32          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9875e-05       0.0099176      0.00092519       0.0017428
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2779         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            10876:        0.76361E+02

===============================================================


 INSTANT    0.108770000E-01   TIME STEP NUMBER           10877
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.427423009E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.876782261E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.493560878E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.525643196E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.745490143E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81199E-03   0.45348E-02 0.19921E+01 
c  Velocity[X]                                      0.13748E-03 
c  Velocity[Y]                                      0.12846E-03 
c  Velocity[Z]                                      0.42689E-02 
c  Pressure     0.36466E-04     133   0.92768E-02   0.25721E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50871E-08   0.16507E-08 0.99766E-01 
c  r22          0.10852E-01      13   0.49581E-08   0.18318E-08 0.10146E+00 
c  r33          0.21861E-01      15   0.64705E-08   0.12562E-07 0.12759E+00 
c  r12          0.93872E-03      18   0.61211E-08   0.29904E-09 0.60464E+00 
c  r13          0.46677E-02      19   0.66910E-08   0.15168E-08 0.20069E+00 
c  r23          0.39979E-02      20   0.58756E-08   0.12948E-08 0.20003E+00 
c  epsilon      0.10969E+02      11   0.35766E-08   0.10150E-01 0.17094E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83658E-02 0.43202E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63323         0.61373       0.0052575       0.0015075
v  Velocity[Y]            -0.57393         0.54419        0.003081      0.00087332
v  Velocity[Z]               1.565          5.4397          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4397          4.3406          4.3632
v  Pressure                -36.385          359.98          87.626          169.82
v  r11                   0.0010619        0.081859        0.013075        0.018286
v  r22                   0.0011153        0.082612        0.013355        0.018646
v  r33                   0.0016428         0.17431        0.027254        0.037207
v  r12                   -0.010654        0.013583     -0.00023384     -0.00030932
v  r13                   -0.045528        0.052797      9.3277e-05       0.0010139
v  r23                   -0.046703        0.051166      3.0576e-05      0.00057463
v  epsilon                0.069331          271.31          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9876e-05       0.0099176      0.00092519       0.0017428
v  CourantNb               0.44255             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2778         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85284


 TIME FOR THE TIME STEP            10877:        0.74518E+02

===============================================================


 INSTANT    0.108780000E-01   TIME STEP NUMBER           10878
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.198054673E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.673909570E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.811655908E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.458790310E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.229833826E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81293E-03   0.45018E-02 0.19889E+01 
c  Velocity[X]                                      0.13791E-03 
c  Velocity[Y]                                      0.12811E-03 
c  Velocity[Z]                                      0.42358E-02 
c  Pressure     0.35949E-04     133   0.91537E-02   0.25356E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51935E-08   0.16435E-08 0.99169E-01 
c  r22          0.10852E-01      13   0.51543E-08   0.18522E-08 0.10197E+00 
c  r33          0.21861E-01      15   0.62338E-08   0.12605E-07 0.12743E+00 
c  r12          0.93872E-03      18   0.60556E-08   0.29707E-09 0.60348E+00 
c  r13          0.46677E-02      19   0.70614E-08   0.15192E-08 0.20148E+00 
c  r23          0.39979E-02      20   0.60544E-08   0.12834E-08 0.19839E+00 
c  epsilon      0.10969E+02      11   0.32430E-08   0.99921E-02 0.16701E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.84003E-02 0.43230E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63328         0.61372       0.0052575       0.0015075
v  Velocity[Y]            -0.57391         0.54416        0.003081       0.0008733
v  Velocity[Z]              1.5653          5.4397          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4397          4.3406          4.3632
v  Pressure                -36.427          360.01          87.655          169.85
v  r11                   0.0010619        0.081855        0.013075        0.018286
v  r22                   0.0011153        0.082614        0.013355        0.018646
v  r33                   0.0016428         0.17428        0.027254        0.037207
v  r12                   -0.010654        0.013578     -0.00023384     -0.00030932
v  r13                   -0.045526        0.052798      9.3277e-05       0.0010139
v  r23                   -0.046704        0.051203      3.0576e-05      0.00057463
v  epsilon                0.069332          271.26          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9876e-05       0.0099177      0.00092519       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017858          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71352         0.85284


 TIME FOR THE TIME STEP            10878:        0.75438E+02

===============================================================


 INSTANT    0.108790000E-01   TIME STEP NUMBER           10879
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.333195816E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.221595534E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.468669213E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.383455855E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.342495980E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81242E-03   0.44890E-02 0.19871E+01 
c  Velocity[X]                                      0.13714E-03 
c  Velocity[Y]                                      0.12850E-03 
c  Velocity[Z]                                      0.42233E-02 
c  Pressure     0.36646E-04     133   0.93217E-02   0.25847E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50562E-08   0.16033E-08 0.98255E-01 
c  r22          0.10852E-01      13   0.52643E-08   0.18283E-08 0.10125E+00 
c  r33          0.21861E-01      15   0.52032E-08   0.12357E-07 0.12629E+00 
c  r12          0.93872E-03      18   0.60812E-08   0.29590E-09 0.60152E+00 
c  r13          0.46677E-02      19   0.64756E-08   0.15115E-08 0.20056E+00 
c  r23          0.39979E-02      20   0.63508E-08   0.12518E-08 0.19609E+00 
c  epsilon      0.10969E+02      11   0.31784E-08   0.96884E-02 0.16382E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84414E-02 0.43300E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63336         0.61367       0.0052575       0.0015075
v  Velocity[Y]             -0.5739         0.54422       0.0030809      0.00087326
v  Velocity[Z]              1.5652          5.4397          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4397          4.3406          4.3632
v  Pressure                -36.391          360.02          87.633          169.84
v  r11                   0.0010619        0.081858        0.013075        0.018286
v  r22                   0.0011153        0.082615        0.013355        0.018646
v  r33                   0.0016428         0.17429        0.027254        0.037207
v  r12                   -0.010652        0.013572     -0.00023384     -0.00030932
v  r13                   -0.045529        0.052794      9.3277e-05       0.0010139
v  r23                   -0.046704        0.051197      3.0576e-05      0.00057463
v  epsilon                0.069333          271.29          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9878e-05       0.0099178      0.00092519       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017859           5.278         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            10879:        0.73587E+02

===============================================================


 INSTANT    0.108800000E-01   TIME STEP NUMBER           10880
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.324413982E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.360051895E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.134067695E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.214582232E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.209266438E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81329E-03   0.45109E-02 0.19900E+01 
c  Velocity[X]                                      0.13849E-03 
c  Velocity[Y]                                      0.12842E-03 
c  Velocity[Z]                                      0.42440E-02 
c  Pressure     0.36271E-04     132   0.92393E-02   0.25583E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54966E-08   0.16064E-08 0.98377E-01 
c  r22          0.10852E-01      13   0.52124E-08   0.18390E-08 0.10151E+00 
c  r33          0.21861E-01      15   0.54384E-08   0.12430E-07 0.12671E+00 
c  r12          0.93872E-03      18   0.63845E-08   0.29375E-09 0.60209E+00 
c  r13          0.46677E-02      19   0.59260E-08   0.15052E-08 0.20037E+00 
c  r23          0.39979E-02      19   0.71944E-08   0.12486E-08 0.19643E+00 
c  epsilon      0.10969E+02      11   0.33895E-08   0.97204E-02 0.16455E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83838E-02 0.43215E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63332         0.61372       0.0052574       0.0015075
v  Velocity[Y]            -0.57362         0.54428       0.0030808      0.00087324
v  Velocity[Z]              1.5652          5.4397          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4397          4.3406          4.3632
v  Pressure                -36.415          359.98          87.631          169.82
v  r11                   0.0010619        0.081867        0.013075        0.018286
v  r22                   0.0011153        0.082615        0.013355        0.018646
v  r33                   0.0016428         0.17432        0.027254        0.037207
v  r12                   -0.010663        0.013577     -0.00023384     -0.00030932
v  r13                   -0.045526        0.052793      9.3278e-05       0.0010139
v  r23                   -0.046704        0.051186      3.0577e-05      0.00057463
v  epsilon                0.069334           271.3          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9878e-05       0.0099177      0.00092519       0.0017428
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017859           5.278         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            10880:        0.74332E+02

===============================================================


 INSTANT    0.108810000E-01   TIME STEP NUMBER           10881
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.186515670E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.766180119E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.139865735E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.306801670E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138678863E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81281E-03   0.44946E-02 0.19843E+01 
c  Velocity[X]                                      0.13736E-03 
c  Velocity[Y]                                      0.12751E-03 
c  Velocity[Z]                                      0.42298E-02 
c  Pressure     0.35830E-04     133   0.91205E-02   0.25272E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57525E-08   0.16172E-08 0.98727E-01 
c  r22          0.10852E-01      13   0.52790E-08   0.18320E-08 0.10119E+00 
c  r33          0.21861E-01      15   0.57315E-08   0.12462E-07 0.12670E+00 
c  r12          0.93872E-03      18   0.63265E-08   0.29261E-09 0.59953E+00 
c  r13          0.46677E-02      19   0.69027E-08   0.14976E-08 0.19994E+00 
c  r23          0.39979E-02      19   0.68792E-08   0.12535E-08 0.19699E+00 
c  epsilon      0.10969E+02      11   0.33910E-08   0.97108E-02 0.16258E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.83739E-02 0.43236E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63336         0.61371       0.0052574       0.0015075
v  Velocity[Y]             -0.5736         0.54436       0.0030809      0.00087327
v  Velocity[Z]              1.5654          5.4397          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4397          4.3406          4.3632
v  Pressure                -36.416          360.03           87.67          169.87
v  r11                   0.0010619        0.081877        0.013075        0.018286
v  r22                   0.0011153        0.082616        0.013355        0.018646
v  r33                   0.0016428         0.17435        0.027254        0.037207
v  r12                   -0.010662        0.013578     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052793      9.3279e-05       0.0010139
v  r23                   -0.046704        0.051208      3.0577e-05      0.00057463
v  epsilon                0.069335          271.31          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9881e-05       0.0099178      0.00092519       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017859          5.2785         0.11443         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            10881:        0.72645E+02

===============================================================


 INSTANT    0.108820000E-01   TIME STEP NUMBER           10882
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.965870610E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.340458921E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.465566225E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.165471180E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.974091769E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69750E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81335E-03   0.45245E-02 0.19927E+01 
c  Velocity[X]                                      0.13774E-03 
c  Velocity[Y]                                      0.12839E-03 
c  Velocity[Z]                                      0.42583E-02 
c  Pressure     0.36925E-04     133   0.94058E-02   0.26043E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55529E-08   0.16188E-08 0.98767E-01 
c  r22          0.10852E-01      13   0.51935E-08   0.18556E-08 0.10205E+00 
c  r33          0.21861E-01      15   0.56049E-08   0.12592E-07 0.12767E+00 
c  r12          0.93872E-03      18   0.54622E-08   0.29426E-09 0.60107E+00 
c  r13          0.46677E-02      19   0.58909E-08   0.15000E-08 0.20036E+00 
c  r23          0.39979E-02      19   0.64710E-08   0.12696E-08 0.19866E+00 
c  epsilon      0.10969E+02      11   0.34051E-08   0.98588E-02 0.16479E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83884E-02 0.43171E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61367       0.0052574       0.0015074
v  Velocity[Y]            -0.57364         0.54413       0.0030808      0.00087321
v  Velocity[Z]              1.5653          5.4397          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4397          4.3406          4.3632
v  Pressure                -36.447          360.08          87.689           169.9
v  r11                   0.0010619        0.081876        0.013075        0.018286
v  r22                   0.0011153        0.082616        0.013355        0.018646
v  r33                   0.0016428         0.17433        0.027254        0.037207
v  r12                   -0.010661        0.013586     -0.00023384     -0.00030932
v  r13                   -0.045529        0.052792      9.3279e-05       0.0010139
v  r23                   -0.046704        0.051201      3.0576e-05      0.00057463
v  epsilon                0.069336          271.32          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9881e-05       0.0099177      0.00092519       0.0017428
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017859          5.2782         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            10882:        0.73251E+02

===============================================================


 INSTANT    0.108830000E-01   TIME STEP NUMBER           10883
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.217155507E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.976197865E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.228780892E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.295102122E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.306103318E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81296E-03   0.45155E-02 0.19917E+01 
c  Velocity[X]                                      0.13817E-03 
c  Velocity[Y]                                      0.12788E-03 
c  Velocity[Z]                                      0.42495E-02 
c  Pressure     0.36145E-04     133   0.92015E-02   0.25494E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58619E-08   0.16633E-08 0.10002E+00 
c  r22          0.10852E-01      13   0.50539E-08   0.18292E-08 0.10122E+00 
c  r33          0.21861E-01      15   0.72528E-08   0.12737E-07 0.12804E+00 
c  r12          0.93872E-03      18   0.57811E-08   0.30294E-09 0.60907E+00 
c  r13          0.46677E-02      19   0.64646E-08   0.15176E-08 0.20041E+00 
c  r23          0.39979E-02      19   0.69240E-08   0.13123E-08 0.20101E+00 
c  epsilon      0.10969E+02      11   0.34188E-08   0.10479E-01 0.17361E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84316E-02 0.43288E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61371       0.0052574       0.0015074
v  Velocity[Y]            -0.57364         0.54421       0.0030809      0.00087325
v  Velocity[Z]              1.5653          5.4397          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4397          4.3406          4.3632
v  Pressure                -36.394          360.07          87.682          169.89
v  r11                   0.0010619        0.081873        0.013075        0.018286
v  r22                   0.0011153        0.082615        0.013355        0.018646
v  r33                   0.0016428          0.1743        0.027254        0.037207
v  r12                   -0.010657        0.013596     -0.00023384     -0.00030932
v  r13                   -0.045526        0.052792       9.328e-05       0.0010139
v  r23                   -0.046704        0.051191      3.0576e-05      0.00057463
v  epsilon                0.069337          271.27          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9883e-05       0.0099177      0.00092519       0.0017428
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017859          5.2781         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            10883:        0.77665E+02

===============================================================


 INSTANT    0.108840000E-01   TIME STEP NUMBER           10884
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.128074376E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.277019430E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.975282629E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935018E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166206235E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.217455249E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69751E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81271E-03   0.44965E-02 0.19861E+01 
c  Velocity[X]                                      0.13790E-03 
c  Velocity[Y]                                      0.12861E-03 
c  Velocity[Z]                                      0.42300E-02 
c  Pressure     0.36028E-04     133   0.91703E-02   0.25412E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57666E-08   0.16242E-08 0.98871E-01 
c  r22          0.10852E-01      13   0.54707E-08   0.18368E-08 0.10099E+00 
c  r33          0.21861E-01      16   0.65078E-08   0.12605E-07 0.12706E+00 
c  r12          0.93872E-03      18   0.58212E-08   0.30291E-09 0.60635E+00 
c  r13          0.46677E-02      20   0.58750E-08   0.15224E-08 0.20062E+00 
c  r23          0.39979E-02      20   0.56704E-08   0.12962E-08 0.19890E+00 
c  epsilon      0.10969E+02      11   0.33888E-08   0.10178E-01 0.16712E+00 
c  TempC        0.25716E+06      16   0.15201E-04   0.84133E-02 0.43276E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161987


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61368       0.0052574       0.0015074
v  Velocity[Y]            -0.57362         0.54437       0.0030809      0.00087327
v  Velocity[Z]              1.5651          5.4397          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4397          4.3406          4.3632
v  Pressure                -36.419          360.02           87.64          169.84
v  r11                    0.001062        0.081873        0.013075        0.018286
v  r22                   0.0011153         0.08261        0.013355        0.018646
v  r33                   0.0016428         0.17431        0.027254        0.037207
v  r12                   -0.010657        0.013594     -0.00023384     -0.00030932
v  r13                   -0.045525        0.052792       9.328e-05       0.0010139
v  r23                   -0.046704        0.051216      3.0576e-05      0.00057463
v  epsilon                0.069338          271.28          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9884e-05       0.0099177      0.00092519       0.0017428
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017859          5.2786         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            10884:        0.74023E+02

===============================================================


 INSTANT    0.108850000E-01   TIME STEP NUMBER           10885
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.262982130E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69752E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.491952049E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69752E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.694288029E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69752E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.510700467E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69752E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.441944844E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69752E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81267E-03   0.45252E-02 0.19895E+01 
c  Velocity[X]                                      0.13725E-03 
c  Velocity[Y]                                      0.12807E-03 
c  Velocity[Z]                                      0.42598E-02 
c  Pressure     0.36248E-04     132   0.92295E-02   0.25567E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54982E-08   0.16194E-08 0.99201E-01 
c  r22          0.10852E-01      13   0.54854E-08   0.18270E-08 0.10130E+00 
c  r33          0.21861E-01      15   0.68831E-08   0.12442E-07 0.12689E+00 
c  r12          0.93872E-03      18   0.54757E-08   0.29219E-09 0.60277E+00 
c  r13          0.46677E-02      19   0.71625E-08   0.14927E-08 0.19967E+00 
c  r23          0.39979E-02      20   0.58388E-08   0.12633E-08 0.19774E+00 
c  epsilon      0.10969E+02      11   0.33447E-08   0.96627E-02 0.16409E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.83535E-02 0.43141E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63329         0.61366       0.0052574       0.0015074
v  Velocity[Y]            -0.57359         0.54421       0.0030809      0.00087329
v  Velocity[Z]              1.5653          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4398          4.3406          4.3632
v  Pressure                -36.399          360.02          87.639          169.85
v  r11                    0.001062        0.081874        0.013075        0.018286
v  r22                   0.0011153         0.08261        0.013355        0.018646
v  r33                   0.0016429         0.17434        0.027254        0.037207
v  r12                   -0.010665        0.013597     -0.00023384     -0.00030932
v  r13                   -0.045529        0.052792       9.328e-05       0.0010139
v  r23                   -0.046705        0.051201      3.0576e-05      0.00057463
v  epsilon                0.069338          271.32          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9886e-05       0.0099176      0.00092519       0.0017428
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017859          5.2787         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85284


 TIME FOR THE TIME STEP            10885:        0.72677E+02

===============================================================


 INSTANT    0.108860000E-01   TIME STEP NUMBER           10886
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.261445124E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171018664E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.633293806E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.341134961E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.123638192E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69754E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81268E-03   0.45167E-02 0.19897E+01 
c  Velocity[X]                                      0.13790E-03 
c  Velocity[Y]                                      0.12797E-03 
c  Velocity[Z]                                      0.42509E-02 
c  Pressure     0.36489E-04     131   0.92916E-02   0.25737E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55985E-08   0.16288E-08 0.99380E-01 
c  r22          0.10852E-01      13   0.53150E-08   0.18095E-08 0.10130E+00 
c  r33          0.21861E-01      15   0.72843E-08   0.12401E-07 0.12722E+00 
c  r12          0.93872E-03      18   0.49733E-08   0.29853E-09 0.60638E+00 
c  r13          0.46677E-02      20   0.63553E-08   0.14782E-08 0.19989E+00 
c  r23          0.39979E-02      20   0.71254E-08   0.12661E-08 0.19848E+00 
c  epsilon      0.10969E+02      11   0.34516E-08   0.96658E-02 0.16314E+00 
c  TempC        0.25716E+06      16   0.15178E-04   0.84227E-02 0.43317E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63333          0.6137       0.0052575       0.0015075
v  Velocity[Y]             -0.5736         0.54415       0.0030808      0.00087323
v  Velocity[Z]              1.5656          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4398          4.3406          4.3632
v  Pressure                -36.412          360.01          87.645          169.84
v  r11                    0.001062        0.081871        0.013075        0.018286
v  r22                   0.0011153        0.082611        0.013355        0.018646
v  r33                   0.0016429         0.17431        0.027254        0.037207
v  r12                   -0.010669        0.013601     -0.00023384     -0.00030932
v  r13                   -0.045526        0.052794       9.328e-05       0.0010139
v  r23                   -0.046705        0.051193      3.0576e-05      0.00057463
v  epsilon                0.069339          271.31          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9887e-05       0.0099177      0.00092519       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017859          5.2789         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            10886:        0.71102E+02

===============================================================


 INSTANT    0.108870000E-01   TIME STEP NUMBER           10887
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.623184439E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107185565E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.635184840E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.854505872E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.433373538E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69755E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81260E-03   0.44970E-02 0.19876E+01 
c  Velocity[X]                                      0.13840E-03 
c  Velocity[Y]                                      0.12784E-03 
c  Velocity[Z]                                      0.42307E-02 
c  Pressure     0.36098E-04     134   0.91911E-02   0.25461E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55323E-08   0.16104E-08 0.98175E-01 
c  r22          0.10852E-01      13   0.59393E-08   0.18118E-08 0.10052E+00 
c  r33          0.21861E-01      15   0.71595E-08   0.12313E-07 0.12577E+00 
c  r12          0.93872E-03      18   0.55869E-08   0.28966E-09 0.59627E+00 
c  r13          0.46677E-02      20   0.66706E-08   0.14674E-08 0.19798E+00 
c  r23          0.39979E-02      20   0.72400E-08   0.12589E-08 0.19651E+00 
c  epsilon      0.10969E+02      11   0.34676E-08   0.96602E-02 0.16220E+00 
c  TempC        0.25716E+06      16   0.15117E-04   0.84433E-02 0.43342E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63333         0.61369       0.0052575       0.0015075
v  Velocity[Y]            -0.57379         0.54423       0.0030809      0.00087325
v  Velocity[Z]              1.5653          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4398          4.3406          4.3632
v  Pressure                -36.365          360.11          87.702          169.92
v  r11                    0.001062        0.081883        0.013075        0.018286
v  r22                   0.0011153        0.082612        0.013355        0.018646
v  r33                   0.0016429         0.17428        0.027254        0.037207
v  r12                    -0.01067        0.013604     -0.00023384     -0.00030932
v  r13                   -0.045525        0.052791      9.3281e-05       0.0010139
v  r23                   -0.046706        0.051223      3.0576e-05      0.00057463
v  epsilon                 0.06934          271.25          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9888e-05       0.0099178       0.0009252       0.0017428
v  CourantNb               0.44259             0.6         0.59908         0.59839
v  FourierNb             0.0017859          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            10887:        0.73969E+02

===============================================================


 INSTANT    0.108880000E-01   TIME STEP NUMBER           10888
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.101947431E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.140369686E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.315213661E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162736887E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.296762449E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81306E-03   0.44619E-02 0.19789E+01 
c  Velocity[X]                                      0.13723E-03 
c  Velocity[Y]                                      0.12729E-03 
c  Velocity[Z]                                      0.41974E-02 
c  Pressure     0.35939E-04     132   0.91517E-02   0.25349E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57645E-08   0.16232E-08 0.98463E-01 
c  r22          0.10852E-01      13   0.59675E-08   0.18379E-08 0.10074E+00 
c  r33          0.21861E-01      15   0.63402E-08   0.12506E-07 0.12605E+00 
c  r12          0.93872E-03      18   0.52313E-08   0.29820E-09 0.60019E+00 
c  r13          0.46677E-02      19   0.75230E-08   0.15164E-08 0.19929E+00 
c  r23          0.39979E-02      20   0.67179E-08   0.12741E-08 0.19748E+00 
c  epsilon      0.10969E+02      11   0.33090E-08   0.10039E-01 0.16560E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.83589E-02 0.43152E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63336         0.61365       0.0052574       0.0015075
v  Velocity[Y]            -0.57365         0.54432       0.0030809      0.00087324
v  Velocity[Z]              1.5655          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4398          4.3406          4.3632
v  Pressure                -36.467          360.02          87.658          169.85
v  r11                    0.001062        0.081884        0.013075        0.018286
v  r22                   0.0011153        0.082612        0.013355        0.018646
v  r33                   0.0016429         0.17429        0.027254        0.037207
v  r12                   -0.010667        0.013602     -0.00023384     -0.00030932
v  r13                   -0.045527         0.05279      9.3281e-05       0.0010138
v  r23                   -0.046708        0.051212      3.0576e-05      0.00057462
v  epsilon                0.069341          271.27          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9889e-05       0.0099178       0.0009252       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017859          5.2773         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            10888:        0.72999E+02

===============================================================


 INSTANT    0.108890000E-01   TIME STEP NUMBER           10889
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.228979585E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.487575371E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.298793892E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127016813E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.177818326E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81197E-03   0.45221E-02 0.19903E+01 
c  Velocity[X]                                      0.13766E-03 
c  Velocity[Y]                                      0.12876E-03 
c  Velocity[Z]                                      0.42557E-02 
c  Pressure     0.36646E-04     132   0.93264E-02   0.25848E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54984E-08   0.16175E-08 0.98350E-01 
c  r22          0.10852E-01      13   0.57142E-08   0.17971E-08 0.10048E+00 
c  r33          0.21861E-01      15   0.59356E-08   0.12350E-07 0.12578E+00 
c  r12          0.93872E-03      18   0.51779E-08   0.29119E-09 0.59912E+00 
c  r13          0.46677E-02      19   0.68144E-08   0.14943E-08 0.19922E+00 
c  r23          0.39979E-02      20   0.62094E-08   0.12757E-08 0.19742E+00 
c  epsilon      0.10969E+02      11   0.32219E-08   0.97804E-02 0.16334E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84108E-02 0.43291E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61369       0.0052574       0.0015074
v  Velocity[Y]            -0.57366         0.54438       0.0030807      0.00087319
v  Velocity[Z]              1.5655          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4398          4.3406          4.3632
v  Pressure                -36.383             360          87.624          169.83
v  r11                    0.001062        0.081893        0.013075        0.018286
v  r22                   0.0011153        0.082611        0.013355        0.018646
v  r33                   0.0016429         0.17432        0.027254        0.037207
v  r12                   -0.010666        0.013602     -0.00023384     -0.00030932
v  r13                   -0.045526         0.05279      9.3281e-05       0.0010138
v  r23                   -0.046709        0.051196      3.0576e-05      0.00057462
v  epsilon                0.069342          271.29          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9894e-05       0.0099179       0.0009252       0.0017428
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017859          5.2768         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71352         0.85284


 TIME FOR THE TIME STEP            10889:        0.72981E+02

===============================================================


 INSTANT    0.108900000E-01   TIME STEP NUMBER           10890
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.228177944E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.763032804E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.423874237E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.674219078E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178112237E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81322E-03   0.45098E-02 0.19883E+01 
c  Velocity[X]                                      0.13813E-03 
c  Velocity[Y]                                      0.12860E-03 
c  Velocity[Z]                                      0.42430E-02 
c  Pressure     0.36636E-04     133   0.93247E-02   0.25840E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54354E-08   0.16513E-08 0.99618E-01 
c  r22          0.10852E-01      13   0.54084E-08   0.18334E-08 0.10104E+00 
c  r33          0.21861E-01      15   0.52399E-08   0.12604E-07 0.12738E+00 
c  r12          0.93872E-03      18   0.56270E-08   0.29675E-09 0.60550E+00 
c  r13          0.46677E-02      19   0.61252E-08   0.14885E-08 0.19941E+00 
c  r23          0.39979E-02      20   0.54967E-08   0.12792E-08 0.19991E+00 
c  epsilon      0.10969E+02      11   0.33295E-08   0.10316E-01 0.17199E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.84582E-02 0.43393E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61366       0.0052574       0.0015074
v  Velocity[Y]            -0.57348         0.54419       0.0030807      0.00087319
v  Velocity[Z]              1.5653          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4398          4.3406          4.3632
v  Pressure                 -36.44          360.03          87.669          169.86
v  r11                    0.001062        0.081895        0.013075        0.018286
v  r22                   0.0011153        0.082612        0.013355        0.018646
v  r33                   0.0016429         0.17435        0.027254        0.037207
v  r12                   -0.010664        0.013604     -0.00023384     -0.00030932
v  r13                   -0.045525        0.052791      9.3281e-05       0.0010138
v  r23                   -0.046709        0.051211      3.0575e-05      0.00057462
v  epsilon                0.069343           271.3          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9896e-05       0.0099178       0.0009252       0.0017428
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb              0.001786          5.2776         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            10890:        0.73003E+02

===============================================================


 INSTANT    0.108910000E-01   TIME STEP NUMBER           10891
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.113199264E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.382389953E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.194657642E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.909715991E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.988671377E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81306E-03   0.44890E-02 0.19844E+01 
c  Velocity[X]                                      0.13722E-03 
c  Velocity[Y]                                      0.12748E-03 
c  Velocity[Z]                                      0.42243E-02 
c  Pressure     0.36299E-04     133   0.92405E-02   0.25603E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58118E-08   0.16282E-08 0.99013E-01 
c  r22          0.10852E-01      13   0.55491E-08   0.18223E-08 0.10084E+00 
c  r33          0.21861E-01      15   0.53267E-08   0.12505E-07 0.12678E+00 
c  r12          0.93872E-03      18   0.56130E-08   0.29427E-09 0.60067E+00 
c  r13          0.46677E-02      19   0.67665E-08   0.15095E-08 0.19971E+00 
c  r23          0.39979E-02      19   0.70060E-08   0.12766E-08 0.19846E+00 
c  epsilon      0.10969E+02      11   0.34328E-08   0.10073E-01 0.16802E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84145E-02 0.43249E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162017


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61364       0.0052575       0.0015075
v  Velocity[Y]            -0.57356         0.54425       0.0030808       0.0008732
v  Velocity[Z]              1.5653          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4398          4.3406          4.3632
v  Pressure                -36.416          360.02          87.636          169.85
v  r11                    0.001062        0.081907        0.013075        0.018286
v  r22                   0.0011154        0.082607        0.013355        0.018646
v  r33                   0.0016429         0.17433        0.027254        0.037207
v  r12                   -0.010662        0.013606     -0.00023384     -0.00030932
v  r13                   -0.045527         0.05279      9.3282e-05       0.0010138
v  r23                    -0.04671        0.051199      3.0575e-05      0.00057462
v  epsilon                0.069344          271.31          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc               5.99e-05       0.0099177       0.0009252       0.0017428
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb              0.001786          5.2782         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            10891:        0.68559E+02

===============================================================


 INSTANT    0.108920000E-01   TIME STEP NUMBER           10892
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.104153738E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106259811E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.268885414E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168190095E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.583575108E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      45   0.81291E-03   0.45051E-02 0.19889E+01 
c  Velocity[X]                                      0.13743E-03 
c  Velocity[Y]                                      0.12826E-03 
c  Velocity[Z]                                      0.42394E-02 
c  Pressure     0.36446E-04     133   0.92826E-02   0.25707E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60627E-08   0.16276E-08 0.98587E-01 
c  r22          0.10852E-01      13   0.54145E-08   0.17926E-08 0.10058E+00 
c  r33          0.21861E-01      15   0.52977E-08   0.12340E-07 0.12624E+00 
c  r12          0.93872E-03      18   0.56758E-08   0.30162E-09 0.60471E+00 
c  r13          0.46677E-02      19   0.62124E-08   0.14558E-08 0.19805E+00 
c  r23          0.39979E-02      20   0.53858E-08   0.12908E-08 0.19904E+00 
c  epsilon      0.10969E+02      11   0.33878E-08   0.99220E-02 0.16700E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.83895E-02 0.43223E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162022


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61366       0.0052575       0.0015075
v  Velocity[Y]            -0.57357         0.54441       0.0030807      0.00087315
v  Velocity[Z]              1.5652          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4398          4.3406          4.3632
v  Pressure                -36.418          360.01          87.672          169.86
v  r11                    0.001062        0.081908        0.013075        0.018286
v  r22                   0.0011154        0.082607        0.013355        0.018646
v  r33                   0.0016429          0.1743        0.027254        0.037207
v  r12                   -0.010664        0.013597     -0.00023384     -0.00030932
v  r13                   -0.045525        0.052791      9.3282e-05       0.0010138
v  r23                    -0.04671        0.051185      3.0575e-05      0.00057462
v  epsilon                0.069345          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9904e-05       0.0099177       0.0009252       0.0017428
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb              0.001786          5.2785         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            10892:        0.71487E+02

===============================================================


 INSTANT    0.108930000E-01   TIME STEP NUMBER           10893
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.877730044E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.303409174E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.324531028E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285536345E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.990069153E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81141E-03   0.45383E-02 0.19952E+01 
c  Velocity[X]                                      0.13863E-03 
c  Velocity[Y]                                      0.12885E-03 
c  Velocity[Z]                                      0.42708E-02 
c  Pressure     0.36213E-04     133   0.92220E-02   0.25543E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.59480E-08   0.16341E-08 0.99467E-01 
c  r22          0.10852E-01      13   0.50789E-08   0.18369E-08 0.10127E+00 
c  r33          0.21861E-01      14   0.69092E-08   0.12511E-07 0.12732E+00 
c  r12          0.93872E-03      18   0.50575E-08   0.29759E-09 0.60412E+00 
c  r13          0.46677E-02      19   0.61778E-08   0.14833E-08 0.19922E+00 
c  r23          0.39979E-02      19   0.69361E-08   0.12625E-08 0.19846E+00 
c  epsilon      0.10969E+02      11   0.33434E-08   0.99566E-02 0.16555E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.84030E-02 0.43255E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61367       0.0052575       0.0015075
v  Velocity[Y]            -0.57362         0.54407       0.0030807      0.00087316
v  Velocity[Z]              1.5656          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4398          4.3406          4.3632
v  Pressure                -36.388          360.08          87.681           169.9
v  r11                    0.001062        0.081908        0.013075        0.018286
v  r22                   0.0011154        0.082609        0.013355        0.018646
v  r33                   0.0016429         0.17431        0.027254        0.037207
v  r12                   -0.010661        0.013598     -0.00023384     -0.00030932
v  r13                   -0.045526         0.05279      9.3283e-05       0.0010138
v  r23                   -0.046711        0.051188      3.0576e-05      0.00057462
v  epsilon                0.069346          271.25          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9908e-05       0.0099177       0.0009252       0.0017428
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb              0.001786           5.279         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71352         0.85284


 TIME FOR THE TIME STEP            10893:        0.70332E+02

===============================================================


 INSTANT    0.108940000E-01   TIME STEP NUMBER           10894
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.252052442E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107972243E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.367999427E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935011E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.906255729E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.244877498E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81327E-03   0.45152E-02 0.19884E+01 
c  Velocity[X]                                      0.13701E-03 
c  Velocity[Y]                                      0.12768E-03 
c  Velocity[Z]                                      0.42505E-02 
c  Pressure     0.36132E-04     132   0.91988E-02   0.25485E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57457E-08   0.17172E-08 0.10127E+00 
c  r22          0.10852E-01      13   0.52995E-08   0.18247E-08 0.10104E+00 
c  r33          0.21861E-01      14   0.67075E-08   0.12822E-07 0.12849E+00 
c  r12          0.93872E-03      17   0.69698E-08   0.30356E-09 0.61024E+00 
c  r13          0.46677E-02      19   0.58822E-08   0.15019E-08 0.19996E+00 
c  r23          0.39979E-02      19   0.67814E-08   0.13280E-08 0.20255E+00 
c  epsilon      0.10969E+02      11   0.32358E-08   0.10047E-01 0.16612E+00 
c  TempC        0.25716E+06      16   0.15167E-04   0.83878E-02 0.43202E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61365       0.0052575       0.0015075
v  Velocity[Y]            -0.57365         0.54408       0.0030807      0.00087316
v  Velocity[Z]              1.5654          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4398          4.3406          4.3632
v  Pressure                -36.438          360.03          87.646          169.85
v  r11                    0.001062        0.081925        0.013075        0.018286
v  r22                   0.0011154        0.082609        0.013355        0.018646
v  r33                   0.0016429         0.17433        0.027254        0.037207
v  r12                   -0.010662        0.013601     -0.00023384     -0.00030932
v  r13                   -0.045528         0.05279      9.3283e-05       0.0010138
v  r23                   -0.046712        0.051218      3.0577e-05      0.00057462
v  epsilon                0.069347          271.28          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9912e-05       0.0099177       0.0009252       0.0017428
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb              0.001786          5.2789         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            10894:        0.69862E+02

===============================================================


 INSTANT    0.108950000E-01   TIME STEP NUMBER           10895
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.146348332E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119259415E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205047358E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.260167542E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.175562902E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81192E-03   0.45054E-02 0.19891E+01 
c  Velocity[X]                                      0.13793E-03 
c  Velocity[Y]                                      0.12838E-03 
c  Velocity[Z]                                      0.42391E-02 
c  Pressure     0.36244E-04     132   0.92244E-02   0.25564E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52861E-08   0.16906E-08 0.10076E+00 
c  r22          0.10852E-01      13   0.52645E-08   0.18410E-08 0.10142E+00 
c  r33          0.21861E-01      14   0.68203E-08   0.12687E-07 0.12781E+00 
c  r12          0.93872E-03      18   0.50285E-08   0.30141E-09 0.61044E+00 
c  r13          0.46677E-02      19   0.58976E-08   0.14905E-08 0.19939E+00 
c  r23          0.39979E-02      19   0.65265E-08   0.13025E-08 0.20010E+00 
c  epsilon      0.10969E+02      11   0.31582E-08   0.10040E-01 0.16539E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.84318E-02 0.43294E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61367       0.0052575       0.0015074
v  Velocity[Y]            -0.57372         0.54423       0.0030807      0.00087313
v  Velocity[Z]              1.5654          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4398          4.3406          4.3632
v  Pressure                -36.378          360.03          87.651          169.86
v  r11                    0.001062        0.081934        0.013075        0.018286
v  r22                   0.0011154        0.082609        0.013355        0.018646
v  r33                   0.0016429          0.1743        0.027254        0.037207
v  r12                   -0.010665        0.013597     -0.00023384     -0.00030932
v  r13                   -0.045525        0.052791      9.3283e-05       0.0010138
v  r23                   -0.046712         0.05121      3.0576e-05      0.00057462
v  epsilon                0.069348          271.29          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099177       0.0009252       0.0017428
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb              0.001786          5.2787         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85283


 TIME FOR THE TIME STEP            10895:        0.71727E+02

===============================================================


 INSTANT    0.108960000E-01   TIME STEP NUMBER           10896
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.572542965E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.168017407E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.605045839E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199227884E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181252627E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81397E-03   0.45045E-02 0.19873E+01 
c  Velocity[X]                                      0.13825E-03 
c  Velocity[Y]                                      0.12862E-03 
c  Velocity[Z]                                      0.42376E-02 
c  Pressure     0.36412E-04     136   0.92723E-02   0.25683E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53934E-08   0.16385E-08 0.99916E-01 
c  r22          0.10852E-01      13   0.52742E-08   0.18155E-08 0.10121E+00 
c  r33          0.21861E-01      15   0.52602E-08   0.12510E-07 0.12780E+00 
c  r12          0.93872E-03      18   0.51969E-08   0.29318E-09 0.60350E+00 
c  r13          0.46677E-02      19   0.61739E-08   0.14948E-08 0.20071E+00 
c  r23          0.39979E-02      19   0.64392E-08   0.12705E-08 0.19944E+00 
c  epsilon      0.10969E+02      11   0.32439E-08   0.10216E-01 0.17167E+00 
c  TempC        0.25716E+06      16   0.15174E-04   0.84006E-02 0.43282E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61365       0.0052574       0.0015074
v  Velocity[Y]            -0.57362         0.54441       0.0030806      0.00087311
v  Velocity[Z]              1.5654          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4398          4.3406          4.3632
v  Pressure                -36.417          360.03          87.675          169.87
v  r11                    0.001062        0.081949        0.013075        0.018286
v  r22                   0.0011154         0.08261        0.013355        0.018646
v  r33                   0.0016429         0.17427        0.027254        0.037207
v  r12                   -0.010664        0.013597     -0.00023384     -0.00030932
v  r13                   -0.045523        0.052789      9.3284e-05       0.0010138
v  r23                   -0.046711          0.0512      3.0577e-05      0.00057462
v  epsilon                0.069349          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099177       0.0009252       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb              0.001786          5.2779         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85283


 TIME FOR THE TIME STEP            10896:        0.72140E+02

===============================================================


 INSTANT    0.108970000E-01   TIME STEP NUMBER           10897
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107274666E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.569043011E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203233193E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.832194744E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.158145553E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81254E-03   0.44996E-02 0.19856E+01 
c  Velocity[X]                                      0.13738E-03 
c  Velocity[Y]                                      0.12805E-03 
c  Velocity[Z]                                      0.42342E-02 
c  Pressure     0.36023E-04     133   0.91723E-02   0.25409E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50598E-08   0.16186E-08 0.98888E-01 
c  r22          0.10852E-01      13   0.55011E-08   0.18004E-08 0.10061E+00 
c  r33          0.21861E-01      14   0.71271E-08   0.12344E-07 0.12654E+00 
c  r12          0.93872E-03      18   0.56826E-08   0.29179E-09 0.60123E+00 
c  r13          0.46677E-02      19   0.55354E-08   0.14785E-08 0.19865E+00 
c  r23          0.39979E-02      19   0.63377E-08   0.12773E-08 0.19866E+00 
c  epsilon      0.10969E+02      11   0.32387E-08   0.97597E-02 0.16509E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.83777E-02 0.43199E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161988


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63354         0.61363       0.0052575       0.0015074
v  Velocity[Y]            -0.57366         0.54406       0.0030807      0.00087315
v  Velocity[Z]              1.5655          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4398          4.3406          4.3632
v  Pressure                -36.386          360.05          87.665          169.88
v  r11                    0.001062        0.081954        0.013075        0.018286
v  r22                   0.0011154        0.082605        0.013355        0.018646
v  r33                   0.0016429         0.17427        0.027254        0.037207
v  r12                   -0.010661        0.013599     -0.00023384     -0.00030932
v  r13                   -0.045527         0.05279      9.3284e-05       0.0010138
v  r23                   -0.046711        0.051196      3.0577e-05      0.00057462
v  epsilon                 0.06935          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099177       0.0009252       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb              0.001786           5.278         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            10897:        0.71189E+02

===============================================================


 INSTANT    0.108980000E-01   TIME STEP NUMBER           10898
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.604497680E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.952378078E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.131353949E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232162176E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.312712485E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81262E-03   0.45125E-02 0.19906E+01 
c  Velocity[X]                                      0.13833E-03 
c  Velocity[Y]                                      0.12832E-03 
c  Velocity[Z]                                      0.42459E-02 
c  Pressure     0.36287E-04     132   0.92415E-02   0.25593E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49074E-08   0.16639E-08 0.99704E-01 
c  r22          0.10852E-01      13   0.54332E-08   0.17944E-08 0.10066E+00 
c  r33          0.21861E-01      15   0.55112E-08   0.12505E-07 0.12693E+00 
c  r12          0.93872E-03      18   0.56619E-08   0.29398E-09 0.60212E+00 
c  r13          0.46677E-02      18   0.61288E-08   0.14527E-08 0.19807E+00 
c  r23          0.39979E-02      19   0.62821E-08   0.12953E-08 0.19923E+00 
c  epsilon      0.10969E+02      11   0.33366E-08   0.99586E-02 0.16552E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.83989E-02 0.43207E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63363         0.61365       0.0052574       0.0015074
v  Velocity[Y]             -0.5735         0.54409       0.0030806      0.00087312
v  Velocity[Z]              1.5654          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4398          4.3406          4.3632
v  Pressure                -36.421          359.94          87.617          169.79
v  r11                    0.001062        0.081954        0.013075        0.018286
v  r22                   0.0011154        0.082607        0.013355        0.018646
v  r33                   0.0016429         0.17428        0.027254        0.037207
v  r12                   -0.010668        0.013602     -0.00023384     -0.00030932
v  r13                   -0.045525        0.052792      9.3285e-05       0.0010138
v  r23                    -0.04671        0.051228      3.0577e-05      0.00057462
v  epsilon                0.069351          271.27          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099178       0.0009252       0.0017428
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb              0.001786          5.2783         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71352         0.85284


 TIME FOR THE TIME STEP            10898:        0.20685E+03

===============================================================


 INSTANT    0.108990000E-01   TIME STEP NUMBER           10899
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.303571956E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130770507E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.345486078E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.163122811E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.339165143E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81245E-03   0.45107E-02 0.19890E+01 
c  Velocity[X]                                      0.13749E-03 
c  Velocity[Y]                                      0.12834E-03 
c  Velocity[Z]                                      0.42449E-02 
c  Pressure     0.36260E-04     133   0.92283E-02   0.25576E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49777E-08   0.16286E-08 0.99154E-01 
c  r22          0.10852E-01      13   0.56313E-08   0.18247E-08 0.10102E+00 
c  r33          0.21861E-01      15   0.53529E-08   0.12486E-07 0.12681E+00 
c  r12          0.93872E-03      18   0.62143E-08   0.30287E-09 0.60565E+00 
c  r13          0.46677E-02      18   0.68925E-08   0.14958E-08 0.19993E+00 
c  r23          0.39979E-02      19   0.62629E-08   0.12599E-08 0.19698E+00 
c  epsilon      0.10969E+02      11   0.32542E-08   0.10215E-01 0.16778E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.84926E-02 0.43441E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61366       0.0052574       0.0015074
v  Velocity[Y]            -0.57359         0.54426       0.0030807      0.00087317
v  Velocity[Z]              1.5653          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4398          4.3406          4.3632
v  Pressure                -36.383          360.04          87.653          169.87
v  r11                    0.001062        0.081951        0.013075        0.018286
v  r22                   0.0011154        0.082609        0.013355        0.018646
v  r33                   0.0016429         0.17431        0.027254        0.037207
v  r12                   -0.010669        0.013598     -0.00023384     -0.00030932
v  r13                   -0.045523        0.052791      9.3286e-05       0.0010138
v  r23                   -0.046709        0.051218      3.0578e-05      0.00057462
v  epsilon                0.069352          271.28          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099177       0.0009252       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb              0.001786          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            10899:        0.94349E+02

===============================================================


 INSTANT    0.109000000E-01   TIME STEP NUMBER           10900
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.612142979E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209781565E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.325505752E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190247955E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.436196911E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81306E-03   0.44851E-02 0.19827E+01 
c  Velocity[X]                                      0.13730E-03 
c  Velocity[Y]                                      0.12703E-03 
c  Velocity[Z]                                      0.42208E-02 
c  Pressure     0.36052E-04     133   0.91859E-02   0.25429E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50530E-08   0.16632E-08 0.99605E-01 
c  r22          0.10852E-01      13   0.55493E-08   0.18496E-08 0.10140E+00 
c  r33          0.21861E-01      15   0.57183E-08   0.12661E-07 0.12713E+00 
c  r12          0.93872E-03      18   0.57716E-08   0.30293E-09 0.60717E+00 
c  r13          0.46677E-02      19   0.57472E-08   0.15183E-08 0.20023E+00 
c  r23          0.39979E-02      19   0.60421E-08   0.12957E-08 0.19895E+00 
c  epsilon      0.10969E+02      11   0.33665E-08   0.10194E-01 0.16857E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.83920E-02 0.43295E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61365       0.0052573       0.0015074
v  Velocity[Y]            -0.57352         0.54409       0.0030806      0.00087315
v  Velocity[Z]              1.5653          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4398          4.3406          4.3632
v  Pressure                -36.437          360.06          87.669          169.88
v  r11                    0.001062        0.081955        0.013075        0.018286
v  r22                   0.0011154         0.08261        0.013355        0.018646
v  r33                   0.0016429         0.17428        0.027254        0.037207
v  r12                   -0.010668        0.013598     -0.00023384     -0.00030932
v  r13                   -0.045526        0.052789      9.3285e-05       0.0010138
v  r23                   -0.046708        0.051205      3.0578e-05      0.00057462
v  epsilon                0.069354           271.3          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099176       0.0009252       0.0017428
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb              0.001786           5.278         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            10900:        0.73737E+02

===============================================================


 INSTANT    0.109010000E-01   TIME STEP NUMBER           10901
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.467714186E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.118220702E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934911E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.520706676E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.243880746E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205895677E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81223E-03   0.45036E-02 0.19864E+01 
c  Velocity[X]                                      0.13775E-03 
c  Velocity[Y]                                      0.12809E-03 
c  Velocity[Z]                                      0.42378E-02 
c  Pressure     0.36202E-04     134   0.92156E-02   0.25535E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52188E-08   0.15941E-08 0.98466E-01 
c  r22          0.10852E-01      13   0.49860E-08   0.17950E-08 0.10046E+00 
c  r33          0.21861E-01      15   0.57012E-08   0.12156E-07 0.12546E+00 
c  r12          0.93872E-03      17   0.68293E-08   0.29159E-09 0.60310E+00 
c  r13          0.46677E-02      18   0.63396E-08   0.14812E-08 0.19886E+00 
c  r23          0.39979E-02      19   0.54692E-08   0.12533E-08 0.19627E+00 
c  epsilon      0.10969E+02      11   0.32148E-08   0.94309E-02 0.16211E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.83495E-02 0.43141E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61369       0.0052574       0.0015074
v  Velocity[Y]            -0.57359         0.54422       0.0030807       0.0008732
v  Velocity[Z]              1.5654          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4398          4.3406          4.3632
v  Pressure                -36.395          360.08          87.696           169.9
v  r11                    0.001062        0.081961        0.013075        0.018286
v  r22                   0.0011154         0.08261        0.013355        0.018646
v  r33                    0.001643         0.17424        0.027254        0.037207
v  r12                   -0.010665          0.0136     -0.00023384     -0.00030932
v  r13                   -0.045525        0.052788      9.3285e-05       0.0010138
v  r23                   -0.046708        0.051224      3.0579e-05      0.00057462
v  epsilon                0.069354          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099177       0.0009252       0.0017428
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017861          5.2772         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85284


 TIME FOR THE TIME STEP            10901:        0.71674E+02

===============================================================


 INSTANT    0.109020000E-01   TIME STEP NUMBER           10902
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.345293814E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.328747648E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267696253E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208396494E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.673487943E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81245E-03   0.45450E-02 0.19967E+01 
c  Velocity[X]                                      0.13852E-03 
c  Velocity[Y]                                      0.12871E-03 
c  Velocity[Z]                                      0.42777E-02 
c  Pressure     0.36441E-04     131   0.92721E-02   0.25703E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50430E-08   0.16621E-08 0.10000E+00 
c  r22          0.10852E-01      13   0.46348E-08   0.18347E-08 0.10099E+00 
c  r33          0.21861E-01      15   0.54326E-08   0.12662E-07 0.12755E+00 
c  r12          0.93872E-03      17   0.66699E-08   0.29613E-09 0.60571E+00 
c  r13          0.46677E-02      18   0.65638E-08   0.14976E-08 0.19930E+00 
c  r23          0.39979E-02      19   0.57420E-08   0.12959E-08 0.20012E+00 
c  epsilon      0.10969E+02      10   0.53870E-08   0.10317E-01 0.17181E+00 
c  TempC        0.25716E+06      16   0.15122E-04   0.84196E-02 0.43257E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61368       0.0052575       0.0015075
v  Velocity[Y]            -0.57358         0.54419       0.0030807      0.00087322
v  Velocity[Z]              1.5656          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4398          4.3406          4.3632
v  Pressure                -36.431          359.97          87.616          169.81
v  r11                    0.001062        0.081972        0.013075        0.018286
v  r22                   0.0011154        0.082611        0.013355        0.018646
v  r33                    0.001643         0.17424        0.027254        0.037207
v  r12                   -0.010665        0.013601     -0.00023384     -0.00030932
v  r13                   -0.045523         0.05279      9.3285e-05       0.0010138
v  r23                   -0.046707        0.051215      3.0579e-05      0.00057462
v  epsilon                0.069356          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099178      0.00092521       0.0017428
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017861          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            10902:        0.72055E+02

===============================================================


 INSTANT    0.109030000E-01   TIME STEP NUMBER           10903
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.137657644E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.379403470E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227494877E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.225815851E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.769654698E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81309E-03   0.44835E-02 0.19832E+01 
c  Velocity[X]                                      0.13775E-03 
c  Velocity[Y]                                      0.12805E-03 
c  Velocity[Z]                                      0.42177E-02 
c  Pressure     0.36229E-04     132   0.92266E-02   0.25554E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52048E-08   0.16090E-08 0.98386E-01 
c  r22          0.10852E-01      13   0.47611E-08   0.17973E-08 0.10033E+00 
c  r33          0.21861E-01      15   0.56484E-08   0.12307E-07 0.12598E+00 
c  r12          0.93872E-03      18   0.49447E-08   0.29687E-09 0.60427E+00 
c  r13          0.46677E-02      19   0.56314E-08   0.14856E-08 0.19856E+00 
c  r23          0.39979E-02      19   0.54939E-08   0.12762E-08 0.19792E+00 
c  epsilon      0.10969E+02      11   0.33840E-08   0.96893E-02 0.16394E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.84081E-02 0.43254E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61364       0.0052575       0.0015075
v  Velocity[Y]            -0.57353         0.54426       0.0030807       0.0008732
v  Velocity[Z]              1.5655          5.4399          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4399          4.3406          4.3632
v  Pressure                -36.365          360.02           87.64          169.85
v  r11                    0.001062        0.081977        0.013075        0.018286
v  r22                   0.0011154         0.08261        0.013355        0.018646
v  r33                    0.001643         0.17425        0.027254        0.037207
v  r12                   -0.010666        0.013598     -0.00023384     -0.00030932
v  r13                   -0.045526        0.052787      9.3285e-05       0.0010138
v  r23                   -0.046707        0.051202       3.058e-05      0.00057462
v  epsilon                0.069357          271.26          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099179      0.00092521       0.0017428
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017861          5.2781         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            10903:        0.76498E+02

===============================================================


 INSTANT    0.109040000E-01   TIME STEP NUMBER           10904
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.459532984E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122349241E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.135361341E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.204412801E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.109595209E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81272E-03   0.44879E-02 0.19849E+01 
c  Velocity[X]                                      0.13683E-03 
c  Velocity[Y]                                      0.12738E-03 
c  Velocity[Z]                                      0.42237E-02 
c  Pressure     0.36535E-04     132   0.92971E-02   0.25770E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51331E-08   0.15913E-08 0.97916E-01 
c  r22          0.10852E-01      13   0.51590E-08   0.18146E-08 0.10057E+00 
c  r33          0.21861E-01      14   0.70016E-08   0.12295E-07 0.12581E+00 
c  r12          0.93872E-03      17   0.67895E-08   0.29338E-09 0.60201E+00 
c  r13          0.46677E-02      18   0.71884E-08   0.14885E-08 0.19875E+00 
c  r23          0.39979E-02      19   0.58081E-08   0.12440E-08 0.19609E+00 
c  epsilon      0.10969E+02      11   0.33264E-08   0.97190E-02 0.16337E+00 
c  TempC        0.25716E+06      16   0.15194E-04   0.84483E-02 0.43346E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61363       0.0052574       0.0015074
v  Velocity[Y]             -0.5734         0.54435       0.0030806       0.0008732
v  Velocity[Z]              1.5656          5.4398          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4398          4.3406          4.3632
v  Pressure                -36.404          359.97           87.63          169.82
v  r11                    0.001062        0.081976        0.013075        0.018286
v  r22                   0.0011154        0.082609        0.013355        0.018646
v  r33                    0.001643         0.17423        0.027254        0.037207
v  r12                   -0.010665        0.013598     -0.00023384     -0.00030932
v  r13                   -0.045524        0.052788      9.3285e-05       0.0010138
v  r23                   -0.046706        0.051216      3.0579e-05      0.00057462
v  epsilon                0.069358          271.25          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099179      0.00092521       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017861          5.2782         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            10904:        0.75585E+02

===============================================================


 INSTANT    0.109050000E-01   TIME STEP NUMBER           10905
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.124292785E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.254357461E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.216630642E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.172728901E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.365143889E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81200E-03   0.45216E-02 0.19923E+01 
c  Velocity[X]                                      0.13809E-03 
c  Velocity[Y]                                      0.12853E-03 
c  Velocity[Z]                                      0.42550E-02 
c  Pressure     0.36284E-04     132   0.92344E-02   0.25593E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49699E-08   0.16200E-08 0.98489E-01 
c  r22          0.10852E-01      13   0.45717E-08   0.18101E-08 0.10049E+00 
c  r33          0.21861E-01      15   0.53915E-08   0.12458E-07 0.12641E+00 
c  r12          0.93872E-03      17   0.67020E-08   0.29329E-09 0.60196E+00 
c  r13          0.46677E-02      19   0.56910E-08   0.14934E-08 0.19888E+00 
c  r23          0.39979E-02      19   0.59405E-08   0.12746E-08 0.19781E+00 
c  epsilon      0.10969E+02      11   0.32154E-08   0.97774E-02 0.16386E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84114E-02 0.43258E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63326         0.61365       0.0052574       0.0015074
v  Velocity[Y]            -0.57354         0.54417       0.0030807      0.00087322
v  Velocity[Z]              1.5655          5.4399          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4399          4.3406          4.3632
v  Pressure                 -36.36           360.1          87.698          169.92
v  r11                    0.001062        0.081973        0.013075        0.018286
v  r22                   0.0011154         0.08261        0.013355        0.018646
v  r33                    0.001643         0.17424        0.027254        0.037207
v  r12                   -0.010664          0.0136     -0.00023384     -0.00030932
v  r13                   -0.045525        0.052789      9.3285e-05       0.0010138
v  r23                   -0.046705        0.051197      3.0579e-05      0.00057462
v  epsilon                0.069359          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099179      0.00092521       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017861          5.2785         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            10905:        0.79855E+02

===============================================================


 INSTANT    0.109060000E-01   TIME STEP NUMBER           10906
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.155241587E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.751181387E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.705855003E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.113554088E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.176775492E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81303E-03   0.45205E-02 0.19920E+01 
c  Velocity[X]                                      0.13814E-03 
c  Velocity[Y]                                      0.12782E-03 
c  Velocity[Z]                                      0.42546E-02 
c  Pressure     0.36357E-04     131   0.92504E-02   0.25644E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49707E-08   0.16524E-08 0.98987E-01 
c  r22          0.10852E-01      13   0.49488E-08   0.18168E-08 0.10028E+00 
c  r33          0.21861E-01      15   0.54873E-08   0.12589E-07 0.12646E+00 
c  r12          0.93872E-03      18   0.58204E-08   0.30073E-09 0.60432E+00 
c  r13          0.46677E-02      19   0.67982E-08   0.15006E-08 0.19855E+00 
c  r23          0.39979E-02      19   0.64394E-08   0.12940E-08 0.19794E+00 
c  epsilon      0.10969E+02      11   0.33460E-08   0.10275E-01 0.16795E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.83470E-02 0.43131E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6333         0.61361       0.0052574       0.0015074
v  Velocity[Y]            -0.57352         0.54413       0.0030807      0.00087324
v  Velocity[Z]              1.5654          5.4399          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4399          4.3406          4.3632
v  Pressure                -36.445          359.94          87.603          169.79
v  r11                    0.001062        0.081971        0.013075        0.018286
v  r22                   0.0011154         0.08261        0.013355        0.018646
v  r33                    0.001643         0.17424        0.027254        0.037207
v  r12                   -0.010662        0.013595     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052789      9.3285e-05       0.0010138
v  r23                   -0.046705        0.051178       3.058e-05      0.00057462
v  epsilon                 0.06936          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05        0.009918      0.00092521       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017861          5.2787         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85283


 TIME FOR THE TIME STEP            10906:        0.83031E+02

===============================================================


 INSTANT    0.109070000E-01   TIME STEP NUMBER           10907
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.854378496E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111814024E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.115036429E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.474943430E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221173057E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81237E-03   0.45237E-02 0.19909E+01 
c  Velocity[X]                                      0.13844E-03 
c  Velocity[Y]                                      0.12840E-03 
c  Velocity[Z]                                      0.42569E-02 
c  Pressure     0.36389E-04     132   0.92698E-02   0.25666E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.48415E-08   0.16522E-08 0.99413E-01 
c  r22          0.10852E-01      13   0.50143E-08   0.18210E-08 0.10093E+00 
c  r33          0.21861E-01      15   0.63944E-08   0.12584E-07 0.12717E+00 
c  r12          0.93872E-03      18   0.56273E-08   0.29800E-09 0.60420E+00 
c  r13          0.46677E-02      19   0.62667E-08   0.14991E-08 0.19948E+00 
c  r23          0.39979E-02      19   0.66021E-08   0.13054E-08 0.19977E+00 
c  epsilon      0.10969E+02      11   0.35772E-08   0.98970E-02 0.16481E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.84394E-02 0.43324E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61366       0.0052575       0.0015074
v  Velocity[Y]            -0.57354         0.54421       0.0030807      0.00087325
v  Velocity[Z]              1.5656          5.4399          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4399          4.3406          4.3632
v  Pressure                -36.373          360.01          87.643          169.85
v  r11                    0.001062        0.081966        0.013075        0.018286
v  r22                   0.0011154        0.082605        0.013355        0.018646
v  r33                    0.001643         0.17424        0.027254        0.037207
v  r12                    -0.01066        0.013597     -0.00023384     -0.00030932
v  r13                   -0.045524        0.052791      9.3285e-05       0.0010138
v  r23                   -0.046704        0.051202       3.058e-05      0.00057462
v  epsilon                0.069361          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05        0.009918      0.00092521       0.0017428
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017861          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            10907:        0.86514E+02

===============================================================


 INSTANT    0.109080000E-01   TIME STEP NUMBER           10908
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.198745842E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.967422902E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155016854E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.746971459E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.121945193E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81300E-03   0.44790E-02 0.19826E+01 
c  Velocity[X]                                      0.13751E-03 
c  Velocity[Y]                                      0.12827E-03 
c  Velocity[Z]                                      0.42132E-02 
c  Pressure     0.35881E-04     133   0.91382E-02   0.25308E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52375E-08   0.15850E-08 0.97662E-01 
c  r22          0.10852E-01      13   0.50119E-08   0.17997E-08 0.10035E+00 
c  r33          0.21861E-01      15   0.64864E-08   0.12200E-07 0.12531E+00 
c  r12          0.93873E-03      18   0.54194E-08   0.29352E-09 0.59829E+00 
c  r13          0.46677E-02      19   0.61251E-08   0.14901E-08 0.19879E+00 
c  r23          0.39979E-02      19   0.61799E-08   0.12453E-08 0.19547E+00 
c  epsilon      0.10969E+02      11   0.35570E-08   0.94354E-02 0.16177E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.84002E-02 0.43266E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63323         0.61364       0.0052575       0.0015074
v  Velocity[Y]            -0.57351         0.54434       0.0030807      0.00087328
v  Velocity[Z]              1.5654          5.4399          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4399          4.3406          4.3632
v  Pressure                -36.456          360.04          87.677          169.87
v  r11                    0.001062        0.081967        0.013075        0.018286
v  r22                   0.0011154        0.082606        0.013355        0.018646
v  r33                    0.001643         0.17426        0.027254        0.037207
v  r12                   -0.010657          0.0136     -0.00023384     -0.00030932
v  r13                   -0.045523        0.052791      9.3285e-05       0.0010138
v  r23                   -0.046705        0.051192       3.058e-05      0.00057462
v  epsilon                0.069362          271.26          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9933e-05       0.0099179      0.00092521       0.0017428
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017861          5.2787         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85284


 TIME FOR THE TIME STEP            10908:        0.73032E+02

===============================================================


 INSTANT    0.109090000E-01   TIME STEP NUMBER           10909
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.360146673E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.333379033E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.968252708E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.716735919E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.324290897E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81261E-03   0.44836E-02 0.19862E+01 
c  Velocity[X]                                      0.13735E-03 
c  Velocity[Y]                                      0.12796E-03 
c  Velocity[Z]                                      0.42182E-02 
c  Pressure     0.36343E-04     136   0.92417E-02   0.25634E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54148E-08   0.16444E-08 0.99200E-01 
c  r22          0.10852E-01      13   0.52365E-08   0.18333E-08 0.10049E+00 
c  r33          0.21861E-01      15   0.53575E-08   0.12618E-07 0.12700E+00 
c  r12          0.93873E-03      18   0.58678E-08   0.30052E-09 0.60425E+00 
c  r13          0.46677E-02      18   0.71803E-08   0.15011E-08 0.19861E+00 
c  r23          0.39979E-02      19   0.61929E-08   0.12790E-08 0.19871E+00 
c  epsilon      0.10969E+02      11   0.34001E-08   0.10268E-01 0.17157E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.83933E-02 0.43242E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63329         0.61361       0.0052574       0.0015074
v  Velocity[Y]            -0.57365         0.54412       0.0030808      0.00087332
v  Velocity[Z]              1.5657          5.4399          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4399          4.3406          4.3632
v  Pressure                -36.386          360.05          87.644          169.87
v  r11                    0.001062        0.081963        0.013075        0.018286
v  r22                   0.0011154        0.082608        0.013355        0.018646
v  r33                    0.001643         0.17425        0.027254        0.037207
v  r12                   -0.010654        0.013606     -0.00023384     -0.00030932
v  r13                   -0.045527        0.052789      9.3285e-05       0.0010138
v  r23                   -0.046705        0.051185       3.058e-05      0.00057462
v  epsilon                0.069363          271.27          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099179      0.00092521       0.0017428
v  CourantNb               0.44257             0.6         0.59908         0.59839
v  FourierNb             0.0017862          5.2786         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            10909:        0.77623E+02

===============================================================


 INSTANT    0.109100000E-01   TIME STEP NUMBER           10910
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.655209055E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.665901792E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149165227E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.461425356E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.109123738E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      45   0.81251E-03   0.45274E-02 0.19925E+01 
c  Velocity[X]                                      0.13837E-03 
c  Velocity[Y]                                      0.12805E-03 
c  Velocity[Z]                                      0.42610E-02 
c  Pressure     0.36385E-04     132   0.92628E-02   0.25664E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57152E-08   0.16645E-08 0.99484E-01 
c  r22          0.10852E-01      13   0.48994E-08   0.18646E-08 0.10130E+00 
c  r33          0.21861E-01      15   0.59010E-08   0.12804E-07 0.12735E+00 
c  r12          0.93873E-03      18   0.59165E-08   0.30070E-09 0.60218E+00 
c  r13          0.46677E-02      19   0.57282E-08   0.15284E-08 0.20026E+00 
c  r23          0.39979E-02      19   0.55653E-08   0.12969E-08 0.19885E+00 
c  epsilon      0.10969E+02      11   0.34453E-08   0.10365E-01 0.16816E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.84373E-02 0.43333E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61363       0.0052574       0.0015075
v  Velocity[Y]             -0.5737         0.54425       0.0030807      0.00087328
v  Velocity[Z]              1.5658          5.4399          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4399          4.3406          4.3632
v  Pressure                -36.432          359.96          87.631          169.81
v  r11                    0.001062        0.081966        0.013075        0.018286
v  r22                   0.0011154        0.082609        0.013355        0.018646
v  r33                    0.001643         0.17425        0.027254        0.037207
v  r12                   -0.010662          0.0136     -0.00023384     -0.00030932
v  r13                   -0.045524        0.052791      9.3286e-05       0.0010138
v  r23                   -0.046705        0.051174       3.058e-05      0.00057462
v  epsilon                0.069364          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099178      0.00092521       0.0017428
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017862          5.2789         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            10910:        0.73267E+02

===============================================================


 INSTANT    0.109110000E-01   TIME STEP NUMBER           10911
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119446770E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.404055400E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.212968201E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.302721039E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.548327270E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81288E-03   0.45192E-02 0.19884E+01 
c  Velocity[X]                                      0.13781E-03 
c  Velocity[Y]                                      0.12821E-03 
c  Velocity[Z]                                      0.42532E-02 
c  Pressure     0.36131E-04     134   0.91928E-02   0.25484E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51543E-08   0.16213E-08 0.99002E-01 
c  r22          0.10852E-01      13   0.48171E-08   0.18118E-08 0.10069E+00 
c  r33          0.21861E-01      15   0.53549E-08   0.12349E-07 0.12644E+00 
c  r12          0.93873E-03      18   0.54051E-08   0.29284E-09 0.60089E+00 
c  r13          0.46677E-02      19   0.61846E-08   0.14853E-08 0.19926E+00 
c  r23          0.39979E-02      19   0.62783E-08   0.12649E-08 0.19815E+00 
c  epsilon      0.10969E+02      11   0.32565E-08   0.94226E-02 0.16109E+00 
c  TempC        0.25716E+06      16   0.15118E-04   0.83853E-02 0.43246E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63319         0.61365       0.0052575       0.0015075
v  Velocity[Y]            -0.57373         0.54427       0.0030808      0.00087333
v  Velocity[Z]              1.5653          5.4399          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4399          4.3406          4.3632
v  Pressure                -36.383          360.02          87.633          169.84
v  r11                    0.001062        0.081961        0.013075        0.018286
v  r22                   0.0011154        0.082609        0.013355        0.018646
v  r33                    0.001643         0.17425        0.027254        0.037207
v  r12                   -0.010664        0.013602     -0.00023384     -0.00030932
v  r13                   -0.045523        0.052788      9.3287e-05       0.0010138
v  r23                   -0.046706        0.051197       3.058e-05      0.00057462
v  epsilon                0.069365          271.26          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099178      0.00092521       0.0017428
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017862          5.2784         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85284


 TIME FOR THE TIME STEP            10911:        0.73304E+02

===============================================================


 INSTANT    0.109120000E-01   TIME STEP NUMBER           10912
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.386894458E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.309717816E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136414364E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.295185477E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151447022E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81271E-03   0.45022E-02 0.19877E+01 
c  Velocity[X]                                      0.13817E-03 
c  Velocity[Y]                                      0.12778E-03 
c  Velocity[Z]                                      0.42362E-02 
c  Pressure     0.36657E-04     133   0.93297E-02   0.25855E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50223E-08   0.16152E-08 0.98410E-01 
c  r22          0.10852E-01      13   0.49557E-08   0.18609E-08 0.10165E+00 
c  r33          0.21861E-01      15   0.58118E-08   0.12515E-07 0.12680E+00 
c  r12          0.93873E-03      18   0.58155E-08   0.30017E-09 0.60224E+00 
c  r13          0.46677E-02      19   0.64202E-08   0.15011E-08 0.19999E+00 
c  r23          0.39979E-02      19   0.57623E-08   0.12765E-08 0.19764E+00 
c  epsilon      0.10969E+02      11   0.33595E-08   0.10026E-01 0.16637E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.83819E-02 0.43195E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63325         0.61362       0.0052574       0.0015074
v  Velocity[Y]            -0.57354         0.54432       0.0030808      0.00087329
v  Velocity[Z]              1.5655          5.4399          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4399          4.3406          4.3632
v  Pressure                -36.439          360.03          87.641          169.85
v  r11                    0.001062        0.081966        0.013075        0.018286
v  r22                   0.0011154        0.082609        0.013355        0.018646
v  r33                    0.001643         0.17428        0.027254        0.037207
v  r12                   -0.010663        0.013606     -0.00023384     -0.00030932
v  r13                   -0.045525        0.052788      9.3286e-05       0.0010138
v  r23                   -0.046705        0.051192       3.058e-05      0.00057462
v  epsilon                0.069366          271.28          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099177      0.00092521       0.0017428
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017862          5.2784         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85284


 TIME FOR THE TIME STEP            10912:        0.72363E+02

===============================================================


 INSTANT    0.109130000E-01   TIME STEP NUMBER           10913
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105576445E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.125501450E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227654399E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.292097144E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.565353262E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81199E-03   0.45245E-02 0.19904E+01 
c  Velocity[X]                                      0.13799E-03 
c  Velocity[Y]                                      0.12810E-03 
c  Velocity[Z]                                      0.42585E-02 
c  Pressure     0.35692E-04     131   0.90803E-02   0.25175E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54809E-08   0.16426E-08 0.98966E-01 
c  r22          0.10852E-01      13   0.53414E-08   0.18352E-08 0.10112E+00 
c  r33          0.21861E-01      15   0.63189E-08   0.12596E-07 0.12698E+00 
c  r12          0.93873E-03      18   0.55984E-08   0.29865E-09 0.60229E+00 
c  r13          0.46677E-02      19   0.70724E-08   0.14981E-08 0.20039E+00 
c  r23          0.39979E-02      19   0.68858E-08   0.12737E-08 0.19800E+00 
c  epsilon      0.10969E+02      11   0.33946E-08   0.10245E-01 0.16653E+00 
c  TempC        0.25716E+06      16   0.15178E-04   0.84000E-02 0.43219E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63336         0.61367       0.0052575       0.0015075
v  Velocity[Y]             -0.5734         0.54439       0.0030808      0.00087331
v  Velocity[Z]              1.5655          5.4399          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4399          4.3406          4.3632
v  Pressure                -36.378          360.02          87.651          169.85
v  r11                    0.001062        0.081961        0.013075        0.018286
v  r22                   0.0011154        0.082605        0.013355        0.018646
v  r33                    0.001643         0.17426        0.027254        0.037207
v  r12                    -0.01066        0.013601     -0.00023384     -0.00030932
v  r13                   -0.045524         0.05279      9.3287e-05       0.0010138
v  r23                   -0.046706        0.051188       3.058e-05      0.00057462
v  epsilon                0.069367          271.31          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099177      0.00092521       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017862          5.2781         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            10913:        0.82341E+02

===============================================================


 INSTANT    0.109140000E-01   TIME STEP NUMBER           10914
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.329468408E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.788693280E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.938203130E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.190124832E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155822628E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81282E-03   0.45168E-02 0.19900E+01 
c  Velocity[X]                                      0.13716E-03 
c  Velocity[Y]                                      0.12959E-03 
c  Velocity[Z]                                      0.42501E-02 
c  Pressure     0.36149E-04     134   0.92020E-02   0.25497E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56599E-08   0.16160E-08 0.98456E-01 
c  r22          0.10852E-01      13   0.51498E-08   0.18283E-08 0.10117E+00 
c  r33          0.21861E-01      15   0.66079E-08   0.12490E-07 0.12700E+00 
c  r12          0.93873E-03      18   0.54142E-08   0.29803E-09 0.60117E+00 
c  r13          0.46677E-02      19   0.72026E-08   0.15065E-08 0.20113E+00 
c  r23          0.39979E-02      20   0.56580E-08   0.12588E-08 0.19739E+00 
c  epsilon      0.10969E+02      11   0.35063E-08   0.99230E-02 0.16498E+00 
c  TempC        0.25716E+06      16   0.15174E-04   0.84396E-02 0.43300E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63324         0.61365       0.0052574       0.0015074
v  Velocity[Y]            -0.57347          0.5442       0.0030808      0.00087329
v  Velocity[Z]              1.5657          5.4399          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4399          4.3406          4.3632
v  Pressure                 -36.45          360.09          87.693           169.9
v  r11                    0.001062        0.081968        0.013075        0.018286
v  r22                   0.0011154        0.082607        0.013355        0.018646
v  r33                    0.001643         0.17425        0.027254        0.037207
v  r12                   -0.010658        0.013599     -0.00023385     -0.00030932
v  r13                   -0.045523         0.05279      9.3287e-05       0.0010138
v  r23                   -0.046706        0.051206       3.058e-05      0.00057462
v  epsilon                0.069368          271.25          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9933e-05       0.0099177      0.00092521       0.0017428
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017862          5.2778         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85284


 TIME FOR THE TIME STEP            10914:        0.72586E+02

===============================================================


 INSTANT    0.109150000E-01   TIME STEP NUMBER           10915
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130410810E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.380346987E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.323808128E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.127436960E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242337855E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81271E-03   0.44705E-02 0.19791E+01 
c  Velocity[X]                                      0.13693E-03 
c  Velocity[Y]                                      0.12757E-03 
c  Velocity[Z]                                      0.42060E-02 
c  Pressure     0.36161E-04     133   0.92084E-02   0.25504E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58947E-08   0.16405E-08 0.99574E-01 
c  r22          0.10852E-01      13   0.50479E-08   0.18061E-08 0.10094E+00 
c  r33          0.21861E-01      15   0.53810E-08   0.12447E-07 0.12740E+00 
c  r12          0.93873E-03      18   0.57233E-08   0.29858E-09 0.60294E+00 
c  r13          0.46677E-02      19   0.60111E-08   0.14876E-08 0.20012E+00 
c  r23          0.39979E-02      19   0.68447E-08   0.12913E-08 0.20030E+00 
c  epsilon      0.10969E+02      11   0.35012E-08   0.10008E-01 0.17002E+00 
c  TempC        0.25716E+06      16   0.15107E-04   0.83806E-02 0.43140E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63322         0.61363       0.0052574       0.0015074
v  Velocity[Y]            -0.57373         0.54417       0.0030808      0.00087329
v  Velocity[Z]              1.5655            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5793            5.44          4.3406          4.3632
v  Pressure                -36.407          360.01          87.626          169.83
v  r11                    0.001062        0.081971        0.013075        0.018286
v  r22                   0.0011154        0.082608        0.013355        0.018646
v  r33                    0.001643         0.17427        0.027254        0.037207
v  r12                   -0.010659        0.013599     -0.00023385     -0.00030932
v  r13                   -0.045526        0.052789      9.3287e-05       0.0010138
v  r23                   -0.046706        0.051199       3.058e-05      0.00057462
v  epsilon                0.069369          271.25          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099176      0.00092521       0.0017428
v  CourantNb               0.44258             0.6         0.59908         0.59839
v  FourierNb             0.0017862          5.2771         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71352         0.85284


 TIME FOR THE TIME STEP            10915:        0.71714E+02

===============================================================


 INSTANT    0.109160000E-01   TIME STEP NUMBER           10916
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.388368350E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.301991573E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.322471804E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.252345513E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.653477635E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81310E-03   0.45151E-02 0.19895E+01 
c  Velocity[X]                                      0.13824E-03 
c  Velocity[Y]                                      0.12731E-03 
c  Velocity[Z]                                      0.42495E-02 
c  Pressure     0.36614E-04     132   0.93163E-02   0.25825E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55996E-08   0.16067E-08 0.98347E-01 
c  r22          0.10852E-01      13   0.50736E-08   0.17932E-08 0.10016E+00 
c  r33          0.21861E-01      15   0.54604E-08   0.12323E-07 0.12572E+00 
c  r12          0.93873E-03      18   0.57318E-08   0.29306E-09 0.59948E+00 
c  r13          0.46677E-02      19   0.58078E-08   0.14756E-08 0.19835E+00 
c  r23          0.39979E-02      19   0.63936E-08   0.12696E-08 0.19683E+00 
c  epsilon      0.10969E+02      11   0.33020E-08   0.99461E-02 0.16601E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.83597E-02 0.43182E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6333         0.61367       0.0052576       0.0015075
v  Velocity[Y]            -0.57362         0.54424       0.0030808      0.00087331
v  Velocity[Z]              1.5653            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5792            5.44          4.3406          4.3632
v  Pressure                -36.438          359.99          87.615          169.82
v  r11                    0.001062        0.081979        0.013075        0.018286
v  r22                   0.0011154        0.082608        0.013355        0.018646
v  r33                    0.001643         0.17429        0.027254        0.037207
v  r12                   -0.010658        0.013601     -0.00023384     -0.00030932
v  r13                   -0.045524        0.052789      9.3287e-05       0.0010138
v  r23                   -0.046706        0.051175       3.058e-05      0.00057462
v  epsilon                 0.06937           271.3          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099175      0.00092522       0.0017428
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017862          5.2772         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85284


 TIME FOR THE TIME STEP            10916:        0.72282E+02

===============================================================


 INSTANT    0.109170000E-01   TIME STEP NUMBER           10917
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.434258878E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.177385730E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.260839517E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110466181E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.253569538E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81274E-03   0.45338E-02 0.19936E+01 
c  Velocity[X]                                      0.13842E-03 
c  Velocity[Y]                                      0.12840E-03 
c  Velocity[Z]                                      0.42670E-02 
c  Pressure     0.36039E-04     132   0.91794E-02   0.25418E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55907E-08   0.16195E-08 0.98645E-01 
c  r22          0.10852E-01      13   0.53342E-08   0.17986E-08 0.10029E+00 
c  r33          0.21861E-01      15   0.53332E-08   0.12321E-07 0.12619E+00 
c  r12          0.93873E-03      18   0.60118E-08   0.28976E-09 0.59626E+00 
c  r13          0.46677E-02      19   0.62919E-08   0.14857E-08 0.19910E+00 
c  r23          0.39979E-02      19   0.64886E-08   0.12697E-08 0.19822E+00 
c  epsilon      0.10969E+02      11   0.32459E-08   0.96185E-02 0.16261E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.84089E-02 0.43296E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63331         0.61371       0.0052575       0.0015074
v  Velocity[Y]            -0.57365         0.54433       0.0030808      0.00087329
v  Velocity[Z]              1.5655            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5793            5.44          4.3406          4.3632
v  Pressure                -36.453             360          87.618          169.83
v  r11                    0.001062        0.081978        0.013075        0.018286
v  r22                   0.0011154         0.08261        0.013355        0.018646
v  r33                    0.001643         0.17433        0.027254        0.037207
v  r12                   -0.010666        0.013597     -0.00023384     -0.00030932
v  r13                   -0.045525        0.052789      9.3287e-05       0.0010138
v  r23                   -0.046706        0.051199       3.058e-05      0.00057462
v  epsilon                0.069371          271.31          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9939e-05       0.0099175      0.00092522       0.0017428
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017862          5.2772         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85283


 TIME FOR THE TIME STEP            10917:        0.89341E+02

===============================================================


 INSTANT    0.109180000E-01   TIME STEP NUMBER           10918
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.691436203E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.768371275E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158195253E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.163204551E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.548282268E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81374E-03   0.44973E-02 0.19867E+01 
c  Velocity[X]                                      0.13781E-03 
c  Velocity[Y]                                      0.12815E-03 
c  Velocity[Z]                                      0.42314E-02 
c  Pressure     0.36327E-04     132   0.92451E-02   0.25622E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55648E-08   0.16352E-08 0.99058E-01 
c  r22          0.10852E-01      13   0.52233E-08   0.18531E-08 0.10149E+00 
c  r33          0.21861E-01      15   0.58991E-08   0.12703E-07 0.12802E+00 
c  r12          0.93873E-03      18   0.58643E-08   0.30263E-09 0.60809E+00 
c  r13          0.46677E-02      19   0.67603E-08   0.15083E-08 0.20065E+00 
c  r23          0.39979E-02      19   0.60985E-08   0.12942E-08 0.20040E+00 
c  epsilon      0.10969E+02      11   0.33882E-08   0.99661E-02 0.16638E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.84135E-02 0.43297E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161988


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63322         0.61366       0.0052575       0.0015075
v  Velocity[Y]            -0.57353         0.54441       0.0030808      0.00087331
v  Velocity[Z]              1.5654            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5792            5.44          4.3406          4.3632
v  Pressure                -36.449          359.97          87.622          169.81
v  r11                    0.001062        0.081984        0.013075        0.018286
v  r22                   0.0011154         0.08261        0.013355        0.018646
v  r33                    0.001643         0.17432        0.027254        0.037207
v  r12                   -0.010665        0.013602     -0.00023385     -0.00030932
v  r13                   -0.045527        0.052788      9.3286e-05       0.0010138
v  r23                   -0.046706        0.051193       3.058e-05      0.00057462
v  epsilon                0.069372           271.3          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.994e-05       0.0099175      0.00092522       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2768         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71352         0.85284


 TIME FOR THE TIME STEP            10918:        0.76943E+02

===============================================================


 INSTANT    0.109190000E-01   TIME STEP NUMBER           10919
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.780148175E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130656452E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.110526704E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.655715026E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154761648E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81202E-03   0.44928E-02 0.19843E+01 
c  Velocity[X]                                      0.13695E-03 
c  Velocity[Y]                                      0.12770E-03 
c  Velocity[Z]                                      0.42282E-02 
c  Pressure     0.36041E-04     133   0.91742E-02   0.25421E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51538E-08   0.16333E-08 0.99002E-01 
c  r22          0.10852E-01      13   0.53622E-08   0.18161E-08 0.10053E+00 
c  r33          0.21861E-01      14   0.70589E-08   0.12429E-07 0.12656E+00 
c  r12          0.93873E-03      18   0.60055E-08   0.29835E-09 0.59994E+00 
c  r13          0.46677E-02      19   0.57543E-08   0.14869E-08 0.19870E+00 
c  r23          0.39979E-02      19   0.53089E-08   0.12804E-08 0.19836E+00 
c  epsilon      0.10969E+02      11   0.32970E-08   0.98511E-02 0.16428E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.84311E-02 0.43302E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161988


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6332          0.6137       0.0052576       0.0015075
v  Velocity[Y]            -0.57359          0.5442       0.0030808      0.00087331
v  Velocity[Z]              1.5655            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5793            5.44          4.3406          4.3632
v  Pressure                -36.365          359.93          87.568          169.76
v  r11                    0.001062        0.081978        0.013075        0.018286
v  r22                   0.0011154         0.08261        0.013355        0.018646
v  r33                    0.001643         0.17427        0.027254        0.037207
v  r12                   -0.010663        0.013596     -0.00023385     -0.00030932
v  r13                   -0.045524        0.052788      9.3287e-05       0.0010138
v  r23                   -0.046707        0.051185       3.058e-05      0.00057462
v  epsilon                0.069373          271.26          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9944e-05       0.0099175      0.00092522       0.0017428
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2772         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85284


 TIME FOR THE TIME STEP            10919:        0.75815E+02

===============================================================


 INSTANT    0.109200000E-01   TIME STEP NUMBER           10920
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.144249470E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.350334235E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934913E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168700059E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.146885129E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.260723887E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81297E-03   0.45252E-02 0.19926E+01 
c  Velocity[X]                                      0.13887E-03 
c  Velocity[Y]                                      0.12861E-03 
c  Velocity[Z]                                      0.42577E-02 
c  Pressure     0.36656E-04     133   0.93297E-02   0.25854E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53335E-08   0.16361E-08 0.99184E-01 
c  r22          0.10852E-01      13   0.50861E-08   0.18093E-08 0.10066E+00 
c  r33          0.21861E-01      15   0.58393E-08   0.12494E-07 0.12685E+00 
c  r12          0.93873E-03      18   0.54483E-08   0.29664E-09 0.60200E+00 
c  r13          0.46677E-02      19   0.71532E-08   0.14902E-08 0.19924E+00 
c  r23          0.39979E-02      19   0.68035E-08   0.12832E-08 0.19826E+00 
c  epsilon      0.10969E+02      11   0.33907E-08   0.97762E-02 0.16385E+00 
c  TempC        0.25716E+06      16   0.15187E-04   0.83883E-02 0.43210E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63333         0.61368       0.0052574       0.0015074
v  Velocity[Y]            -0.57347         0.54435       0.0030807       0.0008733
v  Velocity[Z]              1.5656            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5794            5.44          4.3406          4.3632
v  Pressure                -36.443          360.03          87.659          169.86
v  r11                    0.001062         0.08198        0.013075        0.018286
v  r22                   0.0011154        0.082611        0.013355        0.018646
v  r33                   0.0016431         0.17429        0.027254        0.037207
v  r12                   -0.010661        0.013596     -0.00023385     -0.00030932
v  r13                   -0.045523        0.052788      9.3287e-05       0.0010138
v  r23                   -0.046706        0.051171      3.0579e-05      0.00057462
v  epsilon                0.069374          271.25          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9948e-05       0.0099176      0.00092522       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017862          5.2781         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            10920:        0.80716E+02

===============================================================


 INSTANT    0.109210000E-01   TIME STEP NUMBER           10921
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186041736E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.501912603E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.194660436E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935018E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.665823271E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.910929447E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81321E-03   0.45087E-02 0.19872E+01 
c  Velocity[X]                                      0.13746E-03 
c  Velocity[Y]                                      0.12825E-03 
c  Velocity[Z]                                      0.42430E-02 
c  Pressure     0.36036E-04     133   0.91782E-02   0.25417E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55469E-08   0.16703E-08 0.10012E+00 
c  r22          0.10852E-01      13   0.58901E-08   0.18516E-08 0.10165E+00 
c  r33          0.21861E-01      15   0.61481E-08   0.12769E-07 0.12801E+00 
c  r12          0.93873E-03      17   0.69316E-08   0.30944E-09 0.61081E+00 
c  r13          0.46677E-02      19   0.73953E-08   0.15025E-08 0.20010E+00 
c  r23          0.39979E-02      19   0.66085E-08   0.13080E-08 0.20139E+00 
c  epsilon      0.10969E+02      11   0.33970E-08   0.10406E-01 0.17213E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.83806E-02 0.43222E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63331         0.61367       0.0052575       0.0015075
v  Velocity[Y]            -0.57349         0.54405       0.0030808      0.00087331
v  Velocity[Z]              1.5654            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5793            5.44          4.3406          4.3632
v  Pressure                -36.393          360.02          87.643          169.85
v  r11                    0.001062        0.081976        0.013075        0.018286
v  r22                   0.0011154        0.082607        0.013356        0.018646
v  r33                   0.0016431         0.17432        0.027254        0.037207
v  r12                   -0.010657        0.013598     -0.00023385     -0.00030932
v  r13                   -0.045528         0.05279      9.3288e-05       0.0010138
v  r23                   -0.046706          0.0512      3.0579e-05      0.00057462
v  epsilon                0.069375          271.27          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9953e-05       0.0099175      0.00092522       0.0017428
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2789         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            10921:        0.70711E+02

===============================================================


 INSTANT    0.109220000E-01   TIME STEP NUMBER           10922
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.419572796E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.311027069E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.554673887E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.318690729E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.193643607E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81231E-03   0.45162E-02 0.19901E+01 
c  Velocity[X]                                      0.13807E-03 
c  Velocity[Y]                                      0.12842E-03 
c  Velocity[Z]                                      0.42497E-02 
c  Pressure     0.36122E-04     132   0.91961E-02   0.25478E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51162E-08   0.16433E-08 0.99159E-01 
c  r22          0.10852E-01      13   0.58531E-08   0.18421E-08 0.10094E+00 
c  r33          0.21861E-01      15   0.59000E-08   0.12592E-07 0.12669E+00 
c  r12          0.93873E-03      17   0.67781E-08   0.29624E-09 0.60072E+00 
c  r13          0.46677E-02      19   0.63542E-08   0.15232E-08 0.19957E+00 
c  r23          0.39979E-02      19   0.70011E-08   0.12792E-08 0.19845E+00 
c  epsilon      0.10969E+02      11   0.34245E-08   0.99666E-02 0.16566E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.83919E-02 0.43218E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63324         0.61368       0.0052575       0.0015075
v  Velocity[Y]            -0.57334          0.5441       0.0030807      0.00087325
v  Velocity[Z]              1.5657            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5795            5.44          4.3406          4.3632
v  Pressure                -36.438             360          87.658          169.84
v  r11                    0.001062        0.081978        0.013075        0.018286
v  r22                   0.0011154         0.08261        0.013356        0.018646
v  r33                   0.0016431         0.17429        0.027254        0.037207
v  r12                   -0.010654        0.013593     -0.00023385     -0.00030932
v  r13                   -0.045524        0.052791      9.3288e-05       0.0010138
v  r23                   -0.046706        0.051195      3.0579e-05      0.00057462
v  epsilon                0.069376           271.3          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9956e-05       0.0099176      0.00092522       0.0017428
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2789         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            10922:        0.72808E+02

===============================================================


 INSTANT    0.109230000E-01   TIME STEP NUMBER           10923
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.355786361E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.273526352E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.644394207E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.415470705E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.260040200E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81198E-03   0.45043E-02 0.19858E+01 
c  Velocity[X]                                      0.13822E-03 
c  Velocity[Y]                                      0.12839E-03 
c  Velocity[Z]                                      0.42377E-02 
c  Pressure     0.35865E-04     133   0.91386E-02   0.25297E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54107E-08   0.16241E-08 0.98775E-01 
c  r22          0.10852E-01      13   0.52388E-08   0.18325E-08 0.10124E+00 
c  r33          0.21861E-01      15   0.73912E-08   0.12459E-07 0.12680E+00 
c  r12          0.93873E-03      18   0.49155E-08   0.30004E-09 0.60509E+00 
c  r13          0.46677E-02      19   0.74987E-08   0.15027E-08 0.20015E+00 
c  r23          0.39979E-02      19   0.59241E-08   0.12713E-08 0.19862E+00 
c  epsilon      0.10969E+02      11   0.33681E-08   0.96127E-02 0.16332E+00 
c  TempC        0.25716E+06      16   0.15122E-04   0.84024E-02 0.43215E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63324         0.61369       0.0052574       0.0015075
v  Velocity[Y]            -0.57345         0.54424       0.0030807      0.00087328
v  Velocity[Z]               1.566            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5797            5.44          4.3406          4.3632
v  Pressure                -36.408          360.04          87.647          169.86
v  r11                    0.001062        0.081968        0.013075        0.018286
v  r22                   0.0011154        0.082612        0.013356        0.018646
v  r33                   0.0016431         0.17427        0.027254        0.037207
v  r12                   -0.010657        0.013592     -0.00023385     -0.00030932
v  r13                   -0.045523        0.052789      9.3289e-05       0.0010138
v  r23                   -0.046706        0.051185       3.058e-05      0.00057462
v  epsilon                0.069377          271.25          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9963e-05       0.0099176      0.00092522       0.0017428
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2789         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            10923:        0.70295E+02

===============================================================


 INSTANT    0.109240000E-01   TIME STEP NUMBER           10924
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.752298171E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.967716043E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120778338E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.206889354E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.114058848E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81329E-03   0.44884E-02 0.19835E+01 
c  Velocity[X]                                      0.13745E-03 
c  Velocity[Y]                                      0.12725E-03 
c  Velocity[Z]                                      0.42237E-02 
c  Pressure     0.36284E-04     131   0.92341E-02   0.25592E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.49684E-08   0.15953E-08 0.97978E-01 
c  r22          0.10852E-01      13   0.46793E-08   0.18092E-08 0.10048E+00 
c  r33          0.21861E-01      15   0.66827E-08   0.12321E-07 0.12596E+00 
c  r12          0.93873E-03      18   0.51075E-08   0.29496E-09 0.60075E+00 
c  r13          0.46677E-02      18   0.71650E-08   0.15006E-08 0.19935E+00 
c  r23          0.39979E-02      19   0.59780E-08   0.12633E-08 0.19753E+00 
c  epsilon      0.10969E+02      11   0.32839E-08   0.97020E-02 0.16466E+00 
c  TempC        0.25716E+06      16   0.15185E-04   0.84257E-02 0.43301E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63328         0.61367       0.0052574       0.0015074
v  Velocity[Y]            -0.57342         0.54438       0.0030807      0.00087326
v  Velocity[Z]              1.5657            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5795            5.44          4.3406          4.3632
v  Pressure                -36.448          360.05          87.663          169.87
v  r11                    0.001062         0.08197        0.013075        0.018286
v  r22                   0.0011154        0.082613        0.013356        0.018646
v  r33                   0.0016431         0.17428        0.027254        0.037207
v  r12                   -0.010658        0.013594     -0.00023385     -0.00030932
v  r13                   -0.045525         0.05279      9.3289e-05       0.0010138
v  r23                   -0.046705        0.051208       3.058e-05      0.00057462
v  epsilon                0.069378          271.25          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9968e-05       0.0099176      0.00092522       0.0017428
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2788         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71352         0.85284


 TIME FOR THE TIME STEP            10924:        0.75715E+02

===============================================================


 INSTANT    0.109250000E-01   TIME STEP NUMBER           10925
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.219528095E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.189534520E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.254366769E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.459463400E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.230928394E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81144E-03   0.44960E-02 0.19856E+01 
c  Velocity[X]                                      0.13691E-03 
c  Velocity[Y]                                      0.12796E-03 
c  Velocity[Z]                                      0.42311E-02 
c  Pressure     0.36010E-04     131   0.91715E-02   0.25398E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.48051E-08   0.16050E-08 0.98072E-01 
c  r22          0.10852E-01      13   0.45888E-08   0.17954E-08 0.10025E+00 
c  r33          0.21861E-01      15   0.68424E-08   0.12317E-07 0.12566E+00 
c  r12          0.93873E-03      18   0.53171E-08   0.29001E-09 0.59738E+00 
c  r13          0.46677E-02      19   0.56396E-08   0.14929E-08 0.19876E+00 
c  r23          0.39979E-02      19   0.52965E-08   0.12780E-08 0.19720E+00 
c  epsilon      0.10969E+02      11   0.34492E-08   0.97928E-02 0.16468E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.84212E-02 0.43340E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162015


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63333          0.6137       0.0052574       0.0015074
v  Velocity[Y]            -0.57352          0.5442       0.0030806      0.00087322
v  Velocity[Z]              1.5656            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5794            5.44          4.3406          4.3632
v  Pressure                -36.391             360          87.624          169.83
v  r11                    0.001062        0.081969        0.013075        0.018286
v  r22                   0.0011154        0.082614        0.013356        0.018646
v  r33                   0.0016431         0.17429        0.027254        0.037207
v  r12                   -0.010657        0.013589     -0.00023385     -0.00030932
v  r13                   -0.045525        0.052792       9.329e-05       0.0010138
v  r23                   -0.046705        0.051196       3.058e-05      0.00057462
v  epsilon                0.069379          271.29          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9971e-05       0.0099176      0.00092522       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2783         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71352         0.85284


 TIME FOR THE TIME STEP            10925:        0.73016E+02

===============================================================


 INSTANT    0.109260000E-01   TIME STEP NUMBER           10926
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179839048E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123240698E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.241215483E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.404678869E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.261447687E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81370E-03   0.44987E-02 0.19849E+01 
c  Velocity[X]                                      0.13787E-03 
c  Velocity[Y]                                      0.12850E-03 
c  Velocity[Z]                                      0.42323E-02 
c  Pressure     0.35929E-04     132   0.91557E-02   0.25342E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.50353E-08   0.16092E-08 0.97833E-01 
c  r22          0.10852E-01      13   0.47202E-08   0.18002E-08 0.99976E-01 
c  r33          0.21861E-01      15   0.66204E-08   0.12353E-07 0.12534E+00 
c  r12          0.93873E-03      17   0.64400E-08   0.29007E-09 0.59664E+00 
c  r13          0.46677E-02      19   0.56014E-08   0.14857E-08 0.19835E+00 
c  r23          0.39979E-02      19   0.52423E-08   0.12637E-08 0.19607E+00 
c  epsilon      0.10969E+02      11   0.36167E-08   0.97923E-02 0.16364E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.84300E-02 0.43322E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63322         0.61368       0.0052575       0.0015075
v  Velocity[Y]            -0.57353         0.54436       0.0030807      0.00087323
v  Velocity[Z]              1.5653            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5791            5.44          4.3406          4.3632
v  Pressure                -36.442          359.97          87.628          169.81
v  r11                    0.001062        0.081972        0.013075        0.018286
v  r22                   0.0011154        0.082615        0.013356        0.018646
v  r33                   0.0016431         0.17433        0.027254        0.037207
v  r12                   -0.010659        0.013589     -0.00023385     -0.00030932
v  r13                   -0.045523        0.052794      9.3291e-05       0.0010138
v  r23                   -0.046704        0.051171      3.0581e-05      0.00057462
v  epsilon                 0.06938          271.28          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9974e-05       0.0099176      0.00092522       0.0017428
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2778         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85283


 TIME FOR THE TIME STEP            10926:        0.73447E+02

===============================================================


 INSTANT    0.109270000E-01   TIME STEP NUMBER           10927
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.605251705E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.947969166E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.658044366E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155162015E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.976419484E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81345E-03   0.44793E-02 0.19806E+01 
c  Velocity[X]                                      0.13781E-03 
c  Velocity[Y]                                      0.12797E-03 
c  Velocity[Z]                                      0.42135E-02 
c  Pressure     0.36232E-04     131   0.92330E-02   0.25555E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.51130E-08   0.16443E-08 0.98952E-01 
c  r22          0.10852E-01      13   0.45133E-08   0.18192E-08 0.10045E+00 
c  r33          0.21861E-01      15   0.55804E-08   0.12631E-07 0.12692E+00 
c  r12          0.93873E-03      17   0.69065E-08   0.29530E-09 0.60083E+00 
c  r13          0.46677E-02      19   0.65424E-08   0.15013E-08 0.19914E+00 
c  r23          0.39979E-02      19   0.54668E-08   0.12962E-08 0.19935E+00 
c  epsilon      0.10969E+02      11   0.33947E-08   0.10293E-01 0.17085E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.84016E-02 0.43191E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63323         0.61366       0.0052574       0.0015074
v  Velocity[Y]            -0.57348         0.54427       0.0030807      0.00087326
v  Velocity[Z]              1.5655            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5793            5.44          4.3406          4.3632
v  Pressure                -36.438           360.1          87.671           169.9
v  r11                    0.001062        0.081968        0.013076        0.018286
v  r22                   0.0011154        0.082617        0.013356        0.018646
v  r33                   0.0016431         0.17431        0.027254        0.037207
v  r12                   -0.010659        0.013593     -0.00023385     -0.00030932
v  r13                   -0.045526        0.052794       9.329e-05       0.0010138
v  r23                   -0.046704        0.051159      3.0581e-05      0.00057462
v  epsilon                0.069381           271.3          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9974e-05       0.0099177      0.00092522       0.0017428
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2785         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            10927:        0.72600E+02

===============================================================


 INSTANT    0.109280000E-01   TIME STEP NUMBER           10928
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.351396648E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.577882331E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133340054E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.281610150E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.370235331E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81232E-03   0.45226E-02 0.19921E+01 
c  Velocity[X]                                      0.13758E-03 
c  Velocity[Y]                                      0.12752E-03 
c  Velocity[Z]                                      0.42575E-02 
c  Pressure     0.36261E-04     133   0.92274E-02   0.25576E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.48596E-08   0.16119E-08 0.98446E-01 
c  r22          0.10852E-01      13   0.49860E-08   0.18000E-08 0.10040E+00 
c  r33          0.21861E-01      15   0.64565E-08   0.12396E-07 0.12643E+00 
c  r12          0.93873E-03      18   0.53084E-08   0.29071E-09 0.59868E+00 
c  r13          0.46677E-02      18   0.71593E-08   0.14702E-08 0.19832E+00 
c  r23          0.39979E-02      19   0.61609E-08   0.12744E-08 0.19799E+00 
c  epsilon      0.10969E+02      11   0.34959E-08   0.97266E-02 0.16517E+00 
c  TempC        0.25716E+06      16   0.15186E-04   0.83903E-02 0.43233E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63336         0.61367       0.0052574       0.0015075
v  Velocity[Y]            -0.57336         0.54438       0.0030807      0.00087325
v  Velocity[Z]              1.5657            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5795            5.44          4.3406          4.3632
v  Pressure                -36.468          360.03          87.655          169.86
v  r11                    0.001062        0.081956        0.013076        0.018286
v  r22                   0.0011154        0.082617        0.013356        0.018646
v  r33                   0.0016431         0.17428        0.027254        0.037207
v  r12                   -0.010659        0.013592     -0.00023385     -0.00030932
v  r13                   -0.045524        0.052794       9.329e-05       0.0010138
v  r23                   -0.046704        0.051184      3.0582e-05      0.00057462
v  epsilon                0.069382          271.26          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9974e-05       0.0099179      0.00092522       0.0017428
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2789         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            10928:        0.73811E+02

===============================================================


 INSTANT    0.109290000E-01   TIME STEP NUMBER           10929
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.580179543E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.265106414E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.318746831E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.251718161E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.259875180E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81281E-03   0.45172E-02 0.19901E+01 
c  Velocity[X]                                      0.13833E-03 
c  Velocity[Y]                                      0.12804E-03 
c  Velocity[Z]                                      0.42508E-02 
c  Pressure     0.36179E-04     133   0.92099E-02   0.25519E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57611E-08   0.16065E-08 0.98040E-01 
c  r22          0.10852E-01      13   0.49784E-08   0.18179E-08 0.10040E+00 
c  r33          0.21861E-01      15   0.63130E-08   0.12384E-07 0.12606E+00 
c  r12          0.93873E-03      18   0.50638E-08   0.28743E-09 0.59568E+00 
c  r13          0.46677E-02      19   0.59400E-08   0.14971E-08 0.19927E+00 
c  r23          0.39979E-02      19   0.58023E-08   0.12513E-08 0.19682E+00 
c  epsilon      0.10969E+02      11   0.32997E-08   0.98145E-02 0.16329E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.83773E-02 0.43191E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63327         0.61368       0.0052575       0.0015075
v  Velocity[Y]            -0.57351         0.54413       0.0030807      0.00087324
v  Velocity[Z]              1.5657            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5795            5.44          4.3406          4.3632
v  Pressure                -36.402          360.02          87.633          169.84
v  r11                    0.001062        0.081934        0.013076        0.018286
v  r22                   0.0011154        0.082618        0.013356        0.018646
v  r33                   0.0016431         0.17429        0.027254        0.037207
v  r12                    -0.01066        0.013596     -0.00023385     -0.00030932
v  r13                   -0.045525        0.052795      9.3291e-05       0.0010138
v  r23                   -0.046703        0.051175      3.0583e-05      0.00057463
v  epsilon                0.069383          271.26          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9975e-05       0.0099179      0.00092522       0.0017428
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2791         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71352         0.85284


 TIME FOR THE TIME STEP            10929:        0.72375E+02

===============================================================


 INSTANT    0.109300000E-01   TIME STEP NUMBER           10930
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.360000600E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.260271161E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.915817392E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.308450126E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276729367E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81347E-03   0.44996E-02 0.19861E+01 
c  Velocity[X]                                      0.13681E-03 
c  Velocity[Y]                                      0.12782E-03 
c  Velocity[Z]                                      0.42350E-02 
c  Pressure     0.36242E-04     134   0.92270E-02   0.25563E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57822E-08   0.15957E-08 0.97907E-01 
c  r22          0.10852E-01      13   0.54476E-08   0.17632E-08 0.99634E-01 
c  r33          0.21861E-01      15   0.60255E-08   0.12135E-07 0.12511E+00 
c  r12          0.93873E-03      18   0.50942E-08   0.29084E-09 0.59650E+00 
c  r13          0.46677E-02      20   0.61935E-08   0.14503E-08 0.19737E+00 
c  r23          0.39979E-02      19   0.68498E-08   0.12528E-08 0.19627E+00 
c  epsilon      0.10969E+02      11   0.34080E-08   0.93275E-02 0.16082E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.83510E-02 0.43084E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63335         0.61364       0.0052575       0.0015075
v  Velocity[Y]            -0.57342         0.54422       0.0030806      0.00087324
v  Velocity[Z]              1.5658            5.44          4.3387          4.3625
v  ǁVelocityǁ               1.5796            5.44          4.3406          4.3632
v  Pressure                -36.448          360.02          87.646          169.85
v  r11                    0.001062        0.081909        0.013076        0.018286
v  r22                   0.0011154        0.082619        0.013356        0.018646
v  r33                   0.0016431         0.17431        0.027254        0.037207
v  r12                   -0.010657        0.013594     -0.00023385     -0.00030932
v  r13                   -0.045527        0.052796      9.3291e-05       0.0010138
v  r23                   -0.046704        0.051169      3.0583e-05      0.00057463
v  epsilon                0.069384          271.27          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9973e-05       0.0099179      0.00092522       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2799         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8799         0.71352         0.85285


 TIME FOR THE TIME STEP            10930:        0.73701E+02

===============================================================


 INSTANT    0.109310000E-01   TIME STEP NUMBER           10931
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.236428564E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.311217073E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.180486109E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.143274475E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.889621879E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69775E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81243E-03   0.45187E-02 0.19885E+01 
c  Velocity[X]                                      0.13766E-03 
c  Velocity[Y]                                      0.12835E-03 
c  Velocity[Z]                                      0.42527E-02 
c  Pressure     0.36115E-04     134   0.91971E-02   0.25473E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56017E-08   0.16207E-08 0.98349E-01 
c  r22          0.10852E-01      13   0.52707E-08   0.18336E-08 0.10064E+00 
c  r33          0.21861E-01      15   0.71251E-08   0.12562E-07 0.12616E+00 
c  r12          0.93873E-03      18   0.50909E-08   0.29459E-09 0.59815E+00 
c  r13          0.46677E-02      19   0.67726E-08   0.15014E-08 0.19912E+00 
c  r23          0.39979E-02      19   0.68765E-08   0.12861E-08 0.19788E+00 
c  epsilon      0.10969E+02      11   0.36043E-08   0.10208E-01 0.16576E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.84193E-02 0.43270E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63317         0.61367       0.0052575       0.0015075
v  Velocity[Y]            -0.57364         0.54438       0.0030807      0.00087327
v  Velocity[Z]              1.5657          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4401          4.3406          4.3632
v  Pressure                -36.392          359.96          87.599           169.8
v  r11                    0.001062        0.081893        0.013076        0.018286
v  r22                   0.0011154        0.082619        0.013356        0.018646
v  r33                   0.0016431         0.17428        0.027254        0.037207
v  r12                   -0.010658        0.013599     -0.00023385     -0.00030932
v  r13                   -0.045524        0.052795      9.3291e-05       0.0010138
v  r23                   -0.046704        0.051188      3.0583e-05      0.00057463
v  epsilon                0.069385          271.27          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9973e-05       0.0099178      0.00092523       0.0017428
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017864            5.28         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179            5.88         0.71352         0.85284


 TIME FOR THE TIME STEP            10931:        0.72325E+02

===============================================================


 INSTANT    0.109320000E-01   TIME STEP NUMBER           10932
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.594150167E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.328851235E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127391907E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.245502471E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.258091480E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69774E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81296E-03   0.45050E-02 0.19876E+01 
c  Velocity[X]                                      0.13799E-03 
c  Velocity[Y]                                      0.12903E-03 
c  Velocity[Z]                                      0.42380E-02 
c  Pressure     0.36593E-04     131   0.93090E-02   0.25810E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55490E-08   0.16264E-08 0.98371E-01 
c  r22          0.10852E-01      13   0.54329E-08   0.18557E-08 0.10099E+00 
c  r33          0.21861E-01      16   0.65033E-08   0.12629E-07 0.12676E+00 
c  r12          0.93873E-03      18   0.57929E-08   0.29895E-09 0.59917E+00 
c  r13          0.46677E-02      19   0.69743E-08   0.15376E-08 0.20059E+00 
c  r23          0.39979E-02      20   0.56107E-08   0.12754E-08 0.19738E+00 
c  epsilon      0.10969E+02      11   0.37004E-08   0.10160E-01 0.16776E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.84387E-02 0.43365E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63329         0.61367       0.0052575       0.0015075
v  Velocity[Y]            -0.57364         0.54412       0.0030806      0.00087324
v  Velocity[Z]              1.5654          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4401          4.3406          4.3632
v  Pressure                -36.469          360.05          87.666          169.88
v  r11                    0.001062        0.081883        0.013076        0.018286
v  r22                   0.0011154         0.08262        0.013356        0.018646
v  r33                   0.0016431         0.17426        0.027254        0.037208
v  r12                   -0.010663        0.013595     -0.00023385     -0.00030932
v  r13                   -0.045523        0.052796      9.3292e-05       0.0010138
v  r23                   -0.046703        0.051182      3.0584e-05      0.00057463
v  epsilon                0.069386          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9971e-05       0.0099177      0.00092523       0.0017428
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017863          5.2792         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8792         0.71352         0.85284


 TIME FOR THE TIME STEP            10932:        0.70304E+02

===============================================================


 INSTANT    0.109330000E-01   TIME STEP NUMBER           10933
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209206828E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.729775202E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.293548674E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.332796021E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.295615379E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81288E-03   0.44597E-02 0.19798E+01 
c  Velocity[X]                                      0.13717E-03 
c  Velocity[Y]                                      0.12768E-03 
c  Velocity[Z]                                      0.41948E-02 
c  Pressure     0.36136E-04     133   0.91965E-02   0.25487E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58472E-08   0.16638E-08 0.99450E-01 
c  r22          0.10852E-01      13   0.58629E-08   0.18129E-08 0.10028E+00 
c  r33          0.21861E-01      16   0.63831E-08   0.12559E-07 0.12680E+00 
c  r12          0.93873E-03      18   0.64306E-08   0.29371E-09 0.60142E+00 
c  r13          0.46677E-02      19   0.69539E-08   0.14935E-08 0.19931E+00 
c  r23          0.39979E-02      20   0.55890E-08   0.12955E-08 0.19919E+00 
c  epsilon      0.10969E+02      11   0.36256E-08   0.10440E-01 0.17437E+00 
c  TempC        0.25716E+06      16   0.15124E-04   0.83481E-02 0.43151E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61366       0.0052575       0.0015075
v  Velocity[Y]            -0.57377         0.54406       0.0030807      0.00087325
v  Velocity[Z]              1.5656          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4401          4.3406          4.3632
v  Pressure                -36.413          360.01          87.629          169.84
v  r11                    0.001062        0.081875        0.013076        0.018286
v  r22                   0.0011154        0.082617        0.013356        0.018646
v  r33                   0.0016431         0.17427        0.027254        0.037208
v  r12                   -0.010663        0.013595     -0.00023385     -0.00030932
v  r13                   -0.045527        0.052797      9.3292e-05       0.0010138
v  r23                   -0.046704        0.051173      3.0585e-05      0.00057463
v  epsilon                0.069387          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9969e-05       0.0099176      0.00092523       0.0017428
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017864          5.2783         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71352         0.85284


 TIME FOR THE TIME STEP            10933:        0.69386E+02

===============================================================


 INSTANT    0.109340000E-01   TIME STEP NUMBER           10934
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125752130E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276123577E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.382851933E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.156843858E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171805383E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81249E-03   0.45153E-02 0.19928E+01 
c  Velocity[X]                                      0.13748E-03 
c  Velocity[Y]                                      0.12780E-03 
c  Velocity[Z]                                      0.42500E-02 
c  Pressure     0.36203E-04     133   0.92228E-02   0.25536E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56590E-08   0.16386E-08 0.98420E-01 
c  r22          0.10852E-01      13   0.62183E-08   0.18190E-08 0.10019E+00 
c  r33          0.21861E-01      15   0.73518E-08   0.12556E-07 0.12641E+00 
c  r12          0.93873E-03      18   0.62211E-08   0.29557E-09 0.60034E+00 
c  r13          0.46677E-02      19   0.72977E-08   0.15041E-08 0.19920E+00 
c  r23          0.39979E-02      20   0.55651E-08   0.12849E-08 0.19798E+00 
c  epsilon      0.10969E+02      11   0.34072E-08   0.10081E-01 0.16619E+00 
c  TempC        0.25716E+06      16   0.15169E-04   0.84534E-02 0.43367E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63332         0.61368       0.0052576       0.0015075
v  Velocity[Y]            -0.57372         0.54419       0.0030807      0.00087327
v  Velocity[Z]              1.5653          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4401          4.3406          4.3632
v  Pressure                -36.454             360          87.651          169.84
v  r11                    0.001062        0.081865        0.013076        0.018286
v  r22                   0.0011154        0.082618        0.013356        0.018646
v  r33                   0.0016431         0.17429        0.027254        0.037208
v  r12                   -0.010665        0.013597     -0.00023385     -0.00030932
v  r13                   -0.045523        0.052798      9.3293e-05       0.0010138
v  r23                   -0.046703        0.051193      3.0584e-05      0.00057463
v  epsilon                0.069388          271.27          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9966e-05       0.0099176      0.00092523       0.0017428
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017864          5.2781         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            10934:        0.71814E+02

===============================================================


 INSTANT    0.109350000E-01   TIME STEP NUMBER           10935
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.273293016E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.300585531E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.254339820E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.143471186E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.516967279E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81313E-03   0.45177E-02 0.19903E+01 
c  Velocity[X]                                      0.13825E-03 
c  Velocity[Y]                                      0.12844E-03 
c  Velocity[Z]                                      0.42510E-02 
c  Pressure     0.35985E-04     131   0.91745E-02   0.25382E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.60067E-08   0.16072E-08 0.97979E-01 
c  r22          0.10852E-01      13   0.68067E-08   0.17955E-08 0.10016E+00 
c  r33          0.21861E-01      15   0.66586E-08   0.12268E-07 0.12572E+00 
c  r12          0.93873E-03      18   0.64068E-08   0.29462E-09 0.59974E+00 
c  r13          0.46677E-02      20   0.68551E-08   0.14838E-08 0.19862E+00 
c  r23          0.39979E-02      19   0.71522E-08   0.12710E-08 0.19731E+00 
c  epsilon      0.10969E+02      11   0.33657E-08   0.93752E-02 0.16086E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84950E-02 0.43450E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6333          0.6137       0.0052576       0.0015075
v  Velocity[Y]            -0.57367         0.54436       0.0030807      0.00087329
v  Velocity[Z]              1.5655          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4401          4.3406          4.3632
v  Pressure                -36.413          360.04           87.64          169.85
v  r11                    0.001062        0.081866        0.013076        0.018286
v  r22                   0.0011154        0.082621        0.013356        0.018646
v  r33                   0.0016431         0.17433        0.027254        0.037208
v  r12                   -0.010672        0.013598     -0.00023385     -0.00030932
v  r13                   -0.045523        0.052796      9.3293e-05       0.0010138
v  r23                   -0.046702        0.051186      3.0584e-05      0.00057463
v  epsilon                0.069389          271.26          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9964e-05       0.0099177      0.00092523       0.0017428
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017864          5.2771         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71352         0.85284


 TIME FOR THE TIME STEP            10935:        0.71535E+02

===============================================================


 INSTANT    0.109360000E-01   TIME STEP NUMBER           10936
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106720002E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.343576408E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.398444889E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.308312374E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.308938082E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81387E-03   0.44994E-02 0.19856E+01 
c  Velocity[X]                                      0.13674E-03 
c  Velocity[Y]                                      0.12738E-03 
c  Velocity[Z]                                      0.42353E-02 
c  Pressure     0.36385E-04     131   0.92594E-02   0.25662E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.67716E-08   0.16256E-08 0.98186E-01 
c  r22          0.10852E-01      13   0.65129E-08   0.18357E-08 0.10072E+00 
c  r33          0.21861E-01      15   0.66318E-08   0.12490E-07 0.12592E+00 
c  r12          0.93873E-03      18   0.53540E-08   0.29077E-09 0.59642E+00 
c  r13          0.46677E-02      20   0.74239E-08   0.14816E-08 0.19875E+00 
c  r23          0.39979E-02      19   0.71801E-08   0.12694E-08 0.19633E+00 
c  epsilon      0.10969E+02      11   0.33754E-08   0.10133E-01 0.16748E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.83170E-02 0.43077E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63336         0.61367       0.0052575       0.0015075
v  Velocity[Y]            -0.57342         0.54416       0.0030807      0.00087325
v  Velocity[Z]              1.5656          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4401          4.3406          4.3632
v  Pressure                -36.443          360.02          87.633          169.84
v  r11                    0.001062        0.081862        0.013076        0.018286
v  r22                   0.0011155        0.082621        0.013356        0.018646
v  r33                   0.0016431         0.17431        0.027254        0.037208
v  r12                   -0.010673        0.013605     -0.00023385     -0.00030932
v  r13                   -0.045525        0.052795      9.3293e-05       0.0010138
v  r23                   -0.046701        0.051172      3.0585e-05      0.00057463
v  epsilon                 0.06939          271.27          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.996e-05       0.0099176      0.00092523       0.0017428
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017864          5.2771         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71352         0.85284


 TIME FOR THE TIME STEP            10936:        0.71194E+02

===============================================================


 INSTANT    0.109370000E-01   TIME STEP NUMBER           10937
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.272266727E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.229934645E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.231214275E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.167964285E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.120432186E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81247E-03   0.45133E-02 0.19889E+01 
c  Velocity[X]                                      0.13752E-03 
c  Velocity[Y]                                      0.12773E-03 
c  Velocity[Z]                                      0.42481E-02 
c  Pressure     0.36416E-04     133   0.92686E-02   0.25685E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.71285E-08   0.16461E-08 0.98718E-01 
c  r22          0.10852E-01      13   0.62099E-08   0.18140E-08 0.10027E+00 
c  r33          0.21861E-01      15   0.59179E-08   0.12514E-07 0.12599E+00 
c  r12          0.93873E-03      18   0.53441E-08   0.29375E-09 0.59932E+00 
c  r13          0.46677E-02      20   0.73358E-08   0.14913E-08 0.19855E+00 
c  r23          0.39979E-02      19   0.58913E-08   0.12966E-08 0.19807E+00 
c  epsilon      0.10969E+02      11   0.34428E-08   0.10043E-01 0.16655E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.83948E-02 0.43238E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61369       0.0052575       0.0015075
v  Velocity[Y]            -0.57343         0.54427       0.0030807      0.00087324
v  Velocity[Z]              1.5655          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4401          4.3406          4.3632
v  Pressure                -36.403          360.02          87.647          169.85
v  r11                    0.001062        0.081863        0.013076        0.018286
v  r22                   0.0011155        0.082622        0.013356        0.018646
v  r33                   0.0016431         0.17426        0.027254        0.037208
v  r12                    -0.01067        0.013604     -0.00023385     -0.00030932
v  r13                   -0.045524        0.052796      9.3294e-05       0.0010139
v  r23                     -0.0467          0.0512      3.0585e-05      0.00057463
v  epsilon                0.069391          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9958e-05       0.0099177      0.00092523       0.0017428
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017864          5.2767         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767         0.71352         0.85284


 TIME FOR THE TIME STEP            10937:        0.69911E+02

===============================================================


 INSTANT    0.109380000E-01   TIME STEP NUMBER           10938
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.742433560E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.109471378E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.230733997E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.126888452E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.181941667E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81265E-03   0.45299E-02 0.19928E+01 
c  Velocity[X]                                      0.13865E-03 
c  Velocity[Y]                                      0.12852E-03 
c  Velocity[Z]                                      0.42628E-02 
c  Pressure     0.36261E-04     133   0.92317E-02   0.25576E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.66170E-08   0.16499E-08 0.99234E-01 
c  r22          0.10852E-01      13   0.62372E-08   0.18039E-08 0.10045E+00 
c  r33          0.21861E-01      15   0.61127E-08   0.12426E-07 0.12628E+00 
c  r12          0.93873E-03      18   0.60450E-08   0.29744E-09 0.60109E+00 
c  r13          0.46677E-02      19   0.72084E-08   0.14944E-08 0.19950E+00 
c  r23          0.39979E-02      19   0.56652E-08   0.12783E-08 0.19743E+00 
c  epsilon      0.10969E+02      11   0.33971E-08   0.97174E-02 0.16310E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.84488E-02 0.43309E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63328         0.61368       0.0052576       0.0015075
v  Velocity[Y]            -0.57329         0.54444       0.0030806      0.00087323
v  Velocity[Z]              1.5655          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4401          4.3406          4.3632
v  Pressure                -36.426          360.05          87.672          169.88
v  r11                    0.001062        0.081861        0.013076        0.018286
v  r22                   0.0011155        0.082623        0.013356        0.018646
v  r33                   0.0016431         0.17427        0.027254        0.037208
v  r12                    -0.01067        0.013608     -0.00023385     -0.00030932
v  r13                   -0.045523        0.052796      9.3295e-05       0.0010139
v  r23                   -0.046699        0.051198      3.0586e-05      0.00057463
v  epsilon                0.069392          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9954e-05       0.0099176      0.00092523       0.0017428
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017864           5.277         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71352         0.85284


 TIME FOR THE TIME STEP            10938:        0.70154E+02

===============================================================


 INSTANT    0.109390000E-01   TIME STEP NUMBER           10939
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.185544365E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.378416836E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.347092000E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935018E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.354514335E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.363837216E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81328E-03   0.44462E-02 0.19751E+01 
c  Velocity[X]                                      0.13641E-03 
c  Velocity[Y]                                      0.12782E-03 
c  Velocity[Z]                                      0.41820E-02 
c  Pressure     0.35901E-04     131   0.91378E-02   0.25323E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57452E-08   0.16454E-08 0.98786E-01 
c  r22          0.10852E-01      13   0.56065E-08   0.18139E-08 0.10002E+00 
c  r33          0.21861E-01      15   0.67735E-08   0.12573E-07 0.12652E+00 
c  r12          0.93873E-03      17   0.64728E-08   0.29679E-09 0.60109E+00 
c  r13          0.46677E-02      19   0.60215E-08   0.14875E-08 0.19873E+00 
c  r23          0.39979E-02      19   0.58796E-08   0.13131E-08 0.20037E+00 
c  epsilon      0.10969E+02      11   0.34148E-08   0.10469E-01 0.17191E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.83903E-02 0.43190E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63331         0.61365       0.0052577       0.0015076
v  Velocity[Y]            -0.57347          0.5441       0.0030807      0.00087326
v  Velocity[Z]              1.5652          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4401          4.3406          4.3632
v  Pressure                -36.436          359.96          87.586          169.78
v  r11                    0.001062        0.081864        0.013076        0.018286
v  r22                   0.0011155        0.082622        0.013356        0.018646
v  r33                   0.0016431          0.1743        0.027254        0.037208
v  r12                   -0.010665        0.013612     -0.00023385     -0.00030932
v  r13                   -0.045525        0.052795      9.3295e-05       0.0010139
v  r23                   -0.046697        0.051191      3.0586e-05      0.00057463
v  epsilon                0.069393          271.25          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9953e-05       0.0099175      0.00092523       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017864          5.2772         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85284


 TIME FOR THE TIME STEP            10939:        0.71947E+02

===============================================================


 INSTANT    0.109400000E-01   TIME STEP NUMBER           10940
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.313942305E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.286518969E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934912E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.248372274E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.295255971E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203066701E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81245E-03   0.44984E-02 0.19885E+01 
c  Velocity[X]                                      0.13788E-03 
c  Velocity[Y]                                      0.12787E-03 
c  Velocity[Z]                                      0.42326E-02 
c  Pressure     0.36635E-04     132   0.93246E-02   0.25840E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56264E-08   0.16021E-08 0.97860E-01 
c  r22          0.10852E-01      13   0.57006E-08   0.18095E-08 0.10012E+00 
c  r33          0.21861E-01      15   0.62869E-08   0.12318E-07 0.12553E+00 
c  r12          0.93873E-03      18   0.51197E-08   0.28257E-09 0.59142E+00 
c  r13          0.46677E-02      19   0.54016E-08   0.14966E-08 0.19859E+00 
c  r23          0.39979E-02      19   0.65110E-08   0.12583E-08 0.19659E+00 
c  epsilon      0.10969E+02      11   0.33124E-08   0.98909E-02 0.16590E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.83877E-02 0.43218E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61366       0.0052576       0.0015076
v  Velocity[Y]            -0.57346         0.54411       0.0030807      0.00087324
v  Velocity[Z]              1.5655          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4401          4.3406          4.3632
v  Pressure                -36.455          359.99          87.629          169.82
v  r11                    0.001062        0.081883        0.013076        0.018286
v  r22                   0.0011155        0.082622        0.013356        0.018646
v  r33                   0.0016431         0.17428        0.027254        0.037208
v  r12                    -0.01067        0.013605     -0.00023385     -0.00030932
v  r13                   -0.045522        0.052796      9.3295e-05       0.0010139
v  r23                   -0.046696        0.051215      3.0586e-05      0.00057463
v  epsilon                0.069394          271.29          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05       0.0099175      0.00092523       0.0017428
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017864          5.2768         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71352         0.85284


 TIME FOR THE TIME STEP            10940:        0.70482E+02

===============================================================


 INSTANT    0.109410000E-01   TIME STEP NUMBER           10941
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.502574764E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.304885961E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.379108204E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.320604896E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208817848E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81302E-03   0.45386E-02 0.19947E+01 
c  Velocity[X]                                      0.13865E-03 
c  Velocity[Y]                                      0.12867E-03 
c  Velocity[Z]                                      0.42713E-02 
c  Pressure     0.36336E-04     133   0.92480E-02   0.25629E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56774E-08   0.15878E-08 0.97859E-01 
c  r22          0.10852E-01      13   0.54266E-08   0.17949E-08 0.10027E+00 
c  r33          0.21861E-01      15   0.57987E-08   0.12151E-07 0.12541E+00 
c  r12          0.93874E-03      18   0.50114E-08   0.29252E-09 0.59863E+00 
c  r13          0.46677E-02      19   0.53272E-08   0.14862E-08 0.19912E+00 
c  r23          0.39979E-02      19   0.55204E-08   0.12421E-08 0.19603E+00 
c  epsilon      0.10969E+02      11   0.31588E-08   0.93606E-02 0.16071E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.83785E-02 0.43217E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61368       0.0052575       0.0015075
v  Velocity[Y]            -0.57349         0.54422       0.0030806      0.00087325
v  Velocity[Z]              1.5656          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4401          4.3406          4.3632
v  Pressure                -36.426          360.08          87.674          169.89
v  r11                    0.001062        0.081894        0.013076        0.018286
v  r22                   0.0011155        0.082622        0.013356        0.018646
v  r33                   0.0016431         0.17426        0.027254        0.037208
v  r12                   -0.010669        0.013601     -0.00023385     -0.00030932
v  r13                   -0.045524        0.052795      9.3296e-05       0.0010139
v  r23                   -0.046695        0.051206      3.0587e-05      0.00057463
v  epsilon                0.069395          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05       0.0099176      0.00092523       0.0017428
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017864          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            10941:        0.73625E+02

===============================================================


 INSTANT    0.109420000E-01   TIME STEP NUMBER           10942
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.383794557E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155157178E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119703337E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935014E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.234953939E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.315350713E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81330E-03   0.45130E-02 0.19919E+01 
c  Velocity[X]                                      0.13724E-03 
c  Velocity[Y]                                      0.12852E-03 
c  Velocity[Z]                                      0.42472E-02 
c  Pressure     0.36343E-04     132   0.92490E-02   0.25634E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.57130E-08   0.16374E-08 0.98835E-01 
c  r22          0.10852E-01      13   0.55025E-08   0.18493E-08 0.10139E+00 
c  r33          0.21861E-01      15   0.53144E-08   0.12653E-07 0.12717E+00 
c  r12          0.93874E-03      17   0.67034E-08   0.30220E-09 0.60308E+00 
c  r13          0.46677E-02      18   0.68693E-08   0.14972E-08 0.19969E+00 
c  r23          0.39979E-02      19   0.55596E-08   0.12826E-08 0.19890E+00 
c  epsilon      0.10969E+02      11   0.31788E-08   0.10175E-01 0.16711E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83793E-02 0.43139E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63323         0.61366       0.0052576       0.0015076
v  Velocity[Y]            -0.57352         0.54436       0.0030807      0.00087327
v  Velocity[Z]              1.5654          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4401          4.3406          4.3632
v  Pressure                -36.446          360.05           87.65          169.87
v  r11                    0.001062        0.081896        0.013076        0.018286
v  r22                   0.0011155        0.082622        0.013356        0.018646
v  r33                   0.0016431         0.17426        0.027254        0.037208
v  r12                   -0.010671        0.013599     -0.00023385     -0.00030932
v  r13                   -0.045526        0.052797      9.3295e-05       0.0010139
v  r23                   -0.046695        0.051195      3.0587e-05      0.00057463
v  epsilon                0.069396          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05       0.0099175      0.00092523       0.0017428
v  CourantNb               0.44252             0.6         0.59908         0.59839
v  FourierNb             0.0017864          5.2773         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85283


 TIME FOR THE TIME STEP            10942:        0.74091E+02

===============================================================


 INSTANT    0.109430000E-01   TIME STEP NUMBER           10943
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.611750529E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.359971212E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934918E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.752498809E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.398239063E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.569122227E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81241E-03   0.44791E-02 0.19846E+01 
c  Velocity[X]                                      0.13735E-03 
c  Velocity[Y]                                      0.12745E-03 
c  Velocity[Z]                                      0.42143E-02 
c  Pressure     0.36070E-04     133   0.91816E-02   0.25441E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56019E-08   0.16447E-08 0.98749E-01 
c  r22          0.10852E-01      13   0.54144E-08   0.18255E-08 0.10053E+00 
c  r33          0.21861E-01      15   0.54975E-08   0.12595E-07 0.12658E+00 
c  r12          0.93874E-03      17   0.69444E-08   0.29820E-09 0.60268E+00 
c  r13          0.46677E-02      18   0.72301E-08   0.15023E-08 0.19862E+00 
c  r23          0.39979E-02      19   0.55241E-08   0.12963E-08 0.19866E+00 
c  epsilon      0.10969E+02      11   0.34244E-08   0.10154E-01 0.16701E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.83927E-02 0.43266E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63333         0.61367       0.0052576       0.0015076
v  Velocity[Y]            -0.57348         0.54417       0.0030807      0.00087326
v  Velocity[Z]              1.5656          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4401          4.3406          4.3632
v  Pressure                -36.393          359.98          87.619          169.81
v  r11                    0.001062        0.081906        0.013076        0.018286
v  r22                   0.0011155        0.082618        0.013356        0.018646
v  r33                   0.0016431         0.17427        0.027254        0.037208
v  r12                   -0.010669        0.013599     -0.00023385     -0.00030932
v  r13                   -0.045524        0.052797      9.3296e-05       0.0010139
v  r23                   -0.046694         0.05122      3.0587e-05      0.00057463
v  epsilon                0.069397          271.25          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9951e-05       0.0099175      0.00092523       0.0017428
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017865          5.2777         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71351         0.85283


 TIME FOR THE TIME STEP            10943:        0.72269E+02

===============================================================


 INSTANT    0.109440000E-01   TIME STEP NUMBER           10944
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.402699083E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.132053427E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.709128194E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935014E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.451204483E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.472417579E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81303E-03   0.44819E-02 0.19812E+01 
c  Velocity[X]                                      0.13729E-03 
c  Velocity[Y]                                      0.12711E-03 
c  Velocity[Z]                                      0.42175E-02 
c  Pressure     0.36168E-04     133   0.92083E-02   0.25510E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.58250E-08   0.16200E-08 0.98190E-01 
c  r22          0.10852E-01      13   0.54863E-08   0.18063E-08 0.10011E+00 
c  r33          0.21861E-01      15   0.60518E-08   0.12348E-07 0.12561E+00 
c  r12          0.93874E-03      18   0.52089E-08   0.29656E-09 0.60029E+00 
c  r13          0.46677E-02      19   0.63699E-08   0.14898E-08 0.19819E+00 
c  r23          0.39979E-02      19   0.61210E-08   0.12643E-08 0.19667E+00 
c  epsilon      0.10969E+02      11   0.33615E-08   0.95331E-02 0.16171E+00 
c  TempC        0.25716E+06      16   0.15198E-04   0.84787E-02 0.43432E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61366       0.0052575       0.0015075
v  Velocity[Y]            -0.57333         0.54431       0.0030806      0.00087326
v  Velocity[Z]              1.5658          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4401          4.3406          4.3632
v  Pressure                -36.434          359.98          87.627          169.82
v  r11                    0.001062        0.081907        0.013076        0.018286
v  r22                   0.0011155        0.082619        0.013356        0.018646
v  r33                   0.0016431          0.1743        0.027254        0.037208
v  r12                   -0.010666        0.013596     -0.00023385     -0.00030932
v  r13                   -0.045522        0.052798      9.3296e-05       0.0010139
v  r23                   -0.046694        0.051213      3.0587e-05      0.00057463
v  epsilon                0.069398          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9951e-05       0.0099176      0.00092523       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017864          5.2771         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71352         0.85284


 TIME FOR THE TIME STEP            10944:        0.68036E+02

===============================================================


 INSTANT    0.109450000E-01   TIME STEP NUMBER           10945
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.344728385E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116404772E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.332003332E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.316494054E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127538354E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81298E-03   0.45037E-02 0.19873E+01 
c  Velocity[X]                                      0.13820E-03 
c  Velocity[Y]                                      0.12806E-03 
c  Velocity[Z]                                      0.42375E-02 
c  Pressure     0.36203E-04     131   0.92171E-02   0.25535E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54848E-08   0.16819E-08 0.10051E+00 
c  r22          0.10852E-01      13   0.57684E-08   0.17858E-08 0.99953E-01 
c  r33          0.21861E-01      15   0.58247E-08   0.12527E-07 0.12694E+00 
c  r12          0.93874E-03      18   0.58806E-08   0.30313E-09 0.60905E+00 
c  r13          0.46677E-02      19   0.70312E-08   0.14706E-08 0.19767E+00 
c  r23          0.39979E-02      19   0.60729E-08   0.13164E-08 0.20212E+00 
c  epsilon      0.10969E+02      11   0.34172E-08   0.97805E-02 0.16765E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.83743E-02 0.43152E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61364       0.0052576       0.0015075
v  Velocity[Y]            -0.57344         0.54401       0.0030807      0.00087327
v  Velocity[Z]              1.5658          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4401          4.3406          4.3632
v  Pressure                -36.424          360.05          87.661          169.89
v  r11                    0.001062        0.081909        0.013076        0.018286
v  r22                   0.0011155        0.082621        0.013356        0.018646
v  r33                   0.0016431         0.17427        0.027254        0.037208
v  r12                    -0.01067        0.013599     -0.00023385     -0.00030932
v  r13                   -0.045526        0.052798      9.3296e-05       0.0010139
v  r23                   -0.046694        0.051207      3.0587e-05      0.00057463
v  epsilon                0.069399          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05       0.0099178      0.00092523       0.0017428
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017865          5.2769         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71352         0.85283


 TIME FOR THE TIME STEP            10945:        0.67667E+02

===============================================================


 INSTANT    0.109460000E-01   TIME STEP NUMBER           10946
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.331014519E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140690478E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.361671409E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.121470557E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.684357805E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81346E-03   0.45055E-02 0.19897E+01 
c  Velocity[X]                                      0.13706E-03 
c  Velocity[Y]                                      0.12840E-03 
c  Velocity[Z]                                      0.42401E-02 
c  Pressure     0.36508E-04     133   0.93002E-02   0.25750E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55806E-08   0.16746E-08 0.10007E+00 
c  r22          0.10852E-01      13   0.53317E-08   0.18170E-08 0.10069E+00 
c  r33          0.21861E-01      15   0.57361E-08   0.12570E-07 0.12697E+00 
c  r12          0.93874E-03      18   0.54725E-08   0.30166E-09 0.60833E+00 
c  r13          0.46677E-02      19   0.72549E-08   0.14814E-08 0.19805E+00 
c  r23          0.39979E-02      19   0.68465E-08   0.12859E-08 0.19953E+00 
c  epsilon      0.10969E+02      11   0.33700E-08   0.96503E-02 0.16394E+00 
c  TempC        0.25716E+06      16   0.15175E-04   0.83857E-02 0.43212E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61365       0.0052576       0.0015076
v  Velocity[Y]            -0.57342         0.54406       0.0030805      0.00087321
v  Velocity[Z]              1.5657          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4401          4.3406          4.3632
v  Pressure                -36.453          359.97          87.635          169.82
v  r11                    0.001062          0.0819        0.013076        0.018286
v  r22                   0.0011155        0.082622        0.013356        0.018646
v  r33                   0.0016431         0.17423        0.027254        0.037208
v  r12                    -0.01067        0.013606     -0.00023385     -0.00030932
v  r13                   -0.045523        0.052799      9.3297e-05       0.0010139
v  r23                   -0.046694        0.051196      3.0588e-05      0.00057463
v  epsilon                  0.0694          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05        0.009918      0.00092523       0.0017428
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017865          5.2766         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71352         0.85284


 TIME FOR THE TIME STEP            10946:        0.69595E+02

===============================================================


 INSTANT    0.109470000E-01   TIME STEP NUMBER           10947
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.388898366E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203280280E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.132572465E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.160528339E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.192940858E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81271E-03   0.45259E-02 0.19900E+01 
c  Velocity[X]                                      0.13725E-03 
c  Velocity[Y]                                      0.12883E-03 
c  Velocity[Z]                                      0.42598E-02 
c  Pressure     0.36474E-04     132   0.92837E-02   0.25726E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.55637E-08   0.16104E-08 0.98571E-01 
c  r22          0.10852E-01      13   0.51512E-08   0.17969E-08 0.10040E+00 
c  r33          0.21861E-01      15   0.53769E-08   0.12290E-07 0.12600E+00 
c  r12          0.93874E-03      18   0.58901E-08   0.28870E-09 0.59558E+00 
c  r13          0.46677E-02      20   0.57988E-08   0.14779E-08 0.19852E+00 
c  r23          0.39979E-02      19   0.69252E-08   0.12547E-08 0.19606E+00 
c  epsilon      0.10969E+02      11   0.32574E-08   0.95289E-02 0.16186E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.84288E-02 0.43319E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63331         0.61367       0.0052577       0.0015076
v  Velocity[Y]            -0.57355         0.54418       0.0030806      0.00087323
v  Velocity[Z]              1.5655          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4401          4.3406          4.3632
v  Pressure                -36.407          359.99          87.618          169.82
v  r11                    0.001062        0.081896        0.013076        0.018286
v  r22                   0.0011155        0.082624        0.013356        0.018646
v  r33                   0.0016431         0.17424        0.027254        0.037208
v  r12                   -0.010667        0.013603     -0.00023385     -0.00030932
v  r13                   -0.045522        0.052797      9.3296e-05       0.0010139
v  r23                   -0.046694        0.051221      3.0588e-05      0.00057463
v  epsilon                0.069401          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9957e-05       0.0099181      0.00092524       0.0017428
v  CourantNb               0.44218             0.6         0.59908         0.59839
v  FourierNb             0.0017865          5.2768         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71352         0.85284


 TIME FOR THE TIME STEP            10947:        0.70539E+02

===============================================================


 INSTANT    0.109480000E-01   TIME STEP NUMBER           10948
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.104778841E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.117704521E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179773399E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.847190840E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.212958751E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81309E-03   0.44801E-02 0.19830E+01 
c  Velocity[X]                                      0.13714E-03 
c  Velocity[Y]                                      0.12769E-03 
c  Velocity[Z]                                      0.42153E-02 
c  Pressure     0.36458E-04     132   0.92843E-02   0.25715E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54522E-08   0.16829E-08 0.10053E+00 
c  r22          0.10852E-01      13   0.53854E-08   0.18490E-08 0.10136E+00 
c  r33          0.21861E-01      15   0.64344E-08   0.12766E-07 0.12785E+00 
c  r12          0.93874E-03      18   0.66604E-08   0.30249E-09 0.60565E+00 
c  r13          0.46677E-02      20   0.62861E-08   0.15170E-08 0.20028E+00 
c  r23          0.39979E-02      19   0.71244E-08   0.13101E-08 0.20080E+00 
c  epsilon      0.10969E+02      11   0.35869E-08   0.10042E-01 0.16827E+00 
c  TempC        0.25716E+06      16   0.15164E-04   0.83939E-02 0.43229E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61364       0.0052576       0.0015075
v  Velocity[Y]            -0.57364         0.54432       0.0030806      0.00087323
v  Velocity[Z]              1.5657          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4401          4.3406          4.3632
v  Pressure                -36.461             360           87.64          169.84
v  r11                    0.001062        0.081891        0.013076        0.018286
v  r22                   0.0011155        0.082624        0.013356        0.018646
v  r33                   0.0016431         0.17426        0.027254        0.037208
v  r12                   -0.010666        0.013604     -0.00023385     -0.00030932
v  r13                   -0.045525        0.052797      9.3296e-05       0.0010139
v  r23                   -0.046694         0.05122      3.0589e-05      0.00057463
v  epsilon                0.069402          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9961e-05       0.0099181      0.00092524       0.0017428
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017865          5.2775         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71352         0.85284


 TIME FOR THE TIME STEP            10948:        0.68527E+02

===============================================================


 INSTANT    0.109490000E-01   TIME STEP NUMBER           10949
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.407024761E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.194520435E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934910E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.464644362E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157187462E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226350799E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81254E-03   0.45104E-02 0.19886E+01 
c  Velocity[X]                                      0.13755E-03 
c  Velocity[Y]                                      0.12807E-03 
c  Velocity[Z]                                      0.42448E-02 
c  Pressure     0.36167E-04     131   0.92112E-02   0.25509E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52656E-08   0.16201E-08 0.98334E-01 
c  r22          0.10852E-01      13   0.53879E-08   0.17950E-08 0.99866E-01 
c  r33          0.21861E-01      15   0.52291E-08   0.12359E-07 0.12547E+00 
c  r12          0.93874E-03      18   0.59145E-08   0.29208E-09 0.59917E+00 
c  r13          0.46677E-02      19   0.66640E-08   0.14900E-08 0.19831E+00 
c  r23          0.39979E-02      19   0.71214E-08   0.12869E-08 0.19754E+00 
c  epsilon      0.10969E+02      11   0.34979E-08   0.99828E-02 0.16600E+00 
c  TempC        0.25716E+06      16   0.15187E-04   0.84214E-02 0.43307E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61368       0.0052576       0.0015076
v  Velocity[Y]            -0.57386         0.54414       0.0030806      0.00087321
v  Velocity[Z]              1.5658          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4401          4.3406          4.3632
v  Pressure                -36.405          360.05          87.652          169.86
v  r11                    0.001062        0.081891        0.013076        0.018286
v  r22                   0.0011155        0.082625        0.013356        0.018646
v  r33                   0.0016431         0.17422        0.027254        0.037208
v  r12                   -0.010664        0.013606     -0.00023385     -0.00030932
v  r13                   -0.045524        0.052798      9.3297e-05       0.0010139
v  r23                   -0.046693        0.051208      3.0589e-05      0.00057463
v  epsilon                0.069403          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9966e-05        0.009918      0.00092524       0.0017428
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017865          5.2778         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85283


 TIME FOR THE TIME STEP            10949:        0.67616E+02

===============================================================


 INSTANT    0.109500000E-01   TIME STEP NUMBER           10950
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.572495208E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.350357819E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.299031327E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.247867840E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.314151532E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81311E-03   0.45148E-02 0.19890E+01 
c  Velocity[X]                                      0.13777E-03 
c  Velocity[Y]                                      0.12877E-03 
c  Velocity[Z]                                      0.42482E-02 
c  Pressure     0.35894E-04     131   0.91398E-02   0.25317E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52434E-08   0.16359E-08 0.98952E-01 
c  r22          0.10852E-01      13   0.54920E-08   0.18254E-08 0.10048E+00 
c  r33          0.21861E-01      15   0.54625E-08   0.12475E-07 0.12607E+00 
c  r12          0.93874E-03      18   0.56741E-08   0.29295E-09 0.59824E+00 
c  r13          0.46677E-02      19   0.66788E-08   0.15097E-08 0.19909E+00 
c  r23          0.39979E-02      19   0.72081E-08   0.12732E-08 0.19815E+00 
c  epsilon      0.10969E+02      11   0.35899E-08   0.99655E-02 0.16562E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84197E-02 0.43278E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61365       0.0052576       0.0015075
v  Velocity[Y]            -0.57369         0.54423       0.0030806      0.00087319
v  Velocity[Z]              1.5657          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4401          4.3406          4.3632
v  Pressure                -36.438          360.02          87.646          169.84
v  r11                    0.001062        0.081885        0.013076        0.018286
v  r22                   0.0011155        0.082625        0.013356        0.018646
v  r33                   0.0016431         0.17422        0.027254        0.037208
v  r12                   -0.010664         0.01361     -0.00023385     -0.00030932
v  r13                   -0.045522        0.052798      9.3298e-05       0.0010139
v  r23                   -0.046693        0.051205       3.059e-05      0.00057463
v  epsilon                0.069404          271.13          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.997e-05        0.009918      0.00092524       0.0017428
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017865          5.2785         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            10950:        0.67267E+02

===============================================================


 INSTANT    0.109510000E-01   TIME STEP NUMBER           10951
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.187716317E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.213182170E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.743514276E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935022E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282667970E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226095226E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81347E-03   0.44862E-02 0.19848E+01 
c  Velocity[X]                                      0.13696E-03 
c  Velocity[Y]                                      0.12731E-03 
c  Velocity[Z]                                      0.42219E-02 
c  Pressure     0.36164E-04     131   0.92022E-02   0.25507E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54971E-08   0.16492E-08 0.99375E-01 
c  r22          0.10852E-01      13   0.58415E-08   0.18156E-08 0.10047E+00 
c  r33          0.21861E-01      15   0.55428E-08   0.12604E-07 0.12694E+00 
c  r12          0.93874E-03      18   0.61161E-08   0.29914E-09 0.60531E+00 
c  r13          0.46677E-02      19   0.59036E-08   0.14935E-08 0.19870E+00 
c  r23          0.39979E-02      20   0.55462E-08   0.13115E-08 0.20136E+00 
c  epsilon      0.10969E+02      11   0.34830E-08   0.10419E-01 0.17306E+00 
c  TempC        0.25716E+06      16   0.15125E-04   0.83363E-02 0.43091E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61363       0.0052576       0.0015075
v  Velocity[Y]            -0.57385         0.54436       0.0030806      0.00087323
v  Velocity[Z]              1.5658          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4401          4.3406          4.3632
v  Pressure                -36.391          360.01          87.626          169.84
v  r11                    0.001062        0.081882        0.013076        0.018286
v  r22                   0.0011155        0.082624        0.013356        0.018646
v  r33                   0.0016431         0.17422        0.027254        0.037208
v  r12                   -0.010668        0.013605     -0.00023385     -0.00030932
v  r13                   -0.045524        0.052797      9.3298e-05       0.0010139
v  r23                   -0.046693        0.051239       3.059e-05      0.00057463
v  epsilon                0.069405          271.13          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9975e-05        0.009918      0.00092524       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017865          5.2795         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8795         0.71352         0.85284


 TIME FOR THE TIME STEP            10951:        0.67690E+02

===============================================================


 INSTANT    0.109520000E-01   TIME STEP NUMBER           10952
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.240824513E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.188403808E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934907E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.419902306E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.260302189E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.145803268E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81262E-03   0.45083E-02 0.19890E+01 
c  Velocity[X]                                      0.13805E-03 
c  Velocity[Y]                                      0.12841E-03 
c  Velocity[Z]                                      0.42418E-02 
c  Pressure     0.36221E-04     133   0.92298E-02   0.25547E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.53677E-08   0.16253E-08 0.98954E-01 
c  r22          0.10852E-01      13   0.56387E-08   0.17984E-08 0.10063E+00 
c  r33          0.21861E-01      15   0.69581E-08   0.12345E-07 0.12602E+00 
c  r12          0.93874E-03      18   0.68468E-08   0.29727E-09 0.60417E+00 
c  r13          0.46677E-02      19   0.68784E-08   0.14896E-08 0.19832E+00 
c  r23          0.39979E-02      19   0.72581E-08   0.12830E-08 0.19817E+00 
c  epsilon      0.10969E+02      11   0.34126E-08   0.94986E-02 0.16316E+00 
c  TempC        0.25716E+06      16   0.15166E-04   0.83840E-02 0.43217E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61364       0.0052576       0.0015075
v  Velocity[Y]            -0.57373         0.54425       0.0030805      0.00087319
v  Velocity[Z]              1.5657          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4401          4.3406          4.3632
v  Pressure                -36.456          360.01          87.657          169.85
v  r11                    0.001062        0.081879        0.013076        0.018286
v  r22                   0.0011155        0.082624        0.013356        0.018646
v  r33                   0.0016432         0.17422        0.027254        0.037208
v  r12                   -0.010668        0.013605     -0.00023385     -0.00030932
v  r13                   -0.045522        0.052798      9.3299e-05       0.0010139
v  r23                   -0.046693        0.051234      3.0591e-05      0.00057463
v  epsilon                0.069406          271.14          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9976e-05       0.0099176      0.00092524       0.0017428
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017865          5.2797         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8797         0.71352         0.85284


 TIME FOR THE TIME STEP            10952:        0.69381E+02

===============================================================


 INSTANT    0.109530000E-01   TIME STEP NUMBER           10953
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.249397427E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.184410494E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.190779343E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.925320218E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.308878795E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81270E-03   0.45079E-02 0.19893E+01 
c  Velocity[X]                                      0.13825E-03 
c  Velocity[Y]                                      0.12890E-03 
c  Velocity[Z]                                      0.42407E-02 
c  Pressure     0.36436E-04     133   0.92752E-02   0.25700E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52932E-08   0.16457E-08 0.99505E-01 
c  r22          0.10852E-01      13   0.57928E-08   0.18235E-08 0.10107E+00 
c  r33          0.21861E-01      15   0.67813E-08   0.12494E-07 0.12674E+00 
c  r12          0.93874E-03      18   0.69840E-08   0.29499E-09 0.60422E+00 
c  r13          0.46677E-02      19   0.68640E-08   0.14917E-08 0.19927E+00 
c  r23          0.39979E-02      20   0.55913E-08   0.12780E-08 0.19896E+00 
c  epsilon      0.10969E+02      11   0.33893E-08   0.97796E-02 0.16414E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.84975E-02 0.43498E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61363       0.0052576       0.0015075
v  Velocity[Y]            -0.57366         0.54414       0.0030806      0.00087323
v  Velocity[Z]              1.5655          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4401          4.3406          4.3632
v  Pressure                -36.388          360.03           87.65          169.85
v  r11                    0.001062        0.081881        0.013076        0.018286
v  r22                   0.0011155        0.082623        0.013356        0.018646
v  r33                   0.0016432         0.17424        0.027254        0.037208
v  r12                   -0.010665        0.013605     -0.00023385     -0.00030933
v  r13                   -0.045523        0.052799      9.3299e-05       0.0010139
v  r23                   -0.046692        0.051232      3.0591e-05      0.00057463
v  epsilon                0.069407          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9979e-05       0.0099175      0.00092524       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017866          5.2789         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            10953:        0.69103E+02

===============================================================


 INSTANT    0.109540000E-01   TIME STEP NUMBER           10954
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.176672150E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.516808547E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155190989E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191526361E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.331248453E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81289E-03   0.44952E-02 0.19887E+01 
c  Velocity[X]                                      0.13737E-03 
c  Velocity[Y]                                      0.12774E-03 
c  Velocity[Z]                                      0.42301E-02 
c  Pressure     0.35983E-04     133   0.91603E-02   0.25380E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.52526E-08   0.16480E-08 0.99156E-01 
c  r22          0.10852E-01      13   0.52293E-08   0.18102E-08 0.10053E+00 
c  r33          0.21861E-01      15   0.58009E-08   0.12455E-07 0.12638E+00 
c  r12          0.93874E-03      18   0.55644E-08   0.29538E-09 0.60103E+00 
c  r13          0.46677E-02      19   0.53891E-08   0.14645E-08 0.19803E+00 
c  r23          0.39979E-02      19   0.68688E-08   0.12873E-08 0.19857E+00 
c  epsilon      0.10969E+02      11   0.33592E-08   0.98450E-02 0.16570E+00 
c  TempC        0.25716E+06      16   0.15178E-04   0.83925E-02 0.43188E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61363       0.0052576       0.0015075
v  Velocity[Y]            -0.57358         0.54422       0.0030805       0.0008732
v  Velocity[Z]              1.5654          5.4401          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4401          4.3406          4.3632
v  Pressure                -36.446          360.05          87.661          169.87
v  r11                    0.001062        0.081881        0.013076        0.018286
v  r22                   0.0011155        0.082623        0.013356        0.018646
v  r33                   0.0016432         0.17422        0.027254        0.037208
v  r12                   -0.010663        0.013599     -0.00023385     -0.00030933
v  r13                   -0.045525        0.052802      9.3299e-05       0.0010139
v  r23                   -0.046693        0.051256      3.0591e-05      0.00057463
v  epsilon                0.069408          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9979e-05       0.0099175      0.00092524       0.0017428
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017866          5.2786         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            10954:        0.69635E+02

===============================================================


 INSTANT    0.109550000E-01   TIME STEP NUMBER           10955
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173815856E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.957323697E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173314751E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.373645049E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.314148561E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81242E-03   0.44800E-02 0.19822E+01 
c  Velocity[X]                                      0.13636E-03 
c  Velocity[Y]                                      0.12824E-03 
c  Velocity[Z]                                      0.42154E-02 
c  Pressure     0.36065E-04     131   0.91836E-02   0.25437E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56752E-08   0.16405E-08 0.99033E-01 
c  r22          0.10852E-01      13   0.54581E-08   0.18435E-08 0.10092E+00 
c  r33          0.21861E-01      15   0.56817E-08   0.12675E-07 0.12682E+00 
c  r12          0.93874E-03      18   0.58753E-08   0.30016E-09 0.60540E+00 
c  r13          0.46677E-02      19   0.52751E-08   0.15211E-08 0.19925E+00 
c  r23          0.39979E-02      19   0.68902E-08   0.13094E-08 0.20012E+00 
c  epsilon      0.10969E+02      11   0.34793E-08   0.10100E-01 0.16722E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.83887E-02 0.43205E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61367       0.0052575       0.0015075
v  Velocity[Y]            -0.57358         0.54428       0.0030806       0.0008732
v  Velocity[Z]              1.5654          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4402          4.3406          4.3632
v  Pressure                -36.392          360.05          87.673          169.88
v  r11                    0.001062        0.081902        0.013076        0.018286
v  r22                   0.0011155        0.082619        0.013356        0.018646
v  r33                   0.0016432         0.17422        0.027254        0.037208
v  r12                   -0.010664        0.013599     -0.00023385     -0.00030933
v  r13                   -0.045522        0.052802      9.3299e-05       0.0010139
v  r23                   -0.046692        0.051235      3.0591e-05      0.00057463
v  epsilon                0.069409          271.13          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9982e-05       0.0099175      0.00092524       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017866          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            10955:        0.70816E+02

===============================================================


 INSTANT    0.109560000E-01   TIME STEP NUMBER           10956
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.323168473E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.496487790E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.297169147E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.220057922E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.505172618E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81391E-03   0.44915E-02 0.19855E+01 
c  Velocity[X]                                      0.13859E-03 
c  Velocity[Y]                                      0.12839E-03 
c  Velocity[Z]                                      0.42246E-02 
c  Pressure     0.35961E-04     131   0.91511E-02   0.25364E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56737E-08   0.16340E-08 0.98559E-01 
c  r22          0.10852E-01      13   0.52686E-08   0.18236E-08 0.10042E+00 
c  r33          0.21861E-01      15   0.64046E-08   0.12555E-07 0.12619E+00 
c  r12          0.93874E-03      18   0.57413E-08   0.29818E-09 0.60297E+00 
c  r13          0.46677E-02      19   0.58985E-08   0.15130E-08 0.19844E+00 
c  r23          0.39979E-02      20   0.57047E-08   0.12923E-08 0.19873E+00 
c  epsilon      0.10969E+02      11   0.34625E-08   0.99263E-02 0.16377E+00 
c  TempC        0.25716E+06      16   0.15173E-04   0.84055E-02 0.43286E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61367       0.0052576       0.0015075
v  Velocity[Y]            -0.57351         0.54439       0.0030806      0.00087321
v  Velocity[Z]              1.5657          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4402          4.3406          4.3632
v  Pressure                -36.431          360.03          87.665          169.87
v  r11                    0.001062        0.081907        0.013076        0.018287
v  r22                   0.0011155         0.08262        0.013356        0.018646
v  r33                   0.0016432         0.17422        0.027254        0.037208
v  r12                   -0.010673        0.013604     -0.00023385     -0.00030933
v  r13                   -0.045521        0.052801        9.33e-05       0.0010139
v  r23                   -0.046692        0.051221      3.0592e-05      0.00057463
v  epsilon                 0.06941          271.12          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9982e-05       0.0099175      0.00092524       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017866           5.279         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71352         0.85284


 TIME FOR THE TIME STEP            10956:        0.72201E+02

===============================================================


 INSTANT    0.109570000E-01   TIME STEP NUMBER           10957
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.341867581E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.228387146E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.306618269E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.580712346E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.215776835E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81257E-03   0.45010E-02 0.19878E+01 
c  Velocity[X]                                      0.13740E-03 
c  Velocity[Y]                                      0.12799E-03 
c  Velocity[Z]                                      0.42356E-02 
c  Pressure     0.36197E-04     133   0.92127E-02   0.25531E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.56509E-08   0.16464E-08 0.99356E-01 
c  r22          0.10852E-01      13   0.52211E-08   0.17962E-08 0.10033E+00 
c  r33          0.21861E-01      15   0.58406E-08   0.12501E-07 0.12671E+00 
c  r12          0.93874E-03      18   0.55699E-08   0.29565E-09 0.60454E+00 
c  r13          0.46677E-02      18   0.67810E-08   0.14805E-08 0.19858E+00 
c  r23          0.39979E-02      19   0.65241E-08   0.13060E-08 0.20083E+00 
c  epsilon      0.10969E+02      11   0.33917E-08   0.99868E-02 0.16982E+00 
c  TempC        0.25716E+06      16   0.15121E-04   0.83708E-02 0.43195E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61364       0.0052576       0.0015075
v  Velocity[Y]            -0.57357         0.54416       0.0030805      0.00087316
v  Velocity[Z]              1.5658          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4402          4.3406          4.3632
v  Pressure                -36.397          359.98          87.608          169.81
v  r11                    0.001062         0.08191        0.013076        0.018287
v  r22                   0.0011155        0.082623        0.013356        0.018646
v  r33                   0.0016432         0.17422        0.027254        0.037208
v  r12                   -0.010666        0.013606     -0.00023385     -0.00030933
v  r13                   -0.045524        0.052801        9.33e-05       0.0010139
v  r23                   -0.046692        0.051249      3.0592e-05      0.00057464
v  epsilon                0.069411          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9984e-05       0.0099174      0.00092524       0.0017428
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017866          5.2787         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85284


 TIME FOR THE TIME STEP            10957:        0.72233E+02

===============================================================


 INSTANT    0.109580000E-01   TIME STEP NUMBER           10958
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.305172409E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.229839094E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934895E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.258240847E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227654867E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.193120701E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81324E-03   0.44964E-02 0.19835E+01 
c  Velocity[X]                                      0.13704E-03 
c  Velocity[Y]                                      0.12828E-03 
c  Velocity[Z]                                      0.42311E-02 
c  Pressure     0.36120E-04     133   0.91943E-02   0.25477E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54582E-08   0.16186E-08 0.98150E-01 
c  r22          0.10852E-01      13   0.54322E-08   0.18230E-08 0.10057E+00 
c  r33          0.21861E-01      15   0.59774E-08   0.12534E-07 0.12606E+00 
c  r12          0.93874E-03      18   0.61661E-08   0.29359E-09 0.59919E+00 
c  r13          0.46677E-02      19   0.56378E-08   0.15165E-08 0.19962E+00 
c  r23          0.39979E-02      19   0.67963E-08   0.12787E-08 0.19718E+00 
c  epsilon      0.10969E+02      11   0.35370E-08   0.10152E-01 0.16764E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.84315E-02 0.43307E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61367       0.0052576       0.0015076
v  Velocity[Y]            -0.57365         0.54422       0.0030804      0.00087312
v  Velocity[Z]              1.5657          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4402          4.3406          4.3632
v  Pressure                -36.444          360.07          87.696          169.89
v  r11                    0.001062        0.081915        0.013076        0.018287
v  r22                   0.0011155        0.082623        0.013356        0.018647
v  r33                   0.0016432         0.17422        0.027254        0.037208
v  r12                   -0.010664        0.013601     -0.00023385     -0.00030933
v  r13                   -0.045522          0.0528      9.3301e-05       0.0010139
v  r23                   -0.046692         0.05124      3.0593e-05      0.00057464
v  epsilon                0.069412          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9984e-05       0.0099173      0.00092524       0.0017428
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017866          5.2783         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71352         0.85284


 TIME FOR THE TIME STEP            10958:        0.72615E+02

===============================================================


 INSTANT    0.109590000E-01   TIME STEP NUMBER           10959
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.707365245E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.431622108E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.885688360E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.259750381E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.203028063E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81283E-03   0.45229E-02 0.19906E+01 
c  Velocity[X]                                      0.13809E-03 
c  Velocity[Y]                                      0.12851E-03 
c  Velocity[Z]                                      0.42563E-02 
c  Pressure     0.36260E-04     132   0.92271E-02   0.25576E-01 0.00000E+00 
c  r11          0.10585E-01      13   0.54297E-08   0.16306E-08 0.98541E-01 
c  r22          0.10852E-01      13   0.52503E-08   0.18061E-08 0.10027E+00 
c  r33          0.21861E-01      15   0.59889E-08   0.12336E-07 0.12546E+00 
c  r12          0.93874E-03      18   0.51344E-08   0.29940E-09 0.60429E+00 
c  r13          0.46677E-02      19   0.62129E-08   0.14872E-08 0.19843E+00 
c  r23          0.39979E-02      19   0.68862E-08   0.12739E-08 0.19663E+00 
c  epsilon      0.10969E+02      11   0.34792E-08   0.95895E-02 0.16281E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.84915E-02 0.43450E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61367       0.0052576       0.0015076
v  Velocity[Y]            -0.57377         0.54435       0.0030806      0.00087321
v  Velocity[Z]              1.5654          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4402          4.3406          4.3632
v  Pressure                -36.378          360.09          87.676          169.89
v  r11                    0.001062        0.081914        0.013076        0.018287
v  r22                   0.0011155        0.082623        0.013356        0.018647
v  r33                   0.0016432         0.17423        0.027254        0.037208
v  r12                   -0.010662        0.013604     -0.00023385     -0.00030933
v  r13                   -0.045521        0.052799      9.3301e-05       0.0010139
v  r23                   -0.046691        0.051227      3.0593e-05      0.00057464
v  epsilon                0.069413          271.12          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9987e-05       0.0099173      0.00092524       0.0017428
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017866          5.2782         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            10959:        0.71278E+02

===============================================================


 INSTANT    0.109600000E-01   TIME STEP NUMBER           10960
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.339750739E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186420563E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.271301721E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108760649E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229064382E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81304E-03   0.45158E-02 0.19904E+01 
c  Velocity[X]                                      0.13720E-03 
c  Velocity[Y]                                      0.12763E-03 
c  Velocity[Z]                                      0.42510E-02 
c  Pressure     0.36631E-04     133   0.93297E-02   0.25836E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60246E-08   0.16151E-08 0.98198E-01 
c  r22          0.10852E-01      13   0.53355E-08   0.18121E-08 0.10059E+00 
c  r33          0.21861E-01      15   0.63591E-08   0.12419E-07 0.12606E+00 
c  r12          0.93874E-03      18   0.50475E-08   0.29921E-09 0.60560E+00 
c  r13          0.46677E-02      19   0.65387E-08   0.14985E-08 0.19931E+00 
c  r23          0.39979E-02      19   0.59689E-08   0.12834E-08 0.19826E+00 
c  epsilon      0.10969E+02      11   0.32821E-08   0.95899E-02 0.16327E+00 
c  TempC        0.25716E+06      16   0.15172E-04   0.84015E-02 0.43240E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63356         0.61363       0.0052576       0.0015075
v  Velocity[Y]            -0.57366         0.54416       0.0030806      0.00087321
v  Velocity[Z]              1.5652          5.4402          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4402          4.3406          4.3632
v  Pressure                -36.417          360.03          87.637          169.84
v  r11                    0.001062        0.081913        0.013076        0.018287
v  r22                   0.0011155        0.082622        0.013356        0.018647
v  r33                   0.0016432         0.17423        0.027254        0.037208
v  r12                   -0.010659        0.013608     -0.00023385     -0.00030933
v  r13                   -0.045523        0.052799        9.33e-05       0.0010139
v  r23                    -0.04669        0.051236      3.0593e-05      0.00057464
v  epsilon                0.069414          271.14          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9987e-05       0.0099176      0.00092524       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017867          5.2772         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85284


 TIME FOR THE TIME STEP            10960:        0.70625E+02

===============================================================


 INSTANT    0.109610000E-01   TIME STEP NUMBER           10961
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.174654457E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.274594567E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.996257466E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.813672244E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.387609214E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81250E-03   0.45154E-02 0.19893E+01 
c  Velocity[X]                                      0.13726E-03 
c  Velocity[Y]                                      0.12732E-03 
c  Velocity[Z]                                      0.42508E-02 
c  Pressure     0.36020E-04     131   0.91605E-02   0.25407E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.64474E-08   0.16321E-08 0.98199E-01 
c  r22          0.10852E-01      13   0.54302E-08   0.18275E-08 0.10037E+00 
c  r33          0.21861E-01      15   0.52514E-08   0.12573E-07 0.12587E+00 
c  r12          0.93874E-03      18   0.52600E-08   0.29682E-09 0.60094E+00 
c  r13          0.46677E-02      19   0.60235E-08   0.15148E-08 0.19866E+00 
c  r23          0.39979E-02      19   0.56560E-08   0.13055E-08 0.19864E+00 
c  epsilon      0.10969E+02      11   0.33559E-08   0.10063E-01 0.16524E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.83102E-02 0.43034E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361         0.61372       0.0052577       0.0015076
v  Velocity[Y]            -0.57357         0.54425       0.0030804      0.00087317
v  Velocity[Z]              1.5655          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4402          4.3406          4.3632
v  Pressure                -36.389          360.03          87.644          169.85
v  r11                    0.001062        0.081903        0.013076        0.018287
v  r22                   0.0011155        0.082621        0.013356        0.018647
v  r33                   0.0016432         0.17423        0.027254        0.037208
v  r12                    -0.01066        0.013604     -0.00023385     -0.00030933
v  r13                   -0.045522        0.052801      9.3301e-05       0.0010139
v  r23                   -0.046689        0.051216      3.0594e-05      0.00057464
v  epsilon                0.069415          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9989e-05       0.0099177      0.00092524       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017867          5.2775         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71352         0.85284


 TIME FOR THE TIME STEP            10961:        0.73296E+02

===============================================================


 INSTANT    0.109620000E-01   TIME STEP NUMBER           10962
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.345167815E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.380252028E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.114369387E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.167118900E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.197615770E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81329E-03   0.44889E-02 0.19848E+01 
c  Velocity[X]                                      0.13863E-03 
c  Velocity[Y]                                      0.12841E-03 
c  Velocity[Z]                                      0.42218E-02 
c  Pressure     0.36099E-04     133   0.91834E-02   0.25462E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61103E-08   0.16228E-08 0.98140E-01 
c  r22          0.10852E-01      13   0.54594E-08   0.17860E-08 0.99747E-01 
c  r33          0.21861E-01      15   0.56501E-08   0.12343E-07 0.12544E+00 
c  r12          0.93874E-03      18   0.52261E-08   0.29191E-09 0.59688E+00 
c  r13          0.46677E-02      19   0.56830E-08   0.14909E-08 0.19859E+00 
c  r23          0.39979E-02      19   0.52783E-08   0.12725E-08 0.19690E+00 
c  epsilon      0.10969E+02      11   0.34978E-08   0.96938E-02 0.16363E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.84849E-02 0.43462E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61369       0.0052576       0.0015076
v  Velocity[Y]            -0.57347         0.54429       0.0030805      0.00087321
v  Velocity[Z]              1.5657          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4402          4.3406          4.3632
v  Pressure                -36.433             360           87.64          169.83
v  r11                    0.001062        0.081899        0.013076        0.018287
v  r22                   0.0011155        0.082622        0.013356        0.018647
v  r33                   0.0016432         0.17426        0.027254        0.037208
v  r12                   -0.010662        0.013605     -0.00023385     -0.00030933
v  r13                    -0.04552        0.052803      9.3301e-05       0.0010139
v  r23                   -0.046689        0.051196      3.0594e-05      0.00057464
v  epsilon                0.069416          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9991e-05       0.0099178      0.00092525       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017867          5.2776         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            10962:        0.72072E+02

===============================================================


 INSTANT    0.109630000E-01   TIME STEP NUMBER           10963
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.919611231E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107768257E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.255414428E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.277544166E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.349259839E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81333E-03   0.45104E-02 0.19894E+01 
c  Velocity[X]                                      0.13764E-03 
c  Velocity[Y]                                      0.12877E-03 
c  Velocity[Z]                                      0.42440E-02 
c  Pressure     0.36285E-04     133   0.92403E-02   0.25593E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57507E-08   0.16632E-08 0.99229E-01 
c  r22          0.10852E-01      13   0.52770E-08   0.18324E-08 0.10059E+00 
c  r33          0.21861E-01      15   0.53519E-08   0.12688E-07 0.12704E+00 
c  r12          0.93874E-03      18   0.51692E-08   0.30482E-09 0.60615E+00 
c  r13          0.46677E-02      19   0.55560E-08   0.15116E-08 0.20027E+00 
c  r23          0.39979E-02      19   0.58983E-08   0.13151E-08 0.19993E+00 
c  epsilon      0.10969E+02      11   0.33098E-08   0.10414E-01 0.17301E+00 
c  TempC        0.25716E+06      16   0.15122E-04   0.84053E-02 0.43240E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61366       0.0052577       0.0015076
v  Velocity[Y]            -0.57364         0.54433       0.0030805       0.0008732
v  Velocity[Z]              1.5655          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4402          4.3406          4.3632
v  Pressure                -36.373          360.03          87.653          169.85
v  r11                    0.001062        0.081889        0.013076        0.018287
v  r22                   0.0011155        0.082617        0.013356        0.018647
v  r33                   0.0016432         0.17425        0.027254        0.037208
v  r12                   -0.010661        0.013607     -0.00023385     -0.00030933
v  r13                   -0.045523        0.052802      9.3302e-05       0.0010139
v  r23                   -0.046689        0.051185      3.0594e-05      0.00057464
v  epsilon                0.069417          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9993e-05       0.0099178      0.00092525       0.0017428
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017867          5.2777         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            10963:        0.72993E+02

===============================================================


 INSTANT    0.109640000E-01   TIME STEP NUMBER           10964
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.438194751E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.196647363E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188991407E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.354485270E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.153317985E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81287E-03   0.44856E-02 0.19849E+01 
c  Velocity[X]                                      0.13697E-03 
c  Velocity[Y]                                      0.12838E-03 
c  Velocity[Z]                                      0.42203E-02 
c  Pressure     0.35873E-04     132   0.91355E-02   0.25301E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56311E-08   0.16044E-08 0.97855E-01 
c  r22          0.10852E-01      13   0.52418E-08   0.17834E-08 0.99674E-01 
c  r33          0.21861E-01      15   0.54236E-08   0.12201E-07 0.12496E+00 
c  r12          0.93874E-03      18   0.51908E-08   0.29622E-09 0.59996E+00 
c  r13          0.46677E-02      19   0.53118E-08   0.14766E-08 0.19771E+00 
c  r23          0.39979E-02      19   0.53219E-08   0.12702E-08 0.19668E+00 
c  epsilon      0.10969E+02      10   0.53507E-08   0.94470E-02 0.16223E+00 
c  TempC        0.25716E+06      16   0.15180E-04   0.83910E-02 0.43201E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339          0.6137       0.0052576       0.0015075
v  Velocity[Y]            -0.57356         0.54437       0.0030804      0.00087316
v  Velocity[Z]              1.5655          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4402          4.3406          4.3632
v  Pressure                -36.429          359.97          87.616          169.81
v  r11                    0.001062        0.081882        0.013076        0.018287
v  r22                   0.0011155        0.082617        0.013356        0.018647
v  r33                   0.0016432         0.17423        0.027254        0.037208
v  r12                   -0.010664        0.013609     -0.00023385     -0.00030933
v  r13                    -0.04552        0.052801      9.3303e-05       0.0010139
v  r23                   -0.046689        0.051203      3.0595e-05      0.00057464
v  epsilon                0.069418          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9991e-05       0.0099177      0.00092525       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017867          5.2771         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71352         0.85284


 TIME FOR THE TIME STEP            10964:        0.72386E+02

===============================================================


 INSTANT    0.109650000E-01   TIME STEP NUMBER           10965
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226984390E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.869034562E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.442651662E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.757226045E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.272464770E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81190E-03   0.45041E-02 0.19852E+01 
c  Velocity[X]                                      0.13806E-03 
c  Velocity[Y]                                      0.12769E-03 
c  Velocity[Z]                                      0.42384E-02 
c  Pressure     0.36174E-04     133   0.92041E-02   0.25514E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51135E-08   0.16071E-08 0.98573E-01 
c  r22          0.10852E-01      13   0.51379E-08   0.17956E-08 0.10023E+00 
c  r33          0.21861E-01      15   0.56631E-08   0.12281E-07 0.12601E+00 
c  r12          0.93874E-03      18   0.51952E-08   0.29076E-09 0.60079E+00 
c  r13          0.46677E-02      19   0.71000E-08   0.14829E-08 0.19888E+00 
c  r23          0.39979E-02      19   0.57604E-08   0.12700E-08 0.19868E+00 
c  epsilon      0.10969E+02      11   0.33195E-08   0.95090E-02 0.16247E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.83946E-02 0.43270E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61366       0.0052576       0.0015075
v  Velocity[Y]            -0.57359         0.54422       0.0030805      0.00087318
v  Velocity[Z]              1.5655          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4402          4.3406          4.3632
v  Pressure                -36.411          360.05          87.661          169.87
v  r11                    0.001062         0.08187        0.013076        0.018287
v  r22                   0.0011155        0.082619        0.013356        0.018647
v  r33                   0.0016432         0.17424        0.027254        0.037208
v  r12                   -0.010663        0.013606     -0.00023385     -0.00030933
v  r13                   -0.045521        0.052801      9.3303e-05       0.0010139
v  r23                   -0.046689        0.051198      3.0596e-05      0.00057464
v  epsilon                0.069419          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9988e-05       0.0099179      0.00092525       0.0017428
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017867          5.2765         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765         0.71352         0.85284


 TIME FOR THE TIME STEP            10965:        0.71552E+02

===============================================================


 INSTANT    0.109660000E-01   TIME STEP NUMBER           10966
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.398546776E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.693308444E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.490061439E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.113789662E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.517285008E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81416E-03   0.44990E-02 0.19842E+01 
c  Velocity[X]                                      0.13705E-03 
c  Velocity[Y]                                      0.12690E-03 
c  Velocity[Z]                                      0.42351E-02 
c  Pressure     0.36329E-04     132   0.92439E-02   0.25624E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.49525E-08   0.16523E-08 0.99017E-01 
c  r22          0.10852E-01      13   0.50410E-08   0.18330E-08 0.10068E+00 
c  r33          0.21861E-01      15   0.57551E-08   0.12714E-07 0.12710E+00 
c  r12          0.93874E-03      18   0.52470E-08   0.29640E-09 0.59985E+00 
c  r13          0.46677E-02      19   0.55451E-08   0.15172E-08 0.20055E+00 
c  r23          0.39979E-02      19   0.55404E-08   0.13158E-08 0.20032E+00 
c  epsilon      0.10969E+02      11   0.35072E-08   0.10300E-01 0.16814E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.83391E-02 0.43090E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61363       0.0052576       0.0015075
v  Velocity[Y]            -0.57359         0.54413       0.0030804      0.00087318
v  Velocity[Z]              1.5655          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4402          4.3406          4.3632
v  Pressure                -36.435          360.03          87.652          169.85
v  r11                    0.001062        0.081866        0.013076        0.018287
v  r22                   0.0011155         0.08262        0.013356        0.018647
v  r33                   0.0016432         0.17428        0.027254        0.037208
v  r12                   -0.010663        0.013608     -0.00023385     -0.00030933
v  r13                   -0.045523          0.0528      9.3303e-05       0.0010139
v  r23                    -0.04669        0.051189      3.0596e-05      0.00057464
v  epsilon                 0.06942          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9983e-05       0.0099181      0.00092525       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017867          5.2765         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765         0.71352         0.85284


 TIME FOR THE TIME STEP            10966:        0.71599E+02

===============================================================


 INSTANT    0.109670000E-01   TIME STEP NUMBER           10967
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.769854273E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130286425E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.167745454E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172129296E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.194472377E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81230E-03   0.45069E-02 0.19915E+01 
c  Velocity[X]                                      0.13760E-03 
c  Velocity[Y]                                      0.12905E-03 
c  Velocity[Z]                                      0.42403E-02 
c  Pressure     0.36193E-04     133   0.92141E-02   0.25529E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54098E-08   0.16271E-08 0.98837E-01 
c  r22          0.10852E-01      13   0.54313E-08   0.18260E-08 0.10073E+00 
c  r33          0.21861E-01      15   0.54374E-08   0.12522E-07 0.12675E+00 
c  r12          0.93874E-03      18   0.58689E-08   0.29580E-09 0.60128E+00 
c  r13          0.46677E-02      19   0.53288E-08   0.15127E-08 0.20006E+00 
c  r23          0.39979E-02      19   0.54651E-08   0.12955E-08 0.19989E+00 
c  epsilon      0.10969E+02      11   0.34011E-08   0.10022E-01 0.16640E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.84497E-02 0.43350E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61371       0.0052576       0.0015075
v  Velocity[Y]            -0.57377         0.54418       0.0030805      0.00087323
v  Velocity[Z]              1.5654          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4402          4.3406          4.3632
v  Pressure                -36.348          360.04          87.643          169.86
v  r11                    0.001062        0.081865        0.013076        0.018287
v  r22                   0.0011155         0.08262        0.013356        0.018647
v  r33                   0.0016432         0.17425        0.027254        0.037208
v  r12                   -0.010664        0.013604     -0.00023385     -0.00030933
v  r13                   -0.045521        0.052799      9.3303e-05       0.0010139
v  r23                   -0.046692        0.051206      3.0595e-05      0.00057464
v  epsilon                0.069421          271.26          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9979e-05       0.0099182      0.00092525       0.0017428
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017867          5.2772         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85284


 TIME FOR THE TIME STEP            10967:        0.72220E+02

===============================================================


 INSTANT    0.109680000E-01   TIME STEP NUMBER           10968
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.495530845E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.307714317E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106503015E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.137493725E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117716860E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81294E-03   0.44951E-02 0.19863E+01 
c  Velocity[X]                                      0.13731E-03 
c  Velocity[Y]                                      0.12825E-03 
c  Velocity[Z]                                      0.42296E-02 
c  Pressure     0.36149E-04     133   0.92024E-02   0.25497E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52205E-08   0.16135E-08 0.98457E-01 
c  r22          0.10852E-01      13   0.55550E-08   0.17926E-08 0.10023E+00 
c  r33          0.21861E-01      14   0.69568E-08   0.12364E-07 0.12582E+00 
c  r12          0.93874E-03      18   0.64790E-08   0.29464E-09 0.60009E+00 
c  r13          0.46677E-02      19   0.66312E-08   0.14861E-08 0.19871E+00 
c  r23          0.39979E-02      18   0.70453E-08   0.12800E-08 0.19797E+00 
c  epsilon      0.10969E+02      11   0.33294E-08   0.98582E-02 0.16472E+00 
c  TempC        0.25716E+06      16   0.15182E-04   0.84169E-02 0.43289E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63358         0.61368       0.0052575       0.0015075
v  Velocity[Y]            -0.57378          0.5443       0.0030805      0.00087319
v  Velocity[Z]              1.5653          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4402          4.3406          4.3632
v  Pressure                -36.429             360          87.649          169.84
v  r11                    0.001062        0.081876        0.013076        0.018287
v  r22                   0.0011155         0.08262        0.013356        0.018647
v  r33                   0.0016432         0.17424        0.027254        0.037208
v  r12                   -0.010661        0.013602     -0.00023385     -0.00030933
v  r13                    -0.04552        0.052799      9.3304e-05       0.0010139
v  r23                   -0.046694        0.051195      3.0596e-05      0.00057464
v  epsilon                0.069422          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9973e-05       0.0099183      0.00092525       0.0017428
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017867          5.2777         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            10968:        0.71205E+02

===============================================================


 INSTANT    0.109690000E-01   TIME STEP NUMBER           10969
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.442351844E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.934478988E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.308121639E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141021731E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.203875670E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81316E-03   0.45410E-02 0.19929E+01 
c  Velocity[X]                                      0.13787E-03 
c  Velocity[Y]                                      0.12770E-03 
c  Velocity[Z]                                      0.42754E-02 
c  Pressure     0.36385E-04     133   0.92671E-02   0.25663E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51238E-08   0.16330E-08 0.99193E-01 
c  r22          0.10852E-01      13   0.56162E-08   0.18266E-08 0.10072E+00 
c  r33          0.21861E-01      14   0.70919E-08   0.12603E-07 0.12719E+00 
c  r12          0.93874E-03      18   0.70520E-08   0.29268E-09 0.59883E+00 
c  r13          0.46677E-02      18   0.68069E-08   0.15045E-08 0.19939E+00 
c  r23          0.39979E-02      18   0.70194E-08   0.12885E-08 0.20078E+00 
c  epsilon      0.10969E+02      11   0.32258E-08   0.10288E-01 0.17170E+00 
c  TempC        0.25716E+06      16   0.15165E-04   0.83822E-02 0.43171E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364         0.61367       0.0052576       0.0015075
v  Velocity[Y]             -0.5738         0.54407       0.0030805      0.00087321
v  Velocity[Z]              1.5655          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4402          4.3406          4.3632
v  Pressure                -36.411          360.05           87.66          169.87
v  r11                    0.001062        0.081879        0.013076        0.018287
v  r22                   0.0011155         0.08262        0.013356        0.018647
v  r33                   0.0016432         0.17426        0.027254        0.037208
v  r12                    -0.01066        0.013598     -0.00023385     -0.00030933
v  r13                   -0.045524          0.0528      9.3304e-05       0.0010139
v  r23                   -0.046696        0.051188      3.0596e-05      0.00057464
v  epsilon                0.069423          271.25          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9967e-05       0.0099184      0.00092525       0.0017428
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017868          5.2774         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            10969:        0.67226E+02

===============================================================


 INSTANT    0.109700000E-01   TIME STEP NUMBER           10970
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.380336053E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.528732599E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.416128452E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157005278E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.331906700E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81249E-03   0.45220E-02 0.19910E+01 
c  Velocity[X]                                      0.13695E-03 
c  Velocity[Y]                                      0.12803E-03 
c  Velocity[Z]                                      0.42570E-02 
c  Pressure     0.35934E-04     132   0.91476E-02   0.25346E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.50974E-08   0.16530E-08 0.99367E-01 
c  r22          0.10852E-01      13   0.51722E-08   0.18261E-08 0.10044E+00 
c  r33          0.21861E-01      14   0.70726E-08   0.12650E-07 0.12707E+00 
c  r12          0.93874E-03      18   0.64120E-08   0.29352E-09 0.60087E+00 
c  r13          0.46677E-02      18   0.71417E-08   0.14974E-08 0.19909E+00 
c  r23          0.39979E-02      19   0.53758E-08   0.12987E-08 0.20058E+00 
c  epsilon      0.10969E+02      11   0.33537E-08   0.10275E-01 0.16851E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.84057E-02 0.43218E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344          0.6137       0.0052576       0.0015075
v  Velocity[Y]            -0.57377         0.54418       0.0030804      0.00087316
v  Velocity[Z]              1.5656          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4402          4.3406          4.3632
v  Pressure                -36.418          360.03          87.665          169.86
v  r11                    0.001062        0.081879        0.013076        0.018287
v  r22                   0.0011155         0.08262        0.013356        0.018647
v  r33                   0.0016432         0.17429        0.027254        0.037208
v  r12                   -0.010659        0.013597     -0.00023385     -0.00030933
v  r13                   -0.045521        0.052802      9.3304e-05       0.0010139
v  r23                   -0.046698        0.051215      3.0595e-05      0.00057464
v  epsilon                0.069424          271.28          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.996e-05       0.0099184      0.00092525       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017868          5.2775         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71352         0.85284


 TIME FOR THE TIME STEP            10970:        0.68081E+02

===============================================================


 INSTANT    0.109710000E-01   TIME STEP NUMBER           10971
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154039246E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.312564611E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.424576273E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.270946302E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.501879413E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81358E-03   0.44873E-02 0.19843E+01 
c  Velocity[X]                                      0.13727E-03 
c  Velocity[Y]                                      0.12896E-03 
c  Velocity[Z]                                      0.42210E-02 
c  Pressure     0.36403E-04     131   0.92660E-02   0.25676E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52937E-08   0.16386E-08 0.99094E-01 
c  r22          0.10852E-01      13   0.51198E-08   0.18032E-08 0.10027E+00 
c  r33          0.21861E-01      14   0.70468E-08   0.12371E-07 0.12622E+00 
c  r12          0.93874E-03      18   0.60777E-08   0.28942E-09 0.59906E+00 
c  r13          0.46677E-02      19   0.60677E-08   0.14788E-08 0.19851E+00 
c  r23          0.39979E-02      19   0.53619E-08   0.12730E-08 0.19872E+00 
c  epsilon      0.10969E+02      11   0.33887E-08   0.94903E-02 0.16171E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.84504E-02 0.43382E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61368       0.0052576       0.0015075
v  Velocity[Y]            -0.57387         0.54432       0.0030805       0.0008732
v  Velocity[Z]              1.5655          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4402          4.3406          4.3632
v  Pressure                -36.391          360.03          87.649          169.86
v  r11                    0.001062        0.081879        0.013076        0.018287
v  r22                   0.0011155         0.08262        0.013356        0.018647
v  r33                   0.0016433         0.17433        0.027254        0.037208
v  r12                    -0.01066        0.013598     -0.00023385     -0.00030933
v  r13                    -0.04552        0.052799      9.3305e-05       0.0010139
v  r23                     -0.0467         0.05121      3.0595e-05      0.00057464
v  epsilon                0.069425          271.27          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9957e-05       0.0099184      0.00092525       0.0017428
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017868           5.277         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71352         0.85284


 TIME FOR THE TIME STEP            10971:        0.68373E+02

===============================================================


 INSTANT    0.109720000E-01   TIME STEP NUMBER           10972
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.176717203E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.215436557E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.606347989E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.438716468E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.137572693E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81330E-03   0.45183E-02 0.19896E+01 
c  Velocity[X]                                      0.13735E-03 
c  Velocity[Y]                                      0.12729E-03 
c  Velocity[Z]                                      0.42537E-02 
c  Pressure     0.36384E-04     133   0.92695E-02   0.25663E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52903E-08   0.16477E-08 0.99318E-01 
c  r22          0.10852E-01      13   0.48811E-08   0.18528E-08 0.10113E+00 
c  r33          0.21861E-01      15   0.52572E-08   0.12691E-07 0.12730E+00 
c  r12          0.93875E-03      18   0.61414E-08   0.30140E-09 0.60437E+00 
c  r13          0.46677E-02      19   0.60051E-08   0.15047E-08 0.19963E+00 
c  r23          0.39979E-02      19   0.55479E-08   0.12940E-08 0.20014E+00 
c  epsilon      0.10969E+02      11   0.34193E-08   0.10247E-01 0.16887E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.83723E-02 0.43225E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63354         0.61365       0.0052575       0.0015075
v  Velocity[Y]            -0.57375         0.54412       0.0030804      0.00087316
v  Velocity[Z]              1.5655          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4402          4.3406          4.3632
v  Pressure                -36.419          360.07          87.678          169.89
v  r11                    0.001062        0.081881        0.013076        0.018287
v  r22                   0.0011155        0.082621        0.013356        0.018647
v  r33                   0.0016433         0.17431        0.027254        0.037208
v  r12                   -0.010665        0.013591     -0.00023385     -0.00030933
v  r13                   -0.045522          0.0528      9.3304e-05       0.0010139
v  r23                   -0.046701        0.051206      3.0595e-05      0.00057464
v  epsilon                0.069426           271.3          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099184      0.00092525       0.0017428
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017868          5.2769         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71352         0.85284


 TIME FOR THE TIME STEP            10972:        0.68752E+02

===============================================================


 INSTANT    0.109730000E-01   TIME STEP NUMBER           10973
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.249293015E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.239285331E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.202564033E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.458687972E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.636904324E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81230E-03   0.44999E-02 0.19875E+01 
c  Velocity[X]                                      0.13811E-03 
c  Velocity[Y]                                      0.12720E-03 
c  Velocity[Z]                                      0.42345E-02 
c  Pressure     0.36045E-04     132   0.91787E-02   0.25424E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54801E-08   0.16463E-08 0.99285E-01 
c  r22          0.10852E-01      13   0.53276E-08   0.18211E-08 0.10086E+00 
c  r33          0.21861E-01      15   0.72729E-08   0.12553E-07 0.12702E+00 
c  r12          0.93874E-03      18   0.65827E-08   0.29666E-09 0.60264E+00 
c  r13          0.46677E-02      20   0.58406E-08   0.15043E-08 0.20022E+00 
c  r23          0.39979E-02      19   0.62042E-08   0.12835E-08 0.19899E+00 
c  epsilon      0.10969E+02      11   0.35326E-08   0.99803E-02 0.16652E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83774E-02 0.43215E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63357         0.61372       0.0052575       0.0015075
v  Velocity[Y]            -0.57381         0.54423       0.0030804      0.00087312
v  Velocity[Z]              1.5652          5.4402          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4402          4.3406          4.3632
v  Pressure                -36.384          360.02          87.635          169.84
v  r11                    0.001062         0.08188        0.013076        0.018287
v  r22                   0.0011155        0.082621        0.013356        0.018647
v  r33                   0.0016433         0.17428        0.027254        0.037208
v  r12                   -0.010667         0.01359     -0.00023385     -0.00030933
v  r13                   -0.045522          0.0528      9.3305e-05       0.0010139
v  r23                   -0.046702        0.051232      3.0594e-05      0.00057464
v  epsilon                0.069427          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05        0.009918      0.00092525       0.0017428
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017868          5.2773         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            10973:        0.67178E+02

===============================================================


 INSTANT    0.109740000E-01   TIME STEP NUMBER           10974
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319484132E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.123575071E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.424791045E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.349495876E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.397684992E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81292E-03   0.45147E-02 0.19885E+01 
c  Velocity[X]                                      0.13770E-03 
c  Velocity[Y]                                      0.12908E-03 
c  Velocity[Z]                                      0.42479E-02 
c  Pressure     0.35775E-04     133   0.91026E-02   0.25233E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53694E-08   0.16406E-08 0.99310E-01 
c  r22          0.10852E-01      13   0.51633E-08   0.17932E-08 0.10013E+00 
c  r33          0.21861E-01      15   0.57997E-08   0.12440E-07 0.12657E+00 
c  r12          0.93874E-03      18   0.56717E-08   0.29476E-09 0.60069E+00 
c  r13          0.46677E-02      18   0.70126E-08   0.14767E-08 0.19852E+00 
c  r23          0.39979E-02      19   0.51444E-08   0.12812E-08 0.19884E+00 
c  epsilon      0.10969E+02      11   0.33754E-08   0.97357E-02 0.16514E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.84552E-02 0.43369E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6336          0.6137       0.0052575       0.0015075
v  Velocity[Y]            -0.57386         0.54425       0.0030804      0.00087316
v  Velocity[Z]              1.5653          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4402          4.3406          4.3632
v  Pressure                -36.407          359.99          87.644          169.83
v  r11                    0.001062        0.081889        0.013076        0.018287
v  r22                   0.0011155        0.082617        0.013356        0.018647
v  r33                   0.0016433         0.17429        0.027254        0.037208
v  r12                   -0.010666        0.013589     -0.00023385     -0.00030933
v  r13                    -0.04552        0.052802      9.3305e-05       0.0010139
v  r23                   -0.046703        0.051226      3.0594e-05      0.00057464
v  epsilon                0.069428          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099178      0.00092525       0.0017428
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017868          5.2773         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            10974:        0.68846E+02

===============================================================


 INSTANT    0.109750000E-01   TIME STEP NUMBER           10975
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.189224801E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.349484944E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.887091237E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119982007E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.713480144E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81219E-03   0.45022E-02 0.19887E+01 
c  Velocity[X]                                      0.13698E-03 
c  Velocity[Y]                                      0.12789E-03 
c  Velocity[Z]                                      0.42373E-02 
c  Pressure     0.36378E-04     131   0.92636E-02   0.25658E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55767E-08   0.16537E-08 0.99314E-01 
c  r22          0.10852E-01      13   0.49599E-08   0.18276E-08 0.10063E+00 
c  r33          0.21861E-01      15   0.57605E-08   0.12667E-07 0.12713E+00 
c  r12          0.93875E-03      18   0.56728E-08   0.29414E-09 0.60124E+00 
c  r13          0.46677E-02      19   0.72103E-08   0.14990E-08 0.19938E+00 
c  r23          0.39979E-02      19   0.64807E-08   0.12941E-08 0.20005E+00 
c  epsilon      0.10969E+02      11   0.32999E-08   0.10413E-01 0.17241E+00 
c  TempC        0.25716E+06      16   0.15113E-04   0.84208E-02 0.43215E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61367       0.0052575       0.0015075
v  Velocity[Y]             -0.5738          0.5443       0.0030804      0.00087317
v  Velocity[Z]              1.5652          5.4402          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4402          4.3406          4.3632
v  Pressure                -36.403          360.02          87.634          169.84
v  r11                    0.001062         0.08189        0.013076        0.018287
v  r22                   0.0011155        0.082618        0.013356        0.018647
v  r33                   0.0016433         0.17432        0.027255        0.037208
v  r12                   -0.010664        0.013585     -0.00023385     -0.00030933
v  r13                   -0.045522        0.052801      9.3305e-05       0.0010139
v  r23                   -0.046704        0.051224      3.0594e-05      0.00057464
v  epsilon                0.069429          271.24          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099176      0.00092525       0.0017428
v  CourantNb                0.4422             0.6         0.59908         0.59839
v  FourierNb             0.0017868           5.277         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71352         0.85284


 TIME FOR THE TIME STEP            10975:        0.68124E+02

===============================================================


 INSTANT    0.109760000E-01   TIME STEP NUMBER           10976
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.317266120E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.273195266E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934907E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.868807462E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.402113307E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285084658E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81397E-03   0.45045E-02 0.19867E+01 
c  Velocity[X]                                      0.13652E-03 
c  Velocity[Y]                                      0.12714E-03 
c  Velocity[Z]                                      0.42408E-02 
c  Pressure     0.36315E-04     133   0.92458E-02   0.25614E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57972E-08   0.16117E-08 0.98268E-01 
c  r22          0.10852E-01      13   0.48116E-08   0.18365E-08 0.10082E+00 
c  r33          0.21861E-01      15   0.54998E-08   0.12441E-07 0.12616E+00 
c  r12          0.93875E-03      18   0.59608E-08   0.29552E-09 0.60074E+00 
c  r13          0.46677E-02      19   0.64196E-08   0.14925E-08 0.19912E+00 
c  r23          0.39979E-02      19   0.67990E-08   0.12617E-08 0.19714E+00 
c  epsilon      0.10969E+02      11   0.33270E-08   0.10037E-01 0.16728E+00 
c  TempC        0.25716E+06      16   0.15183E-04   0.83633E-02 0.43177E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63357         0.61372       0.0052575       0.0015075
v  Velocity[Y]            -0.57371         0.54439       0.0030804      0.00087313
v  Velocity[Z]              1.5652          5.4402          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4402          4.3406          4.3632
v  Pressure                -36.472          360.06          87.682          169.89
v  r11                    0.001062        0.081902        0.013076        0.018287
v  r22                   0.0011155        0.082619        0.013356        0.018647
v  r33                   0.0016433         0.17429        0.027255        0.037208
v  r12                   -0.010662        0.013584     -0.00023385     -0.00030933
v  r13                    -0.04552        0.052801      9.3306e-05       0.0010139
v  r23                   -0.046704        0.051249      3.0594e-05      0.00057464
v  epsilon                 0.06943          271.25          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099176      0.00092525       0.0017428
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017869          5.2771         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71352         0.85283


 TIME FOR THE TIME STEP            10976:        0.66711E+02

===============================================================


 INSTANT    0.109770000E-01   TIME STEP NUMBER           10977
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155001358E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.646288431E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.366628099E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.317719858E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319800131E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81158E-03   0.45240E-02 0.19930E+01 
c  Velocity[X]                                      0.13801E-03 
c  Velocity[Y]                                      0.12907E-03 
c  Velocity[Z]                                      0.42570E-02 
c  Pressure     0.36206E-04     133   0.92200E-02   0.25538E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57997E-08   0.16180E-08 0.98353E-01 
c  r22          0.10852E-01      13   0.48699E-08   0.18326E-08 0.10053E+00 
c  r33          0.21861E-01      15   0.53507E-08   0.12491E-07 0.12614E+00 
c  r12          0.93875E-03      18   0.58051E-08   0.28773E-09 0.59713E+00 
c  r13          0.46677E-02      19   0.61436E-08   0.14973E-08 0.19908E+00 
c  r23          0.39979E-02      19   0.71532E-08   0.12689E-08 0.19757E+00 
c  epsilon      0.10969E+02      11   0.33688E-08   0.97925E-02 0.16379E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.84069E-02 0.43285E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61369       0.0052575       0.0015075
v  Velocity[Y]            -0.57377         0.54419       0.0030804      0.00087314
v  Velocity[Z]              1.5654          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4402          4.3406          4.3632
v  Pressure                -36.383          360.06           87.66          169.88
v  r11                    0.001062        0.081909        0.013076        0.018287
v  r22                   0.0011155        0.082621        0.013356        0.018647
v  r33                   0.0016433         0.17427        0.027255        0.037208
v  r12                   -0.010661        0.013582     -0.00023385     -0.00030933
v  r13                    -0.04552        0.052801      9.3306e-05       0.0010139
v  r23                   -0.046705        0.051245      3.0594e-05      0.00057464
v  epsilon                0.069431          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099177      0.00092525       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017869           5.278         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            10977:        0.67127E+02

===============================================================


 INSTANT    0.109780000E-01   TIME STEP NUMBER           10978
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.509593975E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.622417656E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.323791091E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.126456439E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.171076572E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81402E-03   0.45082E-02 0.19878E+01 
c  Velocity[X]                                      0.13690E-03 
c  Velocity[Y]                                      0.12754E-03 
c  Velocity[Z]                                      0.42437E-02 
c  Pressure     0.36334E-04     133   0.92487E-02   0.25627E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58328E-08   0.16353E-08 0.98796E-01 
c  r22          0.10852E-01      13   0.50311E-08   0.18080E-08 0.10035E+00 
c  r33          0.21861E-01      15   0.51646E-08   0.12564E-07 0.12669E+00 
c  r12          0.93875E-03      18   0.58653E-08   0.30066E-09 0.60533E+00 
c  r13          0.46677E-02      19   0.64770E-08   0.14965E-08 0.19956E+00 
c  r23          0.39979E-02      19   0.67435E-08   0.13005E-08 0.19999E+00 
c  epsilon      0.10969E+02      11   0.34338E-08   0.99800E-02 0.16658E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.83460E-02 0.43107E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61365       0.0052574       0.0015074
v  Velocity[Y]            -0.57367          0.5441       0.0030803      0.00087309
v  Velocity[Z]              1.5656          5.4402          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4402          4.3406          4.3632
v  Pressure                -36.444          360.09          87.698           169.9
v  r11                   0.0010621        0.081915        0.013076        0.018287
v  r22                   0.0011155        0.082621        0.013356        0.018647
v  r33                   0.0016433         0.17429        0.027255        0.037208
v  r12                    -0.01066        0.013584     -0.00023385     -0.00030933
v  r13                   -0.045522          0.0528      9.3306e-05       0.0010139
v  r23                   -0.046705        0.051244      3.0594e-05      0.00057464
v  epsilon                0.069432           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.994e-05       0.0099177      0.00092526       0.0017428
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017869          5.2784         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85284


 TIME FOR THE TIME STEP            10978:        0.68575E+02

===============================================================


 INSTANT    0.109790000E-01   TIME STEP NUMBER           10979
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105024716E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.102774394E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.337543709E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935012E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.276555271E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169813085E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81215E-03   0.44835E-02 0.19839E+01 
c  Velocity[X]                                      0.13760E-03 
c  Velocity[Y]                                      0.12804E-03 
c  Velocity[Z]                                      0.42178E-02 
c  Pressure     0.36303E-04     132   0.92407E-02   0.25606E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58536E-08   0.16434E-08 0.99039E-01 
c  r22          0.10852E-01      13   0.50126E-08   0.18138E-08 0.10023E+00 
c  r33          0.21861E-01      15   0.52739E-08   0.12495E-07 0.12629E+00 
c  r12          0.93875E-03      18   0.62911E-08   0.29295E-09 0.59885E+00 
c  r13          0.46677E-02      19   0.69277E-08   0.14826E-08 0.19818E+00 
c  r23          0.39979E-02      19   0.67168E-08   0.12746E-08 0.19786E+00 
c  epsilon      0.10969E+02      11   0.33392E-08   0.10110E-01 0.16732E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.84222E-02 0.43276E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61374       0.0052575       0.0015075
v  Velocity[Y]             -0.5737          0.5442       0.0030803       0.0008731
v  Velocity[Z]              1.5655          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4403          4.3406          4.3632
v  Pressure                -36.374          359.99          87.623          169.81
v  r11                   0.0010621        0.081915        0.013076        0.018287
v  r22                   0.0011155        0.082621        0.013356        0.018647
v  r33                   0.0016433         0.17431        0.027255        0.037208
v  r12                    -0.01066        0.013591     -0.00023385     -0.00030933
v  r13                    -0.04552          0.0528      9.3308e-05       0.0010139
v  r23                   -0.046706        0.051267      3.0595e-05      0.00057464
v  epsilon                0.069433          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099178      0.00092526       0.0017428
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017869          5.2787         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85284


 TIME FOR THE TIME STEP            10979:        0.67364E+02

===============================================================


 INSTANT    0.109800000E-01   TIME STEP NUMBER           10980
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.119030888E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.262792181E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.207239486E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108698743E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.230393739E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81226E-03   0.45091E-02 0.19889E+01 
c  Velocity[X]                                      0.13740E-03 
c  Velocity[Y]                                      0.12872E-03 
c  Velocity[Z]                                      0.42430E-02 
c  Pressure     0.36276E-04     132   0.92399E-02   0.25587E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56875E-08   0.16789E-08 0.10023E+00 
c  r22          0.10852E-01      13   0.49596E-08   0.18545E-08 0.10108E+00 
c  r33          0.21861E-01      14   0.70481E-08   0.12930E-07 0.12845E+00 
c  r12          0.93875E-03      18   0.57850E-08   0.30704E-09 0.61208E+00 
c  r13          0.46677E-02      19   0.59265E-08   0.15408E-08 0.20054E+00 
c  r23          0.39979E-02      19   0.64809E-08   0.13322E-08 0.20257E+00 
c  epsilon      0.10969E+02      11   0.34874E-08   0.10089E-01 0.16803E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.84951E-02 0.43479E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63356         0.61372       0.0052575       0.0015074
v  Velocity[Y]            -0.57358         0.54429       0.0030804      0.00087313
v  Velocity[Z]              1.5656          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4403          4.3406          4.3632
v  Pressure                -36.439          359.99          87.633          169.83
v  r11                   0.0010621        0.081923        0.013076        0.018287
v  r22                   0.0011155        0.082621        0.013356        0.018647
v  r33                   0.0016433         0.17434        0.027255        0.037208
v  r12                   -0.010661        0.013586     -0.00023385     -0.00030933
v  r13                   -0.045518        0.052802      9.3308e-05       0.0010139
v  r23                   -0.046706        0.051255      3.0595e-05      0.00057464
v  epsilon                0.069434          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099177      0.00092526       0.0017428
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017869          5.2789         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            10980:        0.68138E+02

===============================================================


 INSTANT    0.109810000E-01   TIME STEP NUMBER           10981
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.561397038E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.638872586E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.185961678E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.213193041E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.293826566E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81424E-03   0.45116E-02 0.19882E+01 
c  Velocity[X]                                      0.13715E-03 
c  Velocity[Y]                                      0.12781E-03 
c  Velocity[Z]                                      0.42467E-02 
c  Pressure     0.36270E-04     132   0.92327E-02   0.25583E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55973E-08   0.16604E-08 0.99633E-01 
c  r22          0.10852E-01      13   0.51207E-08   0.18291E-08 0.10108E+00 
c  r33          0.21861E-01      15   0.56630E-08   0.12606E-07 0.12740E+00 
c  r12          0.93875E-03      18   0.56163E-08   0.30317E-09 0.60722E+00 
c  r13          0.46678E-02      19   0.63961E-08   0.14904E-08 0.19986E+00 
c  r23          0.39979E-02      20   0.57025E-08   0.12959E-08 0.20028E+00 
c  epsilon      0.10969E+02      11   0.34872E-08   0.98649E-02 0.16620E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.83843E-02 0.43233E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61369       0.0052575       0.0015075
v  Velocity[Y]            -0.57368         0.54435       0.0030804      0.00087312
v  Velocity[Z]              1.5653          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4403          4.3406          4.3632
v  Pressure                -36.422          360.04          87.655          169.87
v  r11                   0.0010621        0.081921        0.013076        0.018287
v  r22                   0.0011155        0.082622        0.013356        0.018647
v  r33                   0.0016433         0.17432        0.027255        0.037208
v  r12                   -0.010665        0.013585     -0.00023385     -0.00030933
v  r13                   -0.045523          0.0528      9.3308e-05       0.0010139
v  r23                   -0.046706        0.051244      3.0595e-05      0.00057464
v  epsilon                0.069435          271.22          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9953e-05       0.0099177      0.00092526       0.0017428
v  CourantNb               0.44219             0.6         0.59908         0.59839
v  FourierNb             0.0017869          5.2784         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85284


 TIME FOR THE TIME STEP            10981:        0.69367E+02

===============================================================


 INSTANT    0.109820000E-01   TIME STEP NUMBER           10982
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.975212494E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.432763849E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.928993323E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.326679134E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.524259318E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81301E-03   0.45080E-02 0.19887E+01 
c  Velocity[X]                                      0.13750E-03 
c  Velocity[Y]                                      0.12785E-03 
c  Velocity[Z]                                      0.42427E-02 
c  Pressure     0.35747E-04     133   0.91001E-02   0.25213E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52210E-08   0.17282E-08 0.10142E+00 
c  r22          0.10852E-01      13   0.54588E-08   0.18588E-08 0.10151E+00 
c  r33          0.21861E-01      15   0.55724E-08   0.13007E-07 0.12917E+00 
c  r12          0.93875E-03      18   0.56888E-08   0.30782E-09 0.61080E+00 
c  r13          0.46678E-02      20   0.60536E-08   0.15124E-08 0.20032E+00 
c  r23          0.39979E-02      20   0.65288E-08   0.13470E-08 0.20511E+00 
c  epsilon      0.10969E+02      11   0.34797E-08   0.10592E-01 0.17507E+00 
c  TempC        0.25716E+06      16   0.15165E-04   0.83395E-02 0.43068E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61374       0.0052575       0.0015075
v  Velocity[Y]            -0.57371         0.54416       0.0030803      0.00087309
v  Velocity[Z]              1.5656          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4403          4.3406          4.3632
v  Pressure                -36.404             360          87.636          169.83
v  r11                   0.0010621        0.081928        0.013076        0.018287
v  r22                   0.0011155        0.082623        0.013356        0.018647
v  r33                   0.0016433         0.17428        0.027255        0.037208
v  r12                   -0.010667        0.013582     -0.00023385     -0.00030933
v  r13                    -0.04552        0.052802      9.3309e-05       0.0010139
v  r23                   -0.046706        0.051266      3.0595e-05      0.00057464
v  epsilon                0.069436          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9954e-05       0.0099176      0.00092526       0.0017428
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017869          5.2769         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71352         0.85284


 TIME FOR THE TIME STEP            10982:        0.66788E+02

===============================================================


 INSTANT    0.109830000E-01   TIME STEP NUMBER           10983
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.257124360E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.422481650E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.165920640E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.451526114E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100065342E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81270E-03   0.45154E-02 0.19885E+01 
c  Velocity[X]                                      0.13880E-03 
c  Velocity[Y]                                      0.12809E-03 
c  Velocity[Z]                                      0.42485E-02 
c  Pressure     0.36583E-04     131   0.93153E-02   0.25803E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55632E-08   0.16262E-08 0.99098E-01 
c  r22          0.10852E-01      13   0.54049E-08   0.18343E-08 0.10131E+00 
c  r33          0.21861E-01      14   0.70674E-08   0.12390E-07 0.12675E+00 
c  r12          0.93875E-03      18   0.58331E-08   0.30386E-09 0.60585E+00 
c  r13          0.46678E-02      19   0.55880E-08   0.14803E-08 0.19924E+00 
c  r23          0.39979E-02      20   0.62641E-08   0.12699E-08 0.19796E+00 
c  epsilon      0.10969E+02      11   0.34958E-08   0.95565E-02 0.16300E+00 
c  TempC        0.25716E+06      16   0.15092E-04   0.84490E-02 0.43378E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61375       0.0052574       0.0015075
v  Velocity[Y]            -0.57378          0.5443       0.0030804      0.00087313
v  Velocity[Z]              1.5655          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4403          4.3406          4.3632
v  Pressure                -36.399          360.07           87.68           169.9
v  r11                   0.0010621        0.081925        0.013076        0.018287
v  r22                   0.0011155        0.082623        0.013356        0.018647
v  r33                   0.0016434         0.17429        0.027255        0.037208
v  r12                   -0.010665        0.013582     -0.00023385     -0.00030933
v  r13                   -0.045519          0.0528       9.331e-05       0.0010139
v  r23                   -0.046705        0.051254      3.0596e-05      0.00057464
v  epsilon                0.069437          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099177      0.00092526       0.0017428
v  CourantNb               0.44217             0.6         0.59908         0.59839
v  FourierNb              0.001787          5.2767         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767         0.71352         0.85284


 TIME FOR THE TIME STEP            10983:        0.66620E+02

===============================================================


 INSTANT    0.109840000E-01   TIME STEP NUMBER           10984
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195206676E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.627497052E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.131735786E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.452916697E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.672078307E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81271E-03   0.45140E-02 0.19897E+01 
c  Velocity[X]                                      0.13670E-03 
c  Velocity[Y]                                      0.12771E-03 
c  Velocity[Z]                                      0.42496E-02 
c  Pressure     0.36333E-04     132   0.92505E-02   0.25627E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.62875E-08   0.16271E-08 0.99196E-01 
c  r22          0.10852E-01      13   0.53125E-08   0.18344E-08 0.10135E+00 
c  r33          0.21861E-01      14   0.72052E-08   0.12508E-07 0.12719E+00 
c  r12          0.93875E-03      18   0.60613E-08   0.29966E-09 0.60742E+00 
c  r13          0.46678E-02      19   0.59721E-08   0.14893E-08 0.19986E+00 
c  r23          0.39979E-02      19   0.68938E-08   0.12750E-08 0.19946E+00 
c  epsilon      0.10969E+02      11   0.35783E-08   0.98052E-02 0.16446E+00 
c  TempC        0.25716E+06      16   0.15187E-04   0.83982E-02 0.43230E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61369       0.0052574       0.0015075
v  Velocity[Y]            -0.57364         0.54398       0.0030803      0.00087306
v  Velocity[Z]              1.5656          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4403          4.3406          4.3632
v  Pressure                -36.426          360.02          87.658          169.86
v  r11                   0.0010621        0.081927        0.013076        0.018287
v  r22                   0.0011155        0.082623        0.013356        0.018647
v  r33                   0.0016434         0.17431        0.027255        0.037208
v  r12                   -0.010663        0.013587     -0.00023385     -0.00030933
v  r13                   -0.045522        0.052799       9.331e-05       0.0010139
v  r23                   -0.046705        0.051244      3.0596e-05      0.00057464
v  epsilon                0.069438           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.996e-05       0.0099178      0.00092526       0.0017428
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb              0.001787          5.2769         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71352         0.85284


 TIME FOR THE TIME STEP            10984:        0.65727E+02

===============================================================


 INSTANT    0.109850000E-01   TIME STEP NUMBER           10985
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.748677408E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.399694017E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.564771464E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.390097577E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138979423E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81184E-03   0.45212E-02 0.19911E+01 
c  Velocity[X]                                      0.13766E-03 
c  Velocity[Y]                                      0.12854E-03 
c  Velocity[Z]                                      0.42550E-02 
c  Pressure     0.36155E-04     131   0.92055E-02   0.25501E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.63842E-08   0.16179E-08 0.98874E-01 
c  r22          0.10852E-01      13   0.55860E-08   0.18379E-08 0.10125E+00 
c  r33          0.21861E-01      15   0.64665E-08   0.12535E-07 0.12698E+00 
c  r12          0.93875E-03      18   0.54772E-08   0.30005E-09 0.60445E+00 
c  r13          0.46678E-02      20   0.68811E-08   0.15322E-08 0.20067E+00 
c  r23          0.39979E-02      19   0.68597E-08   0.12781E-08 0.19862E+00 
c  epsilon      0.10969E+02      11   0.35915E-08   0.98949E-02 0.16488E+00 
c  TempC        0.25716E+06      16   0.15164E-04   0.83965E-02 0.43223E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63358         0.61376       0.0052574       0.0015075
v  Velocity[Y]            -0.57365         0.54404       0.0030803      0.00087305
v  Velocity[Z]              1.5657          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4403          4.3406          4.3632
v  Pressure                -36.365          359.99          87.615          169.82
v  r11                   0.0010621         0.08193        0.013076        0.018287
v  r22                   0.0011155         0.08262        0.013356        0.018647
v  r33                   0.0016434         0.17428        0.027255        0.037208
v  r12                    -0.01066         0.01358     -0.00023385     -0.00030933
v  r13                   -0.045521        0.052801      9.3311e-05       0.0010139
v  r23                   -0.046705        0.051272      3.0597e-05      0.00057464
v  epsilon                0.069439          271.23          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9962e-05       0.0099178      0.00092526       0.0017428
v  CourantNb               0.44219             0.6         0.59908         0.59839
v  FourierNb              0.001787          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            10985:        0.68767E+02

===============================================================


 INSTANT    0.109860000E-01   TIME STEP NUMBER           10986
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.569828401E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.645964264E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125507104E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.527407380E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140485259E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81381E-03   0.45089E-02 0.19872E+01 
c  Velocity[X]                                      0.13766E-03 
c  Velocity[Y]                                      0.12885E-03 
c  Velocity[Z]                                      0.42424E-02 
c  Pressure     0.35979E-04     131   0.91646E-02   0.25377E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.62455E-08   0.16447E-08 0.10019E+00 
c  r22          0.10852E-01      13   0.53354E-08   0.18032E-08 0.10063E+00 
c  r33          0.21861E-01      15   0.53880E-08   0.12388E-07 0.12735E+00 
c  r12          0.93875E-03      18   0.51015E-08   0.29720E-09 0.60466E+00 
c  r13          0.46678E-02      20   0.62288E-08   0.14759E-08 0.19903E+00 
c  r23          0.39979E-02      19   0.66215E-08   0.12697E-08 0.20020E+00 
c  epsilon      0.10969E+02      11   0.33671E-08   0.97477E-02 0.16522E+00 
c  TempC        0.25716E+06      16   0.15164E-04   0.84377E-02 0.43332E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63357         0.61373       0.0052575       0.0015075
v  Velocity[Y]             -0.5736         0.54419       0.0030802      0.00087304
v  Velocity[Z]              1.5654          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4403          4.3406          4.3632
v  Pressure                -36.429          360.02          87.668          169.86
v  r11                   0.0010621        0.081938        0.013076        0.018287
v  r22                   0.0011155        0.082622        0.013356        0.018647
v  r33                   0.0016434         0.17427        0.027255        0.037208
v  r12                   -0.010665        0.013581     -0.00023385     -0.00030933
v  r13                   -0.045519          0.0528      9.3312e-05       0.0010139
v  r23                   -0.046705        0.051252      3.0598e-05      0.00057465
v  epsilon                 0.06944          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9964e-05       0.0099176      0.00092526       0.0017428
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb              0.001787          5.2775         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71352         0.85284


 TIME FOR THE TIME STEP            10986:        0.68980E+02

===============================================================


 INSTANT    0.109870000E-01   TIME STEP NUMBER           10987
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.361977416E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.308496137E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.578758281E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276255291E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.223491183E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81370E-03   0.44845E-02 0.19873E+01 
c  Velocity[X]                                      0.13713E-03 
c  Velocity[Y]                                      0.12846E-03 
c  Velocity[Z]                                      0.42189E-02 
c  Pressure     0.36268E-04     132   0.92282E-02   0.25580E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55854E-08   0.16473E-08 0.99260E-01 
c  r22          0.10852E-01      13   0.53541E-08   0.18246E-08 0.10104E+00 
c  r33          0.21861E-01      15   0.53297E-08   0.12612E-07 0.12742E+00 
c  r12          0.93875E-03      18   0.51435E-08   0.29717E-09 0.60406E+00 
c  r13          0.46678E-02      20   0.66193E-08   0.15025E-08 0.19989E+00 
c  r23          0.39979E-02      19   0.62807E-08   0.12983E-08 0.20008E+00 
c  epsilon      0.10969E+02      11   0.34963E-08   0.10097E-01 0.16689E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.84156E-02 0.43270E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61371       0.0052574       0.0015074
v  Velocity[Y]            -0.57378         0.54433       0.0030802      0.00087301
v  Velocity[Z]              1.5656          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4403          4.3406          4.3632
v  Pressure                -36.373          360.07          87.671          169.89
v  r11                   0.0010621        0.081935        0.013076        0.018287
v  r22                   0.0011156        0.082624        0.013356        0.018647
v  r33                   0.0016434         0.17428        0.027255        0.037208
v  r12                   -0.010669        0.013585     -0.00023385     -0.00030933
v  r13                   -0.045522        0.052797      9.3311e-05       0.0010139
v  r23                   -0.046705        0.051235      3.0598e-05      0.00057465
v  epsilon                0.069441          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9967e-05       0.0099176      0.00092526       0.0017428
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb              0.001787          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            10987:        0.68682E+02

===============================================================


 INSTANT    0.109880000E-01   TIME STEP NUMBER           10988
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209379145E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33841E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.215428711E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33841E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133309648E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33841E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.781016370E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33841E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.305988922E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33841E+00
   Friction velocity        uk    :  0.11558E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81339E-03   0.44914E-02 0.19853E+01 
c  Velocity[X]                                      0.13729E-03 
c  Velocity[Y]                                      0.12743E-03 
c  Velocity[Z]                                      0.42267E-02 
c  Pressure     0.35944E-04     133   0.91528E-02   0.25352E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56892E-08   0.16229E-08 0.99142E-01 
c  r22          0.10852E-01      13   0.55723E-08   0.18045E-08 0.10047E+00 
c  r33          0.21861E-01      14   0.70984E-08   0.12363E-07 0.12669E+00 
c  r12          0.93875E-03      18   0.57406E-08   0.30697E-09 0.60943E+00 
c  r13          0.46678E-02      20   0.64374E-08   0.14971E-08 0.19921E+00 
c  r23          0.39979E-02      19   0.53260E-08   0.12903E-08 0.20028E+00 
c  epsilon      0.10969E+02      11   0.34367E-08   0.98863E-02 0.16897E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.83764E-02 0.43192E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61378       0.0052574       0.0015074
v  Velocity[Y]            -0.57368         0.54416       0.0030802      0.00087301
v  Velocity[Z]              1.5654          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4403          4.3406          4.3632
v  Pressure                -36.426             360          87.629          169.83
v  r11                   0.0010621        0.081936        0.013076        0.018287
v  r22                   0.0011156        0.082623        0.013356        0.018647
v  r33                   0.0016434         0.17431        0.027255        0.037208
v  r12                    -0.01067        0.013584     -0.00023385     -0.00030933
v  r13                    -0.04552        0.052796      9.3312e-05       0.0010139
v  r23                   -0.046706        0.051251      3.0598e-05      0.00057465
v  epsilon                0.069442           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9968e-05       0.0099177      0.00092526       0.0017428
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb              0.001787          5.2791         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71352         0.85284


 TIME FOR THE TIME STEP            10988:        0.67285E+02

===============================================================


 INSTANT    0.109890000E-01   TIME STEP NUMBER           10989
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.749264623E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33841E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.299830926E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33841E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.934291437E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33841E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.218752952E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33841E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119742954E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33841E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81280E-03   0.45233E-02 0.19932E+01 
c  Velocity[X]                                      0.13868E-03 
c  Velocity[Y]                                      0.12735E-03 
c  Velocity[Z]                                      0.42572E-02 
c  Pressure     0.36536E-04     132   0.93006E-02   0.25771E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55744E-08   0.15932E-08 0.98230E-01 
c  r22          0.10852E-01      13   0.53726E-08   0.17806E-08 0.99896E-01 
c  r33          0.21861E-01      15   0.52627E-08   0.12155E-07 0.12551E+00 
c  r12          0.93875E-03      18   0.54808E-08   0.28883E-09 0.59849E+00 
c  r13          0.46678E-02      19   0.75201E-08   0.14610E-08 0.19752E+00 
c  r23          0.39979E-02      19   0.55970E-08   0.12549E-08 0.19662E+00 
c  epsilon      0.10969E+02      11   0.32956E-08   0.94849E-02 0.16227E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84137E-02 0.43300E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61375       0.0052575       0.0015074
v  Velocity[Y]            -0.57383         0.54424       0.0030803      0.00087305
v  Velocity[Z]              1.5657          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4403          4.3406          4.3632
v  Pressure                 -36.41          360.02          87.631          169.84
v  r11                   0.0010621        0.081935        0.013076        0.018287
v  r22                   0.0011156        0.082624        0.013356        0.018647
v  r33                   0.0016434         0.17434        0.027255        0.037208
v  r12                   -0.010668        0.013585     -0.00023385     -0.00030933
v  r13                    -0.04552        0.052797      9.3312e-05       0.0010139
v  r23                   -0.046707        0.051242      3.0599e-05      0.00057465
v  epsilon                0.069443          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9968e-05       0.0099179      0.00092526       0.0017428
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb              0.001787          5.2794         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8794         0.71352         0.85284


 TIME FOR THE TIME STEP            10989:        0.67507E+02

===============================================================


 INSTANT    0.109900000E-01   TIME STEP NUMBER           10990
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.261256702E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.236793409E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.572941559E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115570644E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.295078209E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81285E-03   0.45315E-02 0.19918E+01 
c  Velocity[X]                                      0.13850E-03 
c  Velocity[Y]                                      0.12804E-03 
c  Velocity[Z]                                      0.42650E-02 
c  Pressure     0.36261E-04     133   0.92376E-02   0.25576E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53469E-08   0.16280E-08 0.99235E-01 
c  r22          0.10852E-01      13   0.51695E-08   0.18332E-08 0.10130E+00 
c  r33          0.21861E-01      15   0.53763E-08   0.12511E-07 0.12757E+00 
c  r12          0.93875E-03      18   0.55298E-08   0.29673E-09 0.60361E+00 
c  r13          0.46678E-02      19   0.73131E-08   0.14838E-08 0.19954E+00 
c  r23          0.39979E-02      18   0.68931E-08   0.12654E-08 0.19946E+00 
c  epsilon      0.10969E+02      11   0.31967E-08   0.98922E-02 0.16566E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.83819E-02 0.43173E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61371       0.0052574       0.0015074
v  Velocity[Y]            -0.57358         0.54439       0.0030802        0.000873
v  Velocity[Z]              1.5659          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4403          4.3406          4.3632
v  Pressure                 -36.44          360.05          87.667          169.88
v  r11                   0.0010621        0.081934        0.013076        0.018287
v  r22                   0.0011156        0.082625        0.013356        0.018647
v  r33                   0.0016434         0.17431        0.027255        0.037208
v  r12                   -0.010666        0.013577     -0.00023385     -0.00030933
v  r13                   -0.045522        0.052799      9.3313e-05       0.0010139
v  r23                   -0.046708        0.051226      3.0599e-05      0.00057465
v  epsilon                0.069445          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9966e-05       0.0099179      0.00092526       0.0017428
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb              0.001787           5.279         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71352         0.85284


 TIME FOR THE TIME STEP            10990:        0.66836E+02

===============================================================


 INSTANT    0.109910000E-01   TIME STEP NUMBER           10991
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.331961259E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161391381E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.129696362E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162868475E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.923986572E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81306E-03   0.45056E-02 0.19876E+01 
c  Velocity[X]                                      0.13733E-03 
c  Velocity[Y]                                      0.12805E-03 
c  Velocity[Z]                                      0.42403E-02 
c  Pressure     0.36079E-04     131   0.91907E-02   0.25447E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51995E-08   0.16151E-08 0.98425E-01 
c  r22          0.10852E-01      13   0.47256E-08   0.18221E-08 0.10090E+00 
c  r33          0.21861E-01      15   0.53149E-08   0.12491E-07 0.12661E+00 
c  r12          0.93875E-03      18   0.53349E-08   0.29553E-09 0.60208E+00 
c  r13          0.46678E-02      19   0.69381E-08   0.15048E-08 0.20009E+00 
c  r23          0.39979E-02      18   0.64776E-08   0.12743E-08 0.19756E+00 
c  epsilon      0.10969E+02      11   0.33592E-08   0.99782E-02 0.16543E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.84403E-02 0.43319E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61377       0.0052575       0.0015074
v  Velocity[Y]            -0.57354         0.54422       0.0030802      0.00087302
v  Velocity[Z]              1.5656          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4403          4.3406          4.3632
v  Pressure                -36.386          360.01          87.627          169.84
v  r11                   0.0010621        0.081931        0.013076        0.018287
v  r22                   0.0011156        0.082624        0.013356        0.018647
v  r33                   0.0016434         0.17427        0.027255        0.037208
v  r12                   -0.010666        0.013577     -0.00023385     -0.00030933
v  r13                    -0.04552        0.052798      9.3314e-05       0.0010139
v  r23                   -0.046709        0.051227        3.06e-05      0.00057465
v  epsilon                0.069445          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9964e-05       0.0099181      0.00092526       0.0017428
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017871          5.2791         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71352         0.85283


 TIME FOR THE TIME STEP            10991:        0.66841E+02

===============================================================


 INSTANT    0.109920000E-01   TIME STEP NUMBER           10992
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119034356E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.241868117E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.648043794E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.179809824E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.157713435E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81285E-03   0.44972E-02 0.19869E+01 
c  Velocity[X]                                      0.13701E-03 
c  Velocity[Y]                                      0.12967E-03 
c  Velocity[Z]                                      0.42305E-02 
c  Pressure     0.36143E-04     132   0.91998E-02   0.25493E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55462E-08   0.16742E-08 0.99592E-01 
c  r22          0.10852E-01      13   0.47440E-08   0.18239E-08 0.10085E+00 
c  r33          0.21861E-01      15   0.55923E-08   0.12697E-07 0.12717E+00 
c  r12          0.93875E-03      18   0.55787E-08   0.30030E-09 0.60320E+00 
c  r13          0.46678E-02      19   0.69510E-08   0.14816E-08 0.19870E+00 
c  r23          0.39979E-02      19   0.56001E-08   0.13030E-08 0.19940E+00 
c  epsilon      0.10969E+02      11   0.33478E-08   0.10592E-01 0.17159E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.84142E-02 0.43330E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61375       0.0052574       0.0015074
v  Velocity[Y]             -0.5734         0.54415       0.0030802      0.00087301
v  Velocity[Z]              1.5656          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4403          4.3406          4.3632
v  Pressure                 -36.45          359.95          87.599          169.79
v  r11                   0.0010621        0.081935        0.013076        0.018287
v  r22                   0.0011156        0.082623        0.013356        0.018647
v  r33                   0.0016434         0.17429        0.027255        0.037208
v  r12                    -0.01067        0.013577     -0.00023385     -0.00030933
v  r13                   -0.045519        0.052799      9.3314e-05       0.0010139
v  r23                    -0.04671        0.051255      3.0599e-05      0.00057465
v  epsilon                0.069447          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9961e-05       0.0099182      0.00092526       0.0017428
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb              0.001787          5.2784         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85285


 TIME FOR THE TIME STEP            10992:        0.69201E+02

===============================================================


 INSTANT    0.109930000E-01   TIME STEP NUMBER           10993
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.899032930E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209695762E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.604389860E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.212411441E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.235633443E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81331E-03   0.44775E-02 0.19826E+01 
c  Velocity[X]                                      0.13689E-03 
c  Velocity[Y]                                      0.12727E-03 
c  Velocity[Z]                                      0.42133E-02 
c  Pressure     0.35995E-04     131   0.91685E-02   0.25388E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54397E-08   0.16634E-08 0.99787E-01 
c  r22          0.10852E-01      13   0.48211E-08   0.18371E-08 0.10116E+00 
c  r33          0.21861E-01      14   0.70896E-08   0.12714E-07 0.12749E+00 
c  r12          0.93875E-03      18   0.54572E-08   0.30075E-09 0.60599E+00 
c  r13          0.46678E-02      19   0.56331E-08   0.15242E-08 0.20045E+00 
c  r23          0.39979E-02      19   0.54298E-08   0.13196E-08 0.20120E+00 
c  epsilon      0.10969E+02      11   0.34146E-08   0.10209E-01 0.16796E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.83571E-02 0.43151E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61371       0.0052575       0.0015074
v  Velocity[Y]            -0.57355         0.54421       0.0030802        0.000873
v  Velocity[Z]              1.5655          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4403          4.3406          4.3632
v  Pressure                -36.446          359.98          87.615          169.81
v  r11                   0.0010621        0.081942        0.013076        0.018287
v  r22                   0.0011156        0.082623        0.013356        0.018647
v  r33                   0.0016434         0.17432        0.027255        0.037208
v  r12                    -0.01067         0.01358     -0.00023385     -0.00030933
v  r13                   -0.045523        0.052798      9.3315e-05       0.0010139
v  r23                    -0.04671        0.051255      3.0599e-05      0.00057465
v  epsilon                0.069448          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9957e-05       0.0099179      0.00092526       0.0017428
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017871           5.279         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71352         0.85284


 TIME FOR THE TIME STEP            10993:        0.67431E+02

===============================================================


 INSTANT    0.109940000E-01   TIME STEP NUMBER           10994
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.489071340E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.425032667E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.239502803E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.412677086E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.261130471E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81265E-03   0.45495E-02 0.19987E+01 
c  Velocity[X]                                      0.13769E-03 
c  Velocity[Y]                                      0.12809E-03 
c  Velocity[Z]                                      0.42837E-02 
c  Pressure     0.36278E-04     133   0.92331E-02   0.25588E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55903E-08   0.16117E-08 0.98688E-01 
c  r22          0.10852E-01      13   0.51902E-08   0.17919E-08 0.10038E+00 
c  r33          0.21861E-01      15   0.58122E-08   0.12151E-07 0.12572E+00 
c  r12          0.93875E-03      18   0.53863E-08   0.28954E-09 0.59889E+00 
c  r13          0.46678E-02      18   0.72277E-08   0.14611E-08 0.19812E+00 
c  r23          0.39979E-02      18   0.71166E-08   0.12450E-08 0.19636E+00 
c  epsilon      0.10969E+02      11   0.32907E-08   0.95502E-02 0.16322E+00 
c  TempC        0.25716E+06      16   0.15179E-04   0.84543E-02 0.43307E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61375       0.0052575       0.0015074
v  Velocity[Y]            -0.57341         0.54428       0.0030801      0.00087296
v  Velocity[Z]              1.5656          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4403          4.3406          4.3632
v  Pressure                -36.455          360.03          87.658          169.85
v  r11                   0.0010621         0.08194        0.013076        0.018287
v  r22                   0.0011156        0.082623        0.013356        0.018647
v  r33                   0.0016434          0.1743        0.027255        0.037208
v  r12                   -0.010669        0.013574     -0.00023385     -0.00030933
v  r13                    -0.04552          0.0528      9.3315e-05       0.0010139
v  r23                    -0.04671         0.05125        3.06e-05      0.00057465
v  epsilon                0.069449          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05       0.0099178      0.00092527       0.0017428
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017871          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            10994:        0.68174E+02

===============================================================


 INSTANT    0.109950000E-01   TIME STEP NUMBER           10995
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.275209766E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.837920514E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.167018986E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.170462378E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294759968E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81283E-03   0.45039E-02 0.19853E+01 
c  Velocity[X]                                      0.13699E-03 
c  Velocity[Y]                                      0.12799E-03 
c  Velocity[Z]                                      0.42389E-02 
c  Pressure     0.35941E-04     133   0.91523E-02   0.25350E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53637E-08   0.16437E-08 0.99410E-01 
c  r22          0.10852E-01      13   0.49497E-08   0.18279E-08 0.10088E+00 
c  r33          0.21861E-01      15   0.55707E-08   0.12602E-07 0.12735E+00 
c  r12          0.93875E-03      18   0.50871E-08   0.29305E-09 0.60353E+00 
c  r13          0.46678E-02      18   0.63243E-08   0.14935E-08 0.19958E+00 
c  r23          0.39979E-02      18   0.60925E-08   0.12815E-08 0.19939E+00 
c  epsilon      0.10969E+02      11   0.32921E-08   0.10387E-01 0.17218E+00 
c  TempC        0.25716E+06      16   0.15112E-04   0.84726E-02 0.43399E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63355         0.61375       0.0052575       0.0015074
v  Velocity[Y]            -0.57356          0.5444       0.0030802      0.00087304
v  Velocity[Z]              1.5656          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4403          4.3406          4.3632
v  Pressure                 -36.39          360.03          87.653          169.86
v  r11                   0.0010621        0.081947        0.013076        0.018287
v  r22                   0.0011156        0.082622        0.013356        0.018647
v  r33                   0.0016434         0.17427        0.027255        0.037208
v  r12                   -0.010668        0.013576     -0.00023385     -0.00030933
v  r13                   -0.045519          0.0528      9.3317e-05       0.0010139
v  r23                    -0.04671        0.051265        3.06e-05      0.00057465
v  epsilon                 0.06945          271.14          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099178      0.00092527       0.0017428
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017871          5.2778         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85284


 TIME FOR THE TIME STEP            10995:        0.67632E+02

===============================================================


 INSTANT    0.109960000E-01   TIME STEP NUMBER           10996
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.525580443E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201353847E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.138971029E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935026E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.137182117E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.492518018E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81319E-03   0.44965E-02 0.19866E+01 
c  Velocity[X]                                      0.13776E-03 
c  Velocity[Y]                                      0.12776E-03 
c  Velocity[Z]                                      0.42310E-02 
c  Pressure     0.36453E-04     133   0.92799E-02   0.25712E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55147E-08   0.16323E-08 0.98662E-01 
c  r22          0.10852E-01      13   0.51188E-08   0.18417E-08 0.10098E+00 
c  r33          0.21861E-01      15   0.55596E-08   0.12639E-07 0.12697E+00 
c  r12          0.93875E-03      17   0.68019E-08   0.29381E-09 0.60236E+00 
c  r13          0.46678E-02      18   0.65696E-08   0.15127E-08 0.19957E+00 
c  r23          0.39979E-02      18   0.62738E-08   0.12745E-08 0.19854E+00 
c  epsilon      0.10969E+02      11   0.33750E-08   0.10206E-01 0.16724E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.83160E-02 0.43126E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345          0.6137       0.0052575       0.0015074
v  Velocity[Y]            -0.57343         0.54417       0.0030802        0.000873
v  Velocity[Z]              1.5654          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4403          4.3406          4.3632
v  Pressure                -36.451             360          87.632          169.83
v  r11                   0.0010621        0.081945        0.013076        0.018287
v  r22                   0.0011156        0.082622        0.013356        0.018647
v  r33                   0.0016434         0.17429        0.027255        0.037208
v  r12                   -0.010664        0.013576     -0.00023385     -0.00030933
v  r13                   -0.045521        0.052799      9.3317e-05       0.0010139
v  r23                    -0.04671        0.051257        3.06e-05      0.00057465
v  epsilon                0.069451          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9945e-05       0.0099178      0.00092527       0.0017428
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017871          5.2779         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            10996:        0.68662E+02

===============================================================


 INSTANT    0.109970000E-01   TIME STEP NUMBER           10997
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319549493E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181658259E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.359356889E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276194819E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119955181E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81213E-03   0.45221E-02 0.19913E+01 
c  Velocity[X]                                      0.13780E-03 
c  Velocity[Y]                                      0.12825E-03 
c  Velocity[Z]                                      0.42561E-02 
c  Pressure     0.35994E-04     133   0.91681E-02   0.25388E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59166E-08   0.16299E-08 0.98822E-01 
c  r22          0.10852E-01      13   0.51059E-08   0.18123E-08 0.10062E+00 
c  r33          0.21861E-01      15   0.53963E-08   0.12483E-07 0.12660E+00 
c  r12          0.93875E-03      17   0.69373E-08   0.30545E-09 0.60732E+00 
c  r13          0.46678E-02      19   0.68722E-08   0.14927E-08 0.19931E+00 
c  r23          0.39979E-02      19   0.54168E-08   0.12723E-08 0.19822E+00 
c  epsilon      0.10969E+02      11   0.33268E-08   0.99172E-02 0.16575E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.83964E-02 0.43234E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61376       0.0052575       0.0015075
v  Velocity[Y]             -0.5735         0.54428       0.0030802        0.000873
v  Velocity[Z]              1.5655          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4403          4.3406          4.3632
v  Pressure                 -36.42          360.04          87.638          169.85
v  r11                    0.001062        0.081943        0.013076        0.018287
v  r22                   0.0011156        0.082622        0.013356        0.018647
v  r33                   0.0016434         0.17431        0.027255        0.037208
v  r12                   -0.010663        0.013577     -0.00023386     -0.00030933
v  r13                   -0.045521        0.052801      9.3317e-05       0.0010139
v  r23                    -0.04671        0.051244        3.06e-05      0.00057465
v  epsilon                0.069452          271.19          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099178      0.00092527       0.0017428
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017871          5.2786         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            10997:        0.65728E+02

===============================================================


 INSTANT    0.109980000E-01   TIME STEP NUMBER           10998
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.269856733E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.450672806E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.564796776E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.412758561E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.214165504E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81371E-03   0.45158E-02 0.19890E+01 
c  Velocity[X]                                      0.13686E-03 
c  Velocity[Y]                                      0.12868E-03 
c  Velocity[Z]                                      0.42503E-02 
c  Pressure     0.36063E-04     133   0.91818E-02   0.25436E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56565E-08   0.16416E-08 0.99131E-01 
c  r22          0.10852E-01      13   0.50285E-08   0.18088E-08 0.10025E+00 
c  r33          0.21861E-01      15   0.62491E-08   0.12475E-07 0.12634E+00 
c  r12          0.93875E-03      18   0.48983E-08   0.29975E-09 0.60511E+00 
c  r13          0.46678E-02      19   0.56188E-08   0.14855E-08 0.19863E+00 
c  r23          0.39979E-02      20   0.62503E-08   0.12874E-08 0.19896E+00 
c  epsilon      0.10969E+02      11   0.33933E-08   0.10086E-01 0.16666E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84462E-02 0.43332E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61371       0.0052575       0.0015075
v  Velocity[Y]             -0.5735         0.54398       0.0030802      0.00087299
v  Velocity[Z]              1.5654          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4403          4.3406          4.3632
v  Pressure                -36.447          359.99          87.633          169.82
v  r11                    0.001062        0.081934        0.013076        0.018287
v  r22                   0.0011156        0.082623        0.013356        0.018647
v  r33                   0.0016435         0.17434        0.027255        0.037208
v  r12                   -0.010664        0.013568     -0.00023386     -0.00030933
v  r13                   -0.045519        0.052802      9.3317e-05       0.0010139
v  r23                    -0.04671        0.051239      3.0599e-05      0.00057465
v  epsilon                0.069453          271.21          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05        0.009918      0.00092527       0.0017428
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017871          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            10998:        0.68534E+02

===============================================================


 INSTANT    0.109990000E-01   TIME STEP NUMBER           10999
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208977760E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.259030543E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.311442119E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.606747606E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.137406132E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81306E-03   0.44855E-02 0.19835E+01 
c  Velocity[X]                                      0.13661E-03 
c  Velocity[Y]                                      0.12722E-03 
c  Velocity[Z]                                      0.42216E-02 
c  Pressure     0.36064E-04     131   0.91850E-02   0.25437E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55001E-08   0.16089E-08 0.98022E-01 
c  r22          0.10852E-01      13   0.53481E-08   0.18053E-08 0.10009E+00 
c  r33          0.21861E-01      15   0.65470E-08   0.12298E-07 0.12550E+00 
c  r12          0.93875E-03      18   0.57653E-08   0.29120E-09 0.59869E+00 
c  r13          0.46678E-02      19   0.63965E-08   0.14894E-08 0.19872E+00 
c  r23          0.39979E-02      20   0.62439E-08   0.12640E-08 0.19668E+00 
c  epsilon      0.10969E+02      11   0.35015E-08   0.96783E-02 0.16284E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.83874E-02 0.43200E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61371       0.0052575       0.0015075
v  Velocity[Y]            -0.57355           0.544       0.0030802      0.00087301
v  Velocity[Z]              1.5653          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4403          4.3406          4.3632
v  Pressure                -36.416          360.02          87.639          169.85
v  r11                    0.001062         0.08193        0.013076        0.018287
v  r22                   0.0011156         0.08262        0.013356        0.018647
v  r33                   0.0016435         0.17433        0.027255        0.037208
v  r12                   -0.010662        0.013568     -0.00023386     -0.00030933
v  r13                   -0.045521        0.052803      9.3317e-05       0.0010139
v  r23                   -0.046709        0.051268      3.0599e-05      0.00057465
v  epsilon                0.069454          271.21          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099181      0.00092527       0.0017428
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017871           5.279         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71352         0.85284


 TIME FOR THE TIME STEP            10999:        0.67793E+02

===============================================================


 INSTANT    0.110000000E-01   TIME STEP NUMBER           11000
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.313028182E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123450898E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.291269677E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.278775318E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153925628E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81273E-03   0.44761E-02 0.19818E+01 
c  Velocity[X]                                      0.13659E-03 
c  Velocity[Y]                                      0.12732E-03 
c  Velocity[Z]                                      0.42122E-02 
c  Pressure     0.36353E-04     132   0.92522E-02   0.25641E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60565E-08   0.16363E-08 0.98134E-01 
c  r22          0.10852E-01      13   0.60143E-08   0.18083E-08 0.10010E+00 
c  r33          0.21861E-01      15   0.68228E-08   0.12469E-07 0.12582E+00 
c  r12          0.93875E-03      18   0.62187E-08   0.30276E-09 0.60577E+00 
c  r13          0.46678E-02      19   0.62449E-08   0.14879E-08 0.19810E+00 
c  r23          0.39979E-02      20   0.58603E-08   0.12953E-08 0.19812E+00 
c  epsilon      0.10969E+02      11   0.35280E-08   0.10023E-01 0.16707E+00 
c  TempC        0.25716E+06      16   0.15166E-04   0.83703E-02 0.43175E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61375       0.0052576       0.0015075
v  Velocity[Y]            -0.57348         0.54412       0.0030801      0.00087296
v  Velocity[Z]              1.5654          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4403          4.3406          4.3632
v  Pressure                -36.456          359.98          87.618          169.81
v  r11                    0.001062         0.08193        0.013076        0.018287
v  r22                   0.0011156         0.08262        0.013356        0.018647
v  r33                   0.0016435         0.17429        0.027255        0.037208
v  r12                   -0.010661        0.013571     -0.00023386     -0.00030933
v  r13                   -0.045519        0.052802      9.3317e-05       0.0010139
v  r23                   -0.046709         0.05126        3.06e-05      0.00057465
v  epsilon                0.069455          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099181      0.00092527       0.0017428
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017872          5.2794         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8794         0.71352         0.85284


 TIME FOR THE TIME STEP            11000:        0.68383E+02

===============================================================


 INSTANT    0.110010000E-01   TIME STEP NUMBER           11001
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.732842191E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106331218E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.110014789E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.312806108E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.177648269E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81324E-03   0.45331E-02 0.19926E+01 
c  Velocity[X]                                      0.13787E-03 
c  Velocity[Y]                                      0.12774E-03 
c  Velocity[Z]                                      0.42675E-02 
c  Pressure     0.36376E-04     131   0.92550E-02   0.25657E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60978E-08   0.16235E-08 0.98569E-01 
c  r22          0.10852E-01      13   0.59862E-08   0.18400E-08 0.10060E+00 
c  r33          0.21861E-01      15   0.66889E-08   0.12574E-07 0.12671E+00 
c  r12          0.93875E-03      18   0.70429E-08   0.29462E-09 0.60136E+00 
c  r13          0.46678E-02      19   0.60310E-08   0.14924E-08 0.19882E+00 
c  r23          0.39979E-02      19   0.68491E-08   0.12912E-08 0.20008E+00 
c  epsilon      0.10969E+02      11   0.36380E-08   0.10300E-01 0.17065E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84013E-02 0.43300E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61373       0.0052575       0.0015075
v  Velocity[Y]            -0.57353         0.54425       0.0030802      0.00087299
v  Velocity[Z]              1.5654          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4403          4.3406          4.3632
v  Pressure                -36.412          360.02           87.64          169.84
v  r11                    0.001062        0.081928        0.013076        0.018287
v  r22                   0.0011156        0.082621        0.013356        0.018647
v  r33                   0.0016435         0.17431        0.027255        0.037208
v  r12                   -0.010664        0.013565     -0.00023386     -0.00030933
v  r13                    -0.04552        0.052801      9.3318e-05       0.0010139
v  r23                   -0.046709        0.051252        3.06e-05      0.00057465
v  epsilon                0.069456          271.18          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05        0.009918      0.00092527       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017872          5.2792         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8792         0.71352         0.85284


 TIME FOR THE TIME STEP            11001:        0.65629E+02

===============================================================


 INSTANT    0.110020000E-01   TIME STEP NUMBER           11002
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.361183937E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.207529493E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209935689E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.715565890E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.659450419E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81356E-03   0.45312E-02 0.19929E+01 
c  Velocity[X]                                      0.13738E-03 
c  Velocity[Y]                                      0.12840E-03 
c  Velocity[Z]                                      0.42654E-02 
c  Pressure     0.36161E-04     133   0.92080E-02   0.25505E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59057E-08   0.16472E-08 0.99014E-01 
c  r22          0.10852E-01      13   0.60644E-08   0.18544E-08 0.10138E+00 
c  r33          0.21861E-01      16   0.57890E-08   0.12698E-07 0.12720E+00 
c  r12          0.93875E-03      18   0.63982E-08   0.29622E-09 0.60002E+00 
c  r13          0.46678E-02      19   0.65299E-08   0.15197E-08 0.20054E+00 
c  r23          0.39979E-02      20   0.57466E-08   0.12952E-08 0.19937E+00 
c  epsilon      0.10969E+02      11   0.34448E-08   0.10079E-01 0.16655E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.83909E-02 0.43176E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63358         0.61369       0.0052575       0.0015075
v  Velocity[Y]            -0.57337         0.54439       0.0030801      0.00087295
v  Velocity[Z]              1.5655          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4403          4.3406          4.3632
v  Pressure                -36.451          360.07          87.661          169.88
v  r11                    0.001062        0.081928        0.013076        0.018287
v  r22                   0.0011156        0.082624        0.013356        0.018647
v  r33                   0.0016435         0.17433        0.027255        0.037208
v  r12                    -0.01067        0.013568     -0.00023386     -0.00030933
v  r13                   -0.045522        0.052803      9.3317e-05       0.0010139
v  r23                   -0.046709        0.051242        3.06e-05      0.00057465
v  epsilon                0.069457           271.2          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05        0.009918      0.00092527       0.0017428
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017872          5.2786         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            11002:        0.66526E+02

===============================================================


 INSTANT    0.110030000E-01   TIME STEP NUMBER           11003
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108813238E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208665006E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.135036173E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184952272E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.256595808E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81228E-03   0.45134E-02 0.19890E+01 
c  Velocity[X]                                      0.13795E-03 
c  Velocity[Y]                                      0.12772E-03 
c  Velocity[Z]                                      0.42477E-02 
c  Pressure     0.36125E-04     133   0.92020E-02   0.25480E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56486E-08   0.16488E-08 0.99151E-01 
c  r22          0.10852E-01      13   0.58700E-08   0.18174E-08 0.10048E+00 
c  r33          0.21861E-01      15   0.62006E-08   0.12527E-07 0.12649E+00 
c  r12          0.93875E-03      18   0.58336E-08   0.30605E-09 0.60751E+00 
c  r13          0.46678E-02      19   0.61074E-08   0.14836E-08 0.19862E+00 
c  r23          0.39979E-02      20   0.59959E-08   0.12961E-08 0.19965E+00 
c  epsilon      0.10969E+02      11   0.32846E-08   0.99660E-02 0.16487E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84456E-02 0.43330E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61373       0.0052575       0.0015075
v  Velocity[Y]            -0.57344         0.54417       0.0030802      0.00087299
v  Velocity[Z]              1.5656          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4404          4.3406          4.3632
v  Pressure                -36.394          360.08          87.677          169.89
v  r11                    0.001062        0.081931        0.013076        0.018287
v  r22                   0.0011156        0.082623        0.013356        0.018647
v  r33                   0.0016435          0.1743        0.027255        0.037208
v  r12                   -0.010668        0.013571     -0.00023386     -0.00030933
v  r13                   -0.045519        0.052799      9.3317e-05       0.0010139
v  r23                   -0.046709        0.051244        3.06e-05      0.00057465
v  epsilon                0.069458          271.22          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099181      0.00092527       0.0017428
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017872          5.2776         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11003:        0.65787E+02

===============================================================


 INSTANT    0.110040000E-01   TIME STEP NUMBER           11004
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.321577581E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.180827465E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.720809428E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.815358994E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.442472166E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81298E-03   0.45040E-02 0.19850E+01 
c  Velocity[X]                                      0.13721E-03 
c  Velocity[Y]                                      0.12823E-03 
c  Velocity[Z]                                      0.42385E-02 
c  Pressure     0.35969E-04     133   0.91575E-02   0.25370E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57341E-08   0.16755E-08 0.99723E-01 
c  r22          0.10852E-01      13   0.55689E-08   0.18527E-08 0.10114E+00 
c  r33          0.21861E-01      15   0.67229E-08   0.12787E-07 0.12758E+00 
c  r12          0.93875E-03      18   0.59684E-08   0.30045E-09 0.60408E+00 
c  r13          0.46678E-02      19   0.61186E-08   0.15112E-08 0.20049E+00 
c  r23          0.39979E-02      20   0.62022E-08   0.13080E-08 0.20065E+00 
c  epsilon      0.10969E+02      11   0.34299E-08   0.10288E-01 0.16842E+00 
c  TempC        0.25716E+06      16   0.15181E-04   0.84211E-02 0.43280E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63355         0.61372       0.0052575       0.0015074
v  Velocity[Y]            -0.57336         0.54412       0.0030802        0.000873
v  Velocity[Z]              1.5654          5.4403          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4403          4.3406          4.3632
v  Pressure                -36.445          359.99          87.648          169.84
v  r11                    0.001062        0.081937        0.013076        0.018287
v  r22                   0.0011156        0.082623        0.013356        0.018647
v  r33                   0.0016435         0.17427        0.027255        0.037208
v  r12                   -0.010666        0.013578     -0.00023386     -0.00030933
v  r13                   -0.045517        0.052798      9.3317e-05       0.0010139
v  r23                   -0.046709        0.051255        3.06e-05      0.00057465
v  epsilon                0.069459          271.15          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05        0.009918      0.00092527       0.0017428
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017872          5.2781         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            11004:        0.65806E+02

===============================================================


 INSTANT    0.110050000E-01   TIME STEP NUMBER           11005
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.722297591E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.806899238E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.894094120E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.211275899E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.452027895E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81255E-03   0.44826E-02 0.19817E+01 
c  Velocity[X]                                      0.13823E-03 
c  Velocity[Y]                                      0.12769E-03 
c  Velocity[Z]                                      0.42167E-02 
c  Pressure     0.35944E-04     133   0.91583E-02   0.25352E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59971E-08   0.16079E-08 0.98368E-01 
c  r22          0.10852E-01      13   0.52143E-08   0.18398E-08 0.10082E+00 
c  r33          0.21861E-01      15   0.73669E-08   0.12437E-07 0.12605E+00 
c  r12          0.93875E-03      18   0.50977E-08   0.29789E-09 0.60325E+00 
c  r13          0.46678E-02      19   0.53950E-08   0.15038E-08 0.19936E+00 
c  r23          0.39979E-02      19   0.65971E-08   0.12604E-08 0.19745E+00 
c  epsilon      0.10969E+02      11   0.35720E-08   0.98134E-02 0.16464E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.83300E-02 0.43048E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63359         0.61369       0.0052575       0.0015074
v  Velocity[Y]            -0.57353         0.54417       0.0030801      0.00087297
v  Velocity[Z]              1.5655          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4404          4.3406          4.3632
v  Pressure                -36.433             360          87.616          169.82
v  r11                    0.001062        0.081954        0.013076        0.018287
v  r22                   0.0011156         0.08262        0.013356        0.018647
v  r33                   0.0016435         0.17429        0.027255        0.037208
v  r12                   -0.010666        0.013577     -0.00023386     -0.00030933
v  r13                   -0.045521        0.052801      9.3317e-05       0.0010139
v  r23                   -0.046709        0.051279        3.06e-05      0.00057465
v  epsilon                 0.06946          271.17          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099179      0.00092527       0.0017428
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017872          5.2776         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11005:        0.64824E+02

===============================================================


 INSTANT    0.110060000E-01   TIME STEP NUMBER           11006
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.533143841E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.368219753E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.236551763E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.136904474E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.144310892E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81327E-03   0.45246E-02 0.19919E+01 
c  Velocity[X]                                      0.13788E-03 
c  Velocity[Y]                                      0.12832E-03 
c  Velocity[Z]                                      0.42584E-02 
c  Pressure     0.35789E-04     133   0.91064E-02   0.25242E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.63126E-08   0.16120E-08 0.98336E-01 
c  r22          0.10853E-01      13   0.54747E-08   0.17732E-08 0.99784E-01 
c  r33          0.21861E-01      15   0.66427E-08   0.12192E-07 0.12532E+00 
c  r12          0.93875E-03      18   0.53956E-08   0.29252E-09 0.59887E+00 
c  r13          0.46678E-02      19   0.60281E-08   0.14542E-08 0.19687E+00 
c  r23          0.39979E-02      19   0.56841E-08   0.12716E-08 0.19758E+00 
c  epsilon      0.10969E+02      11   0.34321E-08   0.92847E-02 0.16021E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.83858E-02 0.43254E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61374       0.0052575       0.0015074
v  Velocity[Y]            -0.57354         0.54428         0.00308       0.0008729
v  Velocity[Z]              1.5654          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4404          4.3406          4.3632
v  Pressure                -36.429          360.05           87.67          169.87
v  r11                    0.001062         0.08196        0.013076        0.018287
v  r22                   0.0011156        0.082623        0.013356        0.018647
v  r33                   0.0016435         0.17431        0.027255        0.037208
v  r12                   -0.010666        0.013578     -0.00023386     -0.00030933
v  r13                   -0.045519        0.052802      9.3318e-05       0.0010139
v  r23                   -0.046709        0.051272      3.0601e-05      0.00057465
v  epsilon                0.069462          271.21          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9929e-05       0.0099179      0.00092527       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017872           5.277         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71352         0.85284


 TIME FOR THE TIME STEP            11006:        0.66143E+02

===============================================================


 INSTANT    0.110070000E-01   TIME STEP NUMBER           11007
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.860636260E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934918E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.314994033E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100467367E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.210970983E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119607019E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81388E-03   0.45063E-02 0.19851E+01 
c  Velocity[X]                                      0.13636E-03 
c  Velocity[Y]                                      0.12798E-03 
c  Velocity[Z]                                      0.42420E-02 
c  Pressure     0.36131E-04     131   0.92000E-02   0.25485E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56089E-08   0.16430E-08 0.99122E-01 
c  r22          0.10853E-01      13   0.55130E-08   0.18236E-08 0.10084E+00 
c  r33          0.21861E-01      15   0.70174E-08   0.12565E-07 0.12698E+00 
c  r12          0.93875E-03      18   0.52504E-08   0.29954E-09 0.60486E+00 
c  r13          0.46678E-02      19   0.57923E-08   0.14786E-08 0.19898E+00 
c  r23          0.39979E-02      19   0.57763E-08   0.12933E-08 0.20011E+00 
c  epsilon      0.10969E+02      11   0.33706E-08   0.99832E-02 0.16898E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.84422E-02 0.43340E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61374       0.0052575       0.0015074
v  Velocity[Y]            -0.57365         0.54409       0.0030801      0.00087297
v  Velocity[Z]              1.5653          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4404          4.3406          4.3632
v  Pressure                -36.378          360.09          87.682          169.89
v  r11                    0.001062        0.081964        0.013076        0.018287
v  r22                   0.0011156        0.082624        0.013356        0.018647
v  r33                   0.0016435         0.17434        0.027255        0.037208
v  r12                   -0.010662        0.013582     -0.00023386     -0.00030933
v  r13                   -0.045517          0.0528      9.3318e-05       0.0010139
v  r23                   -0.046709        0.051259        3.06e-05      0.00057465
v  epsilon                0.069463          271.21          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099176      0.00092527       0.0017428
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017872          5.2774         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            11007:        0.67060E+02

===============================================================


 INSTANT    0.110080000E-01   TIME STEP NUMBER           11008
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.686083313E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.919001340E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229583533E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.210624204E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.298120228E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81372E-03   0.44846E-02 0.19836E+01 
c  Velocity[X]                                      0.13735E-03 
c  Velocity[Y]                                      0.12758E-03 
c  Velocity[Z]                                      0.42196E-02 
c  Pressure     0.36440E-04     132   0.92856E-02   0.25702E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.62090E-08   0.16546E-08 0.99355E-01 
c  r22          0.10853E-01      13   0.56672E-08   0.18517E-08 0.10137E+00 
c  r33          0.21861E-01      15   0.61522E-08   0.12692E-07 0.12729E+00 
c  r12          0.93875E-03      18   0.52286E-08   0.29916E-09 0.60598E+00 
c  r13          0.46678E-02      19   0.54210E-08   0.15089E-08 0.20024E+00 
c  r23          0.39979E-02      19   0.61704E-08   0.12727E-08 0.19775E+00 
c  epsilon      0.10969E+02      11   0.33107E-08   0.10098E-01 0.16669E+00 
c  TempC        0.25716E+06      16   0.15176E-04   0.83799E-02 0.43225E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334          0.6137       0.0052574       0.0015074
v  Velocity[Y]            -0.57361         0.54419         0.00308      0.00087291
v  Velocity[Z]              1.5654          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4404          4.3406          4.3632
v  Pressure                -36.445          360.08          87.676          169.89
v  r11                    0.001062        0.081977        0.013076        0.018287
v  r22                   0.0011156        0.082623        0.013356        0.018647
v  r33                   0.0016435         0.17432        0.027255        0.037208
v  r12                   -0.010663         0.01358     -0.00023386     -0.00030933
v  r13                   -0.045519        0.052797      9.3318e-05       0.0010139
v  r23                   -0.046709        0.051261        3.06e-05      0.00057465
v  epsilon                0.069464          271.21          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099176      0.00092527       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017873          5.2774         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            11008:        0.64805E+02

===============================================================


 INSTANT    0.110090000E-01   TIME STEP NUMBER           11009
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.178744499E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.405714875E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.167138169E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.147528513E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.126148269E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81206E-03   0.45405E-02 0.19940E+01 
c  Velocity[X]                                      0.13834E-03 
c  Velocity[Y]                                      0.12749E-03 
c  Velocity[Z]                                      0.42747E-02 
c  Pressure     0.36779E-04     132   0.93591E-02   0.25941E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60649E-08   0.16428E-08 0.99121E-01 
c  r22          0.10853E-01      13   0.54655E-08   0.18342E-08 0.10107E+00 
c  r33          0.21861E-01      15   0.58824E-08   0.12539E-07 0.12678E+00 
c  r12          0.93875E-03      17   0.69153E-08   0.29795E-09 0.60637E+00 
c  r13          0.46678E-02      19   0.67845E-08   0.15030E-08 0.19957E+00 
c  r23          0.39979E-02      19   0.65190E-08   0.12877E-08 0.19817E+00 
c  epsilon      0.10969E+02      11   0.33704E-08   0.96726E-02 0.16273E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.84482E-02 0.43322E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61375       0.0052574       0.0015074
v  Velocity[Y]            -0.57357         0.54437       0.0030801      0.00087296
v  Velocity[Z]              1.5653          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4404          4.3406          4.3632
v  Pressure                -36.396          360.02          87.631          169.83
v  r11                    0.001062        0.081983        0.013076        0.018287
v  r22                   0.0011156        0.082621        0.013356        0.018647
v  r33                   0.0016435          0.1743        0.027255        0.037208
v  r12                   -0.010659         0.01358     -0.00023386     -0.00030933
v  r13                   -0.045519        0.052796      9.3318e-05       0.0010139
v  r23                   -0.046709        0.051261      3.0601e-05      0.00057465
v  epsilon                0.069465          271.17          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099175      0.00092527       0.0017428
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017873          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            11009:        0.66109E+02

===============================================================


 INSTANT    0.110100000E-01   TIME STEP NUMBER           11010
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.585654205E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.228370044E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.225770664E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.700642018E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145651567E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81326E-03   0.45213E-02 0.19887E+01 
c  Velocity[X]                                      0.13716E-03 
c  Velocity[Y]                                      0.12843E-03 
c  Velocity[Z]                                      0.42557E-02 
c  Pressure     0.35973E-04     133   0.91518E-02   0.25373E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60950E-08   0.16239E-08 0.98822E-01 
c  r22          0.10853E-01      13   0.53681E-08   0.18128E-08 0.10079E+00 
c  r33          0.21861E-01      15   0.67077E-08   0.12455E-07 0.12677E+00 
c  r12          0.93875E-03      18   0.53218E-08   0.29810E-09 0.60514E+00 
c  r13          0.46678E-02      19   0.64635E-08   0.14789E-08 0.19925E+00 
c  r23          0.39979E-02      19   0.64531E-08   0.12759E-08 0.19844E+00 
c  epsilon      0.10969E+02      11   0.33712E-08   0.98333E-02 0.16472E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84218E-02 0.43280E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61372       0.0052574       0.0015074
v  Velocity[Y]            -0.57343         0.54405       0.0030801      0.00087297
v  Velocity[Z]              1.5656          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4404          4.3406          4.3632
v  Pressure                -36.433          359.97           87.63          169.81
v  r11                    0.001062         0.08199        0.013076        0.018287
v  r22                   0.0011156        0.082619        0.013356        0.018647
v  r33                   0.0016436         0.17429        0.027255        0.037208
v  r12                   -0.010662        0.013582     -0.00023386     -0.00030933
v  r13                   -0.045518        0.052796      9.3319e-05       0.0010139
v  r23                   -0.046709         0.05129      3.0602e-05      0.00057465
v  epsilon                0.069466          271.18          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099176      0.00092527       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017873          5.2774         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            11010:        0.66540E+02

===============================================================


 INSTANT    0.110110000E-01   TIME STEP NUMBER           11011
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.963357767E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.214517663E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.431474112E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.579732472E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153720160E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81366E-03   0.44839E-02 0.19838E+01 
c  Velocity[X]                                      0.13665E-03 
c  Velocity[Y]                                      0.12795E-03 
c  Velocity[Z]                                      0.42193E-02 
c  Pressure     0.36171E-04     133   0.92153E-02   0.25511E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.63277E-08   0.16293E-08 0.99434E-01 
c  r22          0.10853E-01      13   0.52603E-08   0.18302E-08 0.10115E+00 
c  r33          0.21861E-01      15   0.66386E-08   0.12484E-07 0.12690E+00 
c  r12          0.93875E-03      18   0.56860E-08   0.29457E-09 0.60235E+00 
c  r13          0.46678E-02      19   0.65533E-08   0.14877E-08 0.19946E+00 
c  r23          0.39979E-02      19   0.65935E-08   0.12717E-08 0.19833E+00 
c  epsilon      0.10969E+02      11   0.31824E-08   0.98828E-02 0.16589E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.83953E-02 0.43242E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61371       0.0052574       0.0015074
v  Velocity[Y]            -0.57363         0.54407       0.0030801      0.00087296
v  Velocity[Z]              1.5651          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5789          5.4404          4.3406          4.3632
v  Pressure                -36.383          360.06          87.664          169.87
v  r11                    0.001062        0.081989        0.013076        0.018287
v  r22                   0.0011156        0.082617        0.013356        0.018647
v  r33                   0.0016436         0.17431        0.027255        0.037208
v  r12                   -0.010663        0.013579     -0.00023386     -0.00030933
v  r13                    -0.04552        0.052794      9.3319e-05       0.0010139
v  r23                   -0.046708        0.051276      3.0602e-05      0.00057465
v  epsilon                0.069467          271.21          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099176      0.00092528       0.0017428
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017873          5.2779         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            11011:        0.68183E+02

===============================================================


 INSTANT    0.110120000E-01   TIME STEP NUMBER           11012
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.134638437E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.240520071E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.974865884E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.593149719E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.349721473E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81230E-03   0.45206E-02 0.19895E+01 
c  Velocity[X]                                      0.13755E-03 
c  Velocity[Y]                                      0.12799E-03 
c  Velocity[Z]                                      0.42551E-02 
c  Pressure     0.36230E-04     132   0.92272E-02   0.25554E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.62724E-08   0.16278E-08 0.99351E-01 
c  r22          0.10853E-01      13   0.53405E-08   0.18031E-08 0.10072E+00 
c  r33          0.21861E-01      15   0.64413E-08   0.12398E-07 0.12668E+00 
c  r12          0.93876E-03      18   0.62735E-08   0.29384E-09 0.60130E+00 
c  r13          0.46678E-02      19   0.67813E-08   0.14780E-08 0.19875E+00 
c  r23          0.39979E-02      19   0.62501E-08   0.12714E-08 0.19903E+00 
c  epsilon      0.10969E+02      11   0.32087E-08   0.10034E-01 0.16792E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.83946E-02 0.43217E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61376       0.0052574       0.0015074
v  Velocity[Y]            -0.57354         0.54424         0.00308      0.00087294
v  Velocity[Z]              1.5654          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4404          4.3406          4.3632
v  Pressure                -36.421          360.01          87.657          169.84
v  r11                    0.001062         0.08199        0.013076        0.018287
v  r22                   0.0011156        0.082615        0.013356        0.018647
v  r33                   0.0016436         0.17429        0.027255        0.037208
v  r12                   -0.010662        0.013574     -0.00023386     -0.00030933
v  r13                   -0.045518        0.052796      9.3319e-05       0.0010139
v  r23                   -0.046708         0.05126      3.0602e-05      0.00057465
v  epsilon                0.069468           271.2          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099176      0.00092528       0.0017428
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017873          5.2781         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            11012:        0.66412E+02

===============================================================


 INSTANT    0.110130000E-01   TIME STEP NUMBER           11013
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.368457049E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.150202315E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.467686020E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.201960965E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.291946564E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81323E-03   0.45240E-02 0.19895E+01 
c  Velocity[X]                                      0.13876E-03 
c  Velocity[Y]                                      0.12754E-03 
c  Velocity[Z]                                      0.42577E-02 
c  Pressure     0.36274E-04     133   0.92423E-02   0.25585E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59487E-08   0.16541E-08 0.10026E+00 
c  r22          0.10853E-01      13   0.52021E-08   0.18152E-08 0.10114E+00 
c  r33          0.21861E-01      15   0.71821E-08   0.12621E-07 0.12796E+00 
c  r12          0.93876E-03      18   0.57784E-08   0.29765E-09 0.60638E+00 
c  r13          0.46678E-02      20   0.59466E-08   0.14987E-08 0.20051E+00 
c  r23          0.39979E-02      19   0.62663E-08   0.13048E-08 0.20166E+00 
c  epsilon      0.10969E+02      11   0.33777E-08   0.10141E-01 0.17012E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.84304E-02 0.43351E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61376       0.0052574       0.0015074
v  Velocity[Y]            -0.57365         0.54436       0.0030801      0.00087296
v  Velocity[Z]              1.5656          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4404          4.3406          4.3632
v  Pressure                -36.414          360.07          87.673          169.89
v  r11                    0.001062        0.081987        0.013076        0.018287
v  r22                   0.0011156        0.082614        0.013356        0.018647
v  r33                   0.0016436         0.17431        0.027255        0.037208
v  r12                   -0.010658        0.013574     -0.00023386     -0.00030933
v  r13                   -0.045519        0.052795      9.3318e-05       0.0010139
v  r23                   -0.046708         0.05125      3.0602e-05      0.00057465
v  epsilon                0.069469          271.16          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099176      0.00092528       0.0017428
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017873          5.2793         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8793         0.71352         0.85284


 TIME FOR THE TIME STEP            11013:        0.66878E+02

===============================================================


 INSTANT    0.110140000E-01   TIME STEP NUMBER           11014
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.872136057E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.257799851E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.287899102E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.321728285E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.591220343E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11250E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81347E-03   0.45066E-02 0.19876E+01 
c  Velocity[X]                                      0.13650E-03 
c  Velocity[Y]                                      0.12782E-03 
c  Velocity[Z]                                      0.42423E-02 
c  Pressure     0.36408E-04     132   0.92619E-02   0.25680E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59509E-08   0.16117E-08 0.98719E-01 
c  r22          0.10853E-01      13   0.49545E-08   0.18411E-08 0.10151E+00 
c  r33          0.21861E-01      15   0.57630E-08   0.12436E-07 0.12684E+00 
c  r12          0.93876E-03      18   0.52660E-08   0.29331E-09 0.59984E+00 
c  r13          0.46678E-02      19   0.68386E-08   0.15013E-08 0.19975E+00 
c  r23          0.39979E-02      19   0.62624E-08   0.12515E-08 0.19713E+00 
c  epsilon      0.10969E+02      11   0.32581E-08   0.97070E-02 0.16400E+00 
c  TempC        0.25716E+06      16   0.15171E-04   0.83915E-02 0.43192E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61371       0.0052574       0.0015074
v  Velocity[Y]            -0.57347         0.54419         0.00308      0.00087296
v  Velocity[Z]              1.5653          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4404          4.3406          4.3632
v  Pressure                -36.412          360.05          87.651          169.87
v  r11                    0.001062        0.081987        0.013076        0.018287
v  r22                   0.0011156        0.082614        0.013356        0.018647
v  r33                   0.0016436         0.17434        0.027255        0.037208
v  r12                   -0.010659        0.013575     -0.00023386     -0.00030933
v  r13                    -0.04552        0.052797      9.3318e-05       0.0010139
v  r23                   -0.046708        0.051241      3.0602e-05      0.00057464
v  epsilon                0.069471          271.16          7.2636          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099173      0.00092528       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017873          5.2789         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            11014:        0.65928E+02

===============================================================


 INSTANT    0.110150000E-01   TIME STEP NUMBER           11015
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.253757494E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.112929063E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138290826E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.259915993E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.393767442E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81234E-03   0.45251E-02 0.19927E+01 
c  Velocity[X]                                      0.13757E-03 
c  Velocity[Y]                                      0.12805E-03 
c  Velocity[Z]                                      0.42595E-02 
c  Pressure     0.36133E-04     131   0.91992E-02   0.25486E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.63226E-08   0.16264E-08 0.99098E-01 
c  r22          0.10853E-01      13   0.46639E-08   0.18124E-08 0.10090E+00 
c  r33          0.21861E-01      15   0.61530E-08   0.12449E-07 0.12679E+00 
c  r12          0.93876E-03      18   0.51726E-08   0.29631E-09 0.60405E+00 
c  r13          0.46678E-02      19   0.67593E-08   0.14924E-08 0.19958E+00 
c  r23          0.39979E-02      19   0.67491E-08   0.12718E-08 0.19780E+00 
c  epsilon      0.10969E+02      11   0.33002E-08   0.95970E-02 0.16223E+00 
c  TempC        0.25716E+06      16   0.15125E-04   0.83641E-02 0.43127E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63357         0.61376       0.0052575       0.0015074
v  Velocity[Y]            -0.57344         0.54432         0.00308      0.00087294
v  Velocity[Z]              1.5654          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4404          4.3406          4.3632
v  Pressure                 -36.38          360.03          87.653          169.86
v  r11                    0.001062        0.081998        0.013076        0.018287
v  r22                   0.0011156        0.082612        0.013356        0.018647
v  r33                   0.0016436         0.17436        0.027255        0.037208
v  r12                   -0.010659        0.013579     -0.00023386     -0.00030933
v  r13                   -0.045517        0.052797      9.3319e-05       0.0010139
v  r23                   -0.046707        0.051273      3.0602e-05      0.00057464
v  epsilon                0.069472           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099175      0.00092528       0.0017428
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017873           5.279         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71352         0.85284


 TIME FOR THE TIME STEP            11015:        0.66835E+02

===============================================================


 INSTANT    0.110160000E-01   TIME STEP NUMBER           11016
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161496795E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.203354425E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.538374941E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.406732157E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.782790203E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81383E-03   0.45041E-02 0.19881E+01 
c  Velocity[X]                                      0.13667E-03 
c  Velocity[Y]                                      0.12799E-03 
c  Velocity[Z]                                      0.42395E-02 
c  Pressure     0.36134E-04     133   0.91957E-02   0.25486E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61804E-08   0.16064E-08 0.98455E-01 
c  r22          0.10853E-01      13   0.48593E-08   0.18463E-08 0.10129E+00 
c  r33          0.21861E-01      15   0.54382E-08   0.12534E-07 0.12661E+00 
c  r12          0.93876E-03      18   0.54243E-08   0.29492E-09 0.60270E+00 
c  r13          0.46678E-02      19   0.63299E-08   0.15184E-08 0.20044E+00 
c  r23          0.39979E-02      19   0.62523E-08   0.12759E-08 0.19828E+00 
c  epsilon      0.10969E+02      11   0.33550E-08   0.99462E-02 0.16605E+00 
c  TempC        0.25716E+06      16   0.15171E-04   0.84262E-02 0.43312E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61373       0.0052574       0.0015074
v  Velocity[Y]            -0.57331         0.54432       0.0030801      0.00087296
v  Velocity[Z]              1.5653          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4404          4.3406          4.3632
v  Pressure                -36.463          360.03          87.673          169.87
v  r11                    0.001062        0.082003        0.013076        0.018287
v  r22                   0.0011157        0.082614        0.013356        0.018647
v  r33                   0.0016436         0.17438        0.027255        0.037208
v  r12                   -0.010658        0.013588     -0.00023386     -0.00030933
v  r13                   -0.045516        0.052793      9.3319e-05       0.0010139
v  r23                   -0.046707        0.051261      3.0603e-05      0.00057464
v  epsilon                0.069473           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099176      0.00092528       0.0017428
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017873          5.2786         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            11016:        0.66039E+02

===============================================================


 INSTANT    0.110170000E-01   TIME STEP NUMBER           11017
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136034716E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.449275147E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.523388290E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201416156E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.562395399E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81343E-03   0.45144E-02 0.19892E+01 
c  Velocity[X]                                      0.13653E-03 
c  Velocity[Y]                                      0.12811E-03 
c  Velocity[Z]                                      0.42498E-02 
c  Pressure     0.36112E-04     131   0.91899E-02   0.25470E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.66122E-08   0.16567E-08 0.99371E-01 
c  r22          0.10853E-01      13   0.50905E-08   0.18479E-08 0.10118E+00 
c  r33          0.21861E-01      15   0.58300E-08   0.12626E-07 0.12658E+00 
c  r12          0.93876E-03      18   0.50150E-08   0.29572E-09 0.60267E+00 
c  r13          0.46678E-02      19   0.65564E-08   0.15082E-08 0.19886E+00 
c  r23          0.39979E-02      19   0.63066E-08   0.12958E-08 0.19858E+00 
c  epsilon      0.10969E+02      11   0.34182E-08   0.99446E-02 0.16713E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84180E-02 0.43288E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61369       0.0052575       0.0015074
v  Velocity[Y]             -0.5733         0.54433       0.0030801      0.00087296
v  Velocity[Z]              1.5654          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4404          4.3406          4.3632
v  Pressure                -36.386             360          87.629          169.83
v  r11                    0.001062        0.082003        0.013076        0.018287
v  r22                   0.0011157        0.082616        0.013356        0.018647
v  r33                   0.0016436         0.17435        0.027255        0.037208
v  r12                    -0.01066         0.01359     -0.00023386     -0.00030933
v  r13                   -0.045521        0.052789      9.3318e-05       0.0010139
v  r23                   -0.046706        0.051252      3.0602e-05      0.00057464
v  epsilon                0.069474          271.15          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099176      0.00092528       0.0017428
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017873          5.2783         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71352         0.85284


 TIME FOR THE TIME STEP            11017:        0.67018E+02

===============================================================


 INSTANT    0.110180000E-01   TIME STEP NUMBER           11018
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.102997648E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.215088524E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.257302183E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.123944040E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.250064031E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81279E-03   0.45240E-02 0.19894E+01 
c  Velocity[X]                                      0.13830E-03 
c  Velocity[Y]                                      0.12839E-03 
c  Velocity[Z]                                      0.42573E-02 
c  Pressure     0.36288E-04     132   0.92379E-02   0.25596E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61956E-08   0.16558E-08 0.99590E-01 
c  r22          0.10853E-01      13   0.49484E-08   0.18319E-08 0.10147E+00 
c  r33          0.21861E-01      15   0.71553E-08   0.12560E-07 0.12728E+00 
c  r12          0.93876E-03      18   0.51967E-08   0.29582E-09 0.60469E+00 
c  r13          0.46678E-02      19   0.71831E-08   0.14889E-08 0.19974E+00 
c  r23          0.39979E-02      20   0.54537E-08   0.12956E-08 0.19994E+00 
c  epsilon      0.10969E+02      11   0.34504E-08   0.98578E-02 0.16638E+00 
c  TempC        0.25716E+06      16   0.15180E-04   0.84448E-02 0.43375E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63357         0.61374       0.0052574       0.0015074
v  Velocity[Y]            -0.57343         0.54442         0.00308      0.00087292
v  Velocity[Z]              1.5654          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4404          4.3406          4.3632
v  Pressure                -36.417          360.03          87.662          169.86
v  r11                    0.001062        0.081998        0.013076        0.018287
v  r22                   0.0011157        0.082615        0.013356        0.018647
v  r33                   0.0016436         0.17431        0.027255        0.037208
v  r12                   -0.010661        0.013593     -0.00023386     -0.00030933
v  r13                   -0.045518        0.052786      9.3318e-05       0.0010139
v  r23                   -0.046706        0.051251      3.0603e-05      0.00057464
v  epsilon                0.069475          271.16          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099174      0.00092528       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017874          5.2789         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            11018:        0.67092E+02

===============================================================


 INSTANT    0.110190000E-01   TIME STEP NUMBER           11019
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.412213940E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.953308482E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123598354E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.403509969E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.653034747E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81208E-03   0.45376E-02 0.19935E+01 
c  Velocity[X]                                      0.13888E-03 
c  Velocity[Y]                                      0.12821E-03 
c  Velocity[Z]                                      0.42705E-02 
c  Pressure     0.36370E-04     132   0.92649E-02   0.25653E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.64786E-08   0.16595E-08 0.99825E-01 
c  r22          0.10853E-01      13   0.52730E-08   0.18285E-08 0.10101E+00 
c  r33          0.21861E-01      15   0.54044E-08   0.12614E-07 0.12731E+00 
c  r12          0.93876E-03      18   0.65955E-08   0.30775E-09 0.60697E+00 
c  r13          0.46678E-02      19   0.64632E-08   0.14925E-08 0.19934E+00 
c  r23          0.39979E-02      19   0.66419E-08   0.12945E-08 0.20022E+00 
c  epsilon      0.10969E+02      11   0.32652E-08   0.10299E-01 0.17227E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.84399E-02 0.43350E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63333         0.61374       0.0052574       0.0015074
v  Velocity[Y]            -0.57362         0.54422       0.0030801      0.00087297
v  Velocity[Z]              1.5653          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4405          4.3406          4.3632
v  Pressure                  -36.4          359.98          87.618          169.82
v  r11                    0.001062        0.081996        0.013076        0.018287
v  r22                   0.0011157        0.082614        0.013356        0.018647
v  r33                   0.0016436         0.17432        0.027255        0.037208
v  r12                    -0.01066        0.013597     -0.00023386     -0.00030933
v  r13                   -0.045517        0.052785      9.3318e-05       0.0010139
v  r23                   -0.046704        0.051247      3.0602e-05      0.00057464
v  epsilon                0.069476          271.17          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099173      0.00092528       0.0017428
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017874          5.2787         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85284


 TIME FOR THE TIME STEP            11019:        0.67016E+02

===============================================================


 INSTANT    0.110200000E-01   TIME STEP NUMBER           11020
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.136898834E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.738063363E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221371230E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.307262000E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.149520934E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81346E-03   0.44586E-02 0.19785E+01 
c  Velocity[X]                                      0.13699E-03 
c  Velocity[Y]                                      0.12748E-03 
c  Velocity[Z]                                      0.41941E-02 
c  Pressure     0.35949E-04     133   0.91521E-02   0.25355E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60245E-08   0.16603E-08 0.99617E-01 
c  r22          0.10853E-01      13   0.46478E-08   0.18864E-08 0.10195E+00 
c  r33          0.21861E-01      14   0.68057E-08   0.12863E-07 0.12796E+00 
c  r12          0.93876E-03      18   0.63770E-08   0.29625E-09 0.60191E+00 
c  r13          0.46678E-02      19   0.67494E-08   0.15362E-08 0.20083E+00 
c  r23          0.39979E-02      19   0.60988E-08   0.12852E-08 0.19935E+00 
c  epsilon      0.10969E+02      11   0.34756E-08   0.10480E-01 0.17095E+00 
c  TempC        0.25716E+06      16   0.15155E-04   0.83370E-02 0.43052E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339          0.6137       0.0052574       0.0015074
v  Velocity[Y]            -0.57353          0.5443         0.00308      0.00087292
v  Velocity[Z]              1.5655          5.4404          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4404          4.3406          4.3632
v  Pressure                -36.425          360.05          87.666          169.87
v  r11                    0.001062        0.081996        0.013076        0.018287
v  r22                   0.0011157        0.082612        0.013356        0.018647
v  r33                   0.0016436         0.17434        0.027255        0.037208
v  r12                   -0.010658        0.013597     -0.00023386     -0.00030933
v  r13                   -0.045519        0.052787      9.3317e-05       0.0010139
v  r23                   -0.046702        0.051254      3.0601e-05      0.00057464
v  epsilon                0.069477          271.18          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099174      0.00092528       0.0017428
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017874          5.2789         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            11020:        0.65926E+02

===============================================================


 INSTANT    0.110210000E-01   TIME STEP NUMBER           11021
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.758481248E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.184063741E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.379184365E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.140721491E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.376980172E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81244E-03   0.45223E-02 0.19918E+01 
c  Velocity[X]                                      0.13700E-03 
c  Velocity[Y]                                      0.12755E-03 
c  Velocity[Z]                                      0.42577E-02 
c  Pressure     0.36401E-04     133   0.92636E-02   0.25674E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55827E-08   0.16318E-08 0.99187E-01 
c  r22          0.10853E-01      13   0.47378E-08   0.18185E-08 0.10078E+00 
c  r33          0.21861E-01      15   0.55966E-08   0.12450E-07 0.12639E+00 
c  r12          0.93876E-03      18   0.69736E-08   0.29454E-09 0.60352E+00 
c  r13          0.46678E-02      19   0.69742E-08   0.14958E-08 0.19914E+00 
c  r23          0.39979E-02      19   0.61982E-08   0.12774E-08 0.19814E+00 
c  epsilon      0.10969E+02      11   0.35753E-08   0.98082E-02 0.16484E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.84205E-02 0.43356E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61379       0.0052575       0.0015074
v  Velocity[Y]             -0.5735          0.5444       0.0030801      0.00087294
v  Velocity[Z]              1.5654          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4405          4.3406          4.3632
v  Pressure                -36.397          360.02          87.642          169.85
v  r11                    0.001062        0.082005        0.013076        0.018287
v  r22                   0.0011157        0.082608        0.013356        0.018647
v  r33                   0.0016436         0.17436        0.027255        0.037208
v  r12                   -0.010662        0.013602     -0.00023386     -0.00030933
v  r13                   -0.045518         0.05279      9.3317e-05       0.0010139
v  r23                   -0.046701        0.051292      3.0601e-05      0.00057464
v  epsilon                0.069478          271.15          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099174      0.00092528       0.0017428
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017874          5.2792         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8792         0.71352         0.85284


 TIME FOR THE TIME STEP            11021:        0.69119E+02

===============================================================


 INSTANT    0.110220000E-01   TIME STEP NUMBER           11022
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.567687340E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136554114E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.225776562E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.527642815E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.313606532E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33841E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81342E-03   0.45193E-02 0.19909E+01 
c  Velocity[X]                                      0.13710E-03 
c  Velocity[Y]                                      0.12882E-03 
c  Velocity[Z]                                      0.42534E-02 
c  Pressure     0.36172E-04     133   0.92091E-02   0.25513E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57437E-08   0.16406E-08 0.99462E-01 
c  r22          0.10853E-01      13   0.53863E-08   0.18122E-08 0.10080E+00 
c  r33          0.21861E-01      15   0.58354E-08   0.12485E-07 0.12684E+00 
c  r12          0.93876E-03      18   0.69319E-08   0.29640E-09 0.60482E+00 
c  r13          0.46678E-02      19   0.65339E-08   0.14973E-08 0.19927E+00 
c  r23          0.39979E-02      19   0.52678E-08   0.12817E-08 0.19923E+00 
c  epsilon      0.10969E+02      11   0.34870E-08   0.98269E-02 0.16536E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84253E-02 0.43279E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63335         0.61374       0.0052575       0.0015074
v  Velocity[Y]             -0.5734         0.54421       0.0030801      0.00087293
v  Velocity[Z]              1.5654          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4405          4.3406          4.3632
v  Pressure                -36.435          360.04          87.682          169.87
v  r11                    0.001062         0.08201        0.013076        0.018287
v  r22                   0.0011157        0.082609        0.013356        0.018647
v  r33                   0.0016436         0.17437        0.027255        0.037208
v  r12                   -0.010664          0.0136     -0.00023386     -0.00030933
v  r13                   -0.045516        0.052788      9.3318e-05       0.0010139
v  r23                   -0.046699        0.051284      3.0602e-05      0.00057464
v  epsilon                0.069479          271.17          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099175      0.00092528       0.0017428
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017874          5.2794         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8794         0.71352         0.85284


 TIME FOR THE TIME STEP            11022:        0.66329E+02

===============================================================


 INSTANT    0.110230000E-01   TIME STEP NUMBER           11023
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249846580E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.251494919E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.279408794E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.316976215E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190032198E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81293E-03   0.44668E-02 0.19785E+01 
c  Velocity[X]                                      0.13694E-03 
c  Velocity[Y]                                      0.12731E-03 
c  Velocity[Z]                                      0.42026E-02 
c  Pressure     0.36129E-04     136   0.91965E-02   0.25482E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58875E-08   0.17032E-08 0.10062E+00 
c  r22          0.10853E-01      13   0.52290E-08   0.18448E-08 0.10104E+00 
c  r33          0.21861E-01      15   0.73631E-08   0.12895E-07 0.12796E+00 
c  r12          0.93876E-03      18   0.69331E-08   0.30092E-09 0.60887E+00 
c  r13          0.46678E-02      19   0.62698E-08   0.15043E-08 0.19924E+00 
c  r23          0.39979E-02      18   0.67017E-08   0.13446E-08 0.20287E+00 
c  epsilon      0.10969E+02      11   0.35255E-08   0.10287E-01 0.16843E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.83854E-02 0.43197E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63335         0.61373       0.0052574       0.0015074
v  Velocity[Y]            -0.57357         0.54431       0.0030801      0.00087296
v  Velocity[Z]              1.5654          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4405          4.3406          4.3632
v  Pressure                -36.401          360.05          87.655          169.87
v  r11                    0.001062        0.082005        0.013076        0.018287
v  r22                   0.0011157        0.082606        0.013356        0.018647
v  r33                   0.0016436         0.17438        0.027255        0.037208
v  r12                   -0.010665        0.013602     -0.00023386     -0.00030933
v  r13                   -0.045519        0.052786      9.3318e-05       0.0010139
v  r23                   -0.046698        0.051273      3.0603e-05      0.00057464
v  epsilon                0.069481          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099176      0.00092528       0.0017428
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017874          5.2792         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8792         0.71352         0.85284


 TIME FOR THE TIME STEP            11023:        0.70060E+02

===============================================================


 INSTANT    0.110240000E-01   TIME STEP NUMBER           11024
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.942216234E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.272203067E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.355756475E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.175895462E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.185526130E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81323E-03   0.45213E-02 0.19887E+01 
c  Velocity[X]                                      0.13644E-03 
c  Velocity[Y]                                      0.12695E-03 
c  Velocity[Z]                                      0.42579E-02 
c  Pressure     0.36517E-04     132   0.92892E-02   0.25756E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59430E-08   0.16906E-08 0.10047E+00 
c  r22          0.10853E-01      13   0.54565E-08   0.18232E-08 0.10076E+00 
c  r33          0.21861E-01      15   0.68904E-08   0.12584E-07 0.12698E+00 
c  r12          0.93876E-03      18   0.71019E-08   0.30086E-09 0.60640E+00 
c  r13          0.46678E-02      19   0.70988E-08   0.14708E-08 0.19717E+00 
c  r23          0.39979E-02      19   0.56579E-08   0.13121E-08 0.20102E+00 
c  epsilon      0.10969E+02      11   0.33367E-08   0.96523E-02 0.16467E+00 
c  TempC        0.25716E+06      16   0.15185E-04   0.84149E-02 0.43232E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61376       0.0052574       0.0015074
v  Velocity[Y]            -0.57347         0.54442         0.00308      0.00087294
v  Velocity[Z]              1.5653          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4405          4.3406          4.3632
v  Pressure                -36.451          359.98          87.613          169.81
v  r11                    0.001062        0.082003        0.013076        0.018287
v  r22                   0.0011157        0.082606        0.013356        0.018647
v  r33                   0.0016436         0.17434        0.027255        0.037208
v  r12                   -0.010665        0.013607     -0.00023386     -0.00030933
v  r13                   -0.045516        0.052783      9.3318e-05       0.0010139
v  r23                   -0.046697        0.051261      3.0603e-05      0.00057464
v  epsilon                0.069482          271.17          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099176      0.00092528       0.0017428
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017874          5.2794         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8794         0.71352         0.85284


 TIME FOR THE TIME STEP            11024:        0.66973E+02

===============================================================


 INSTANT    0.110250000E-01   TIME STEP NUMBER           11025
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.345441046E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.414861761E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.532979521E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.298758940E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.872971349E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81244E-03   0.45260E-02 0.19912E+01 
c  Velocity[X]                                      0.13854E-03 
c  Velocity[Y]                                      0.12772E-03 
c  Velocity[Z]                                      0.42597E-02 
c  Pressure     0.36359E-04     132   0.92499E-02   0.25645E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59174E-08   0.16604E-08 0.99606E-01 
c  r22          0.10853E-01      13   0.50223E-08   0.18534E-08 0.10134E+00 
c  r33          0.21861E-01      16   0.66592E-08   0.12755E-07 0.12732E+00 
c  r12          0.93876E-03      18   0.63511E-08   0.29801E-09 0.60506E+00 
c  r13          0.46678E-02      19   0.64330E-08   0.15217E-08 0.20005E+00 
c  r23          0.39979E-02      19   0.59657E-08   0.13068E-08 0.20028E+00 
c  epsilon      0.10969E+02      11   0.34893E-08   0.10513E-01 0.17373E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.84037E-02 0.43269E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61375       0.0052575       0.0015074
v  Velocity[Y]            -0.57347         0.54406       0.0030801      0.00087296
v  Velocity[Z]              1.5655          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4405          4.3406          4.3632
v  Pressure                -36.415          360.06          87.654          169.88
v  r11                   0.0010621        0.082002        0.013076        0.018287
v  r22                   0.0011157        0.082606        0.013356        0.018647
v  r33                   0.0016437         0.17431        0.027255        0.037208
v  r12                   -0.010669        0.013609     -0.00023386     -0.00030933
v  r13                   -0.045517        0.052781      9.3318e-05       0.0010139
v  r23                   -0.046696        0.051291      3.0603e-05      0.00057464
v  epsilon                0.069483          271.12          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099178      0.00092528       0.0017428
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017874          5.2796         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8796         0.71352         0.85284


 TIME FOR THE TIME STEP            11025:        0.68025E+02

===============================================================


 INSTANT    0.110260000E-01   TIME STEP NUMBER           11026
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.933187734E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.279715472E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.584091977E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.407131853E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.304390873E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81385E-03   0.45043E-02 0.19872E+01 
c  Velocity[X]                                      0.13602E-03 
c  Velocity[Y]                                      0.12739E-03 
c  Velocity[Z]                                      0.42409E-02 
c  Pressure     0.36140E-04     133   0.92048E-02   0.25490E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.62589E-08   0.16705E-08 0.10025E+00 
c  r22          0.10853E-01      13   0.48389E-08   0.18609E-08 0.10181E+00 
c  r33          0.21861E-01      16   0.58221E-08   0.12719E-07 0.12783E+00 
c  r12          0.93876E-03      18   0.66326E-08   0.29654E-09 0.60612E+00 
c  r13          0.46678E-02      19   0.65598E-08   0.15146E-08 0.20015E+00 
c  r23          0.39979E-02      19   0.71446E-08   0.12851E-08 0.20009E+00 
c  epsilon      0.10969E+02      11   0.35222E-08   0.99257E-02 0.16626E+00 
c  TempC        0.25716E+06      16   0.15155E-04   0.83625E-02 0.43194E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61373       0.0052574       0.0015074
v  Velocity[Y]            -0.57341         0.54408         0.00308      0.00087294
v  Velocity[Z]              1.5656          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4405          4.3406          4.3632
v  Pressure                -36.442          360.06          87.674          169.88
v  r11                   0.0010621        0.082015        0.013076        0.018287
v  r22                   0.0011157        0.082607        0.013356        0.018647
v  r33                   0.0016437         0.17431        0.027255        0.037208
v  r12                   -0.010666        0.013609     -0.00023386     -0.00030933
v  r13                   -0.045519        0.052783      9.3319e-05       0.0010139
v  r23                   -0.046695        0.051287      3.0603e-05      0.00057464
v  epsilon                0.069484          271.15          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099179      0.00092528       0.0017428
v  CourantNb               0.44257             0.6         0.59908         0.59839
v  FourierNb             0.0017875            5.28         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179            5.88         0.71352         0.85284


 TIME FOR THE TIME STEP            11026:        0.66699E+02

===============================================================


 INSTANT    0.110270000E-01   TIME STEP NUMBER           11027
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.271341105E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.547348597E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.371046783E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.880276121E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232390064E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81219E-03   0.44764E-02 0.19819E+01 
c  Velocity[X]                                      0.13697E-03 
c  Velocity[Y]                                      0.12907E-03 
c  Velocity[Z]                                      0.42103E-02 
c  Pressure     0.36021E-04     132   0.91794E-02   0.25406E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.66510E-08   0.16166E-08 0.98045E-01 
c  r22          0.10853E-01      13   0.51884E-08   0.18303E-08 0.10075E+00 
c  r33          0.21861E-01      15   0.70859E-08   0.12479E-07 0.12577E+00 
c  r12          0.93876E-03      18   0.69921E-08   0.29619E-09 0.60229E+00 
c  r13          0.46678E-02      19   0.73335E-08   0.15081E-08 0.19893E+00 
c  r23          0.39979E-02      19   0.74558E-08   0.12769E-08 0.19701E+00 
c  epsilon      0.10969E+02      11   0.35249E-08   0.97910E-02 0.16424E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84044E-02 0.43222E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61374       0.0052575       0.0015075
v  Velocity[Y]            -0.57341         0.54418         0.00308      0.00087294
v  Velocity[Z]              1.5654          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4405          4.3406          4.3632
v  Pressure                 -36.39          360.01          87.635          169.83
v  r11                   0.0010621        0.082017        0.013076        0.018287
v  r22                   0.0011157        0.082607        0.013356        0.018647
v  r33                   0.0016437         0.17432        0.027255        0.037208
v  r12                   -0.010662        0.013599     -0.00023386     -0.00030933
v  r13                   -0.045516        0.052782      9.3319e-05       0.0010139
v  r23                   -0.046695        0.051273      3.0603e-05      0.00057464
v  epsilon                0.069485          271.18          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9919e-05       0.0099181      0.00092528       0.0017428
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017875          5.2787         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85284


 TIME FOR THE TIME STEP            11027:        0.66625E+02

===============================================================


 INSTANT    0.110280000E-01   TIME STEP NUMBER           11028
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.124876980E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267895959E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.944741719E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.124072241E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.471305665E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81388E-03   0.45386E-02 0.19935E+01 
c  Velocity[X]                                      0.13827E-03 
c  Velocity[Y]                                      0.12856E-03 
c  Velocity[Z]                                      0.42718E-02 
c  Pressure     0.36484E-04     132   0.92875E-02   0.25733E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.68119E-08   0.16463E-08 0.98964E-01 
c  r22          0.10853E-01      13   0.58434E-08   0.18038E-08 0.10024E+00 
c  r33          0.21861E-01      15   0.74938E-08   0.12512E-07 0.12616E+00 
c  r12          0.93876E-03      19   0.62914E-08   0.29181E-09 0.59795E+00 
c  r13          0.46678E-02      20   0.67470E-08   0.14764E-08 0.19754E+00 
c  r23          0.39979E-02      19   0.63644E-08   0.12984E-08 0.19861E+00 
c  epsilon      0.10969E+02      11   0.35554E-08   0.99401E-02 0.16678E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84735E-02 0.43473E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61374       0.0052574       0.0015074
v  Velocity[Y]            -0.57344         0.54426         0.00308      0.00087291
v  Velocity[Z]              1.5656          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4405          4.3406          4.3632
v  Pressure                -36.468          360.02           87.66          169.85
v  r11                   0.0010621        0.082012        0.013076        0.018287
v  r22                   0.0011157        0.082605        0.013356        0.018647
v  r33                   0.0016437         0.17434        0.027255        0.037208
v  r12                    -0.01066        0.013596     -0.00023386     -0.00030933
v  r13                   -0.045514         0.05278       9.332e-05       0.0010139
v  r23                   -0.046695         0.05129      3.0604e-05      0.00057464
v  epsilon                0.069486          271.17          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9917e-05       0.0099183      0.00092528       0.0017428
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017875          5.2781         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            11028:        0.67161E+02

===============================================================


 INSTANT    0.110290000E-01   TIME STEP NUMBER           11029
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.303925524E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.167944861E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.170594440E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.120730302E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.897870635E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81244E-03   0.44978E-02 0.19860E+01 
c  Velocity[X]                                      0.13740E-03 
c  Velocity[Y]                                      0.12652E-03 
c  Velocity[Z]                                      0.42338E-02 
c  Pressure     0.36257E-04     133   0.92287E-02   0.25573E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.68358E-08   0.16475E-08 0.99277E-01 
c  r22          0.10853E-01      13   0.56951E-08   0.18274E-08 0.10091E+00 
c  r33          0.21861E-01      15   0.71666E-08   0.12544E-07 0.12648E+00 
c  r12          0.93876E-03      19   0.56740E-08   0.29805E-09 0.60678E+00 
c  r13          0.46678E-02      20   0.69129E-08   0.15168E-08 0.19990E+00 
c  r23          0.39979E-02      19   0.65977E-08   0.12932E-08 0.19878E+00 
c  epsilon      0.10969E+02      11   0.33065E-08   0.99442E-02 0.16581E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.84040E-02 0.43244E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61372       0.0052574       0.0015074
v  Velocity[Y]            -0.57367         0.54404         0.00308      0.00087293
v  Velocity[Z]              1.5655          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4405          4.3406          4.3632
v  Pressure                -36.417          360.03          87.638          169.85
v  r11                   0.0010621        0.082006        0.013076        0.018287
v  r22                   0.0011157        0.082604        0.013356        0.018647
v  r33                   0.0016437         0.17436        0.027255        0.037208
v  r12                   -0.010659        0.013598     -0.00023386     -0.00030933
v  r13                   -0.045519        0.052781       9.332e-05       0.0010139
v  r23                   -0.046696        0.051274      3.0605e-05      0.00057464
v  epsilon                0.069487          271.18          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099183      0.00092529       0.0017428
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017875          5.2778         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85284


 TIME FOR THE TIME STEP            11029:        0.65677E+02

===============================================================


 INSTANT    0.110300000E-01   TIME STEP NUMBER           11030
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122513036E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.390161142E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.570087041E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.216302496E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.419469680E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81317E-03   0.45109E-02 0.19898E+01 
c  Velocity[X]                                      0.13738E-03 
c  Velocity[Y]                                      0.12856E-03 
c  Velocity[Z]                                      0.42449E-02 
c  Pressure     0.36329E-04     133   0.92491E-02   0.25623E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61327E-08   0.16162E-08 0.98799E-01 
c  r22          0.10853E-01      13   0.52601E-08   0.18068E-08 0.10086E+00 
c  r33          0.21861E-01      15   0.70692E-08   0.12328E-07 0.12616E+00 
c  r12          0.93876E-03      18   0.62624E-08   0.29753E-09 0.60688E+00 
c  r13          0.46678E-02      20   0.71009E-08   0.14789E-08 0.19883E+00 
c  r23          0.39979E-02      19   0.66378E-08   0.12789E-08 0.19845E+00 
c  epsilon      0.10969E+02      11   0.33648E-08   0.96283E-02 0.16368E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.83942E-02 0.43180E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61374       0.0052575       0.0015074
v  Velocity[Y]            -0.57353         0.54414         0.00308      0.00087291
v  Velocity[Z]              1.5657          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4405          4.3406          4.3632
v  Pressure                -36.464          359.99          87.632          169.82
v  r11                   0.0010621        0.082005        0.013076        0.018287
v  r22                   0.0011157        0.082602        0.013356        0.018647
v  r33                   0.0016437         0.17438        0.027255        0.037208
v  r12                   -0.010664        0.013589     -0.00023386     -0.00030933
v  r13                   -0.045515        0.052783       9.332e-05       0.0010139
v  r23                   -0.046697        0.051268      3.0605e-05      0.00057464
v  epsilon                0.069489          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099183      0.00092529       0.0017428
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017875          5.2774         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            11030:        0.65942E+02

===============================================================


 INSTANT    0.110310000E-01   TIME STEP NUMBER           11031
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.132634856E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.669103081E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221272680E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.358217671E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.215994468E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81306E-03   0.45136E-02 0.19906E+01 
c  Velocity[X]                                      0.13783E-03 
c  Velocity[Y]                                      0.12804E-03 
c  Velocity[Z]                                      0.42477E-02 
c  Pressure     0.36209E-04     131   0.92169E-02   0.25539E-01 0.00000E+00 
c  r11          0.10586E-01      14   0.51343E-08   0.16601E-08 0.10001E+00 
c  r22          0.10853E-01      13   0.51581E-08   0.18250E-08 0.10093E+00 
c  r33          0.21861E-01      15   0.72440E-08   0.12641E-07 0.12750E+00 
c  r12          0.93876E-03      18   0.64688E-08   0.29811E-09 0.60642E+00 
c  r13          0.46678E-02      20   0.71308E-08   0.15025E-08 0.19980E+00 
c  r23          0.39979E-02      19   0.58029E-08   0.13093E-08 0.20148E+00 
c  epsilon      0.10969E+02      11   0.34454E-08   0.10190E-01 0.17137E+00 
c  TempC        0.25716E+06      16   0.15121E-04   0.84384E-02 0.43403E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6333         0.61373       0.0052574       0.0015074
v  Velocity[Y]            -0.57357         0.54382         0.00308      0.00087295
v  Velocity[Z]              1.5658          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4405          4.3406          4.3632
v  Pressure                -36.391          360.03          87.651          169.86
v  r11                   0.0010621           0.082        0.013076        0.018287
v  r22                   0.0011157        0.082599        0.013356        0.018647
v  r33                   0.0016437          0.1744        0.027255        0.037208
v  r12                   -0.010666        0.013588     -0.00023386     -0.00030933
v  r13                   -0.045514        0.052783       9.332e-05       0.0010139
v  r23                   -0.046699        0.051268      3.0605e-05      0.00057464
v  epsilon                 0.06949          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9917e-05       0.0099184      0.00092529       0.0017428
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017875          5.2775         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71352         0.85284


 TIME FOR THE TIME STEP            11031:        0.66016E+02

===============================================================


 INSTANT    0.110320000E-01   TIME STEP NUMBER           11032
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.127972168E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179895208E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.516687966E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.666191789E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.988383135E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81344E-03   0.45030E-02 0.19856E+01 
c  Velocity[X]                                      0.13668E-03 
c  Velocity[Y]                                      0.12785E-03 
c  Velocity[Z]                                      0.42384E-02 
c  Pressure     0.36107E-04     132   0.91956E-02   0.25467E-01 0.00000E+00 
c  r11          0.10586E-01      14   0.52466E-08   0.16331E-08 0.98783E-01 
c  r22          0.10853E-01      13   0.52424E-08   0.18222E-08 0.10061E+00 
c  r33          0.21861E-01      15   0.61221E-08   0.12570E-07 0.12647E+00 
c  r12          0.93876E-03      18   0.62405E-08   0.29643E-09 0.60435E+00 
c  r13          0.46678E-02      20   0.61970E-08   0.15153E-08 0.19966E+00 
c  r23          0.39979E-02      19   0.69543E-08   0.12885E-08 0.19880E+00 
c  epsilon      0.10969E+02      11   0.33490E-08   0.10181E-01 0.16663E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.83822E-02 0.43183E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61371       0.0052574       0.0015074
v  Velocity[Y]             -0.5734         0.54385         0.00308      0.00087293
v  Velocity[Z]              1.5658          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4405          4.3406          4.3632
v  Pressure                -36.453          360.04          87.648          169.86
v  r11                   0.0010621        0.081996        0.013076        0.018287
v  r22                   0.0011157        0.082599        0.013356        0.018647
v  r33                   0.0016437         0.17437        0.027255        0.037208
v  r12                   -0.010671        0.013585     -0.00023386     -0.00030933
v  r13                   -0.045517        0.052781       9.332e-05       0.0010139
v  r23                   -0.046701        0.051289      3.0605e-05      0.00057464
v  epsilon                0.069491          271.16          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099184      0.00092529       0.0017428
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017875          5.2781         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            11032:        0.66292E+02

===============================================================


 INSTANT    0.110330000E-01   TIME STEP NUMBER           11033
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.297381762E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154447316E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.428254607E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.240520373E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.270659995E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81211E-03   0.45204E-02 0.19900E+01 
c  Velocity[X]                                      0.13814E-03 
c  Velocity[Y]                                      0.12796E-03 
c  Velocity[Z]                                      0.42543E-02 
c  Pressure     0.36308E-04     133   0.92493E-02   0.25608E-01 0.00000E+00 
c  r11          0.10586E-01      14   0.53935E-08   0.16301E-08 0.99585E-01 
c  r22          0.10853E-01      13   0.54389E-08   0.18186E-08 0.10110E+00 
c  r33          0.21861E-01      15   0.58738E-08   0.12383E-07 0.12699E+00 
c  r12          0.93876E-03      18   0.62612E-08   0.29975E-09 0.61111E+00 
c  r13          0.46678E-02      20   0.56715E-08   0.14910E-08 0.20011E+00 
c  r23          0.39979E-02      19   0.71766E-08   0.12782E-08 0.20034E+00 
c  epsilon      0.10969E+02      11   0.34079E-08   0.95210E-02 0.16225E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84006E-02 0.43243E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61376       0.0052574       0.0015074
v  Velocity[Y]            -0.57354         0.54401         0.00308      0.00087291
v  Velocity[Z]              1.5657          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4405          4.3406          4.3632
v  Pressure                -36.425             360          87.628          169.83
v  r11                   0.0010621        0.081995        0.013076        0.018287
v  r22                   0.0011157        0.082599        0.013356        0.018647
v  r33                   0.0016437         0.17433        0.027255        0.037208
v  r12                   -0.010668        0.013579     -0.00023386     -0.00030933
v  r13                   -0.045516        0.052782       9.332e-05       0.0010139
v  r23                   -0.046704        0.051283      3.0605e-05      0.00057464
v  epsilon                0.069492          271.15          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099184      0.00092529       0.0017428
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017875          5.2786         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            11033:        0.66559E+02

===============================================================


 INSTANT    0.110340000E-01   TIME STEP NUMBER           11034
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195829955E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.108694870E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.853967884E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.467087282E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186769272E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81316E-03   0.45030E-02 0.19889E+01 
c  Velocity[X]                                      0.13809E-03 
c  Velocity[Y]                                      0.12847E-03 
c  Velocity[Z]                                      0.42364E-02 
c  Pressure     0.35915E-04     132   0.91399E-02   0.25332E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.69816E-08   0.16730E-08 0.99971E-01 
c  r22          0.10853E-01      13   0.53603E-08   0.18293E-08 0.10096E+00 
c  r33          0.21861E-01      15   0.58523E-08   0.12676E-07 0.12732E+00 
c  r12          0.93876E-03      18   0.55182E-08   0.30393E-09 0.60733E+00 
c  r13          0.46678E-02      19   0.65722E-08   0.15060E-08 0.20018E+00 
c  r23          0.39979E-02      19   0.69350E-08   0.13176E-08 0.20115E+00 
c  epsilon      0.10969E+02      11   0.33787E-08   0.10268E-01 0.16966E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.84388E-02 0.43276E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61375       0.0052575       0.0015075
v  Velocity[Y]            -0.57343         0.54415         0.00308      0.00087295
v  Velocity[Z]              1.5658          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4405          4.3406          4.3632
v  Pressure                 -36.47          359.93          87.606          169.79
v  r11                   0.0010621        0.082007        0.013076        0.018287
v  r22                   0.0011157          0.0826        0.013356        0.018647
v  r33                   0.0016437         0.17433        0.027255        0.037208
v  r12                   -0.010664        0.013567     -0.00023386     -0.00030933
v  r13                   -0.045515        0.052784      9.3321e-05       0.0010139
v  r23                   -0.046707        0.051267      3.0607e-05      0.00057464
v  epsilon                0.069493          271.14          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099184      0.00092529       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017875          5.2786         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85283


 TIME FOR THE TIME STEP            11034:        0.67070E+02

===============================================================


 INSTANT    0.110350000E-01   TIME STEP NUMBER           11035
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.133870428E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.144167992E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.744886732E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.304089204E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123485058E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81329E-03   0.44751E-02 0.19801E+01 
c  Velocity[X]                                      0.13710E-03 
c  Velocity[Y]                                      0.12716E-03 
c  Velocity[Z]                                      0.42109E-02 
c  Pressure     0.36237E-04     132   0.92377E-02   0.25558E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.67121E-08   0.16644E-08 0.99457E-01 
c  r22          0.10853E-01      13   0.51517E-08   0.18575E-08 0.10102E+00 
c  r33          0.21861E-01      15   0.72921E-08   0.12754E-07 0.12688E+00 
c  r12          0.93876E-03      18   0.54646E-08   0.30353E-09 0.60889E+00 
c  r13          0.46678E-02      19   0.73184E-08   0.15140E-08 0.19930E+00 
c  r23          0.39979E-02      19   0.74318E-08   0.12975E-08 0.19880E+00 
c  epsilon      0.10969E+02      11   0.35645E-08   0.10572E-01 0.17025E+00 
c  TempC        0.25716E+06      16   0.15126E-04   0.83825E-02 0.43179E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61372       0.0052575       0.0015074
v  Velocity[Y]             -0.5734         0.54397         0.00308      0.00087294
v  Velocity[Z]              1.5657          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4405          4.3406          4.3632
v  Pressure                -36.417          360.04          87.651          169.87
v  r11                   0.0010621        0.082009        0.013076        0.018287
v  r22                   0.0011157        0.082601        0.013356        0.018647
v  r33                   0.0016438         0.17435        0.027255        0.037208
v  r12                   -0.010662        0.013572     -0.00023386     -0.00030933
v  r13                   -0.045518        0.052784      9.3322e-05       0.0010139
v  r23                   -0.046709        0.051261      3.0606e-05      0.00057464
v  epsilon                0.069494          271.18          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099183      0.00092529       0.0017428
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017875          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            11035:        0.66103E+02

===============================================================


 INSTANT    0.110360000E-01   TIME STEP NUMBER           11036
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.275813032E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130336826E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.843226508E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106061074E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.119943885E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81281E-03   0.45031E-02 0.19884E+01 
c  Velocity[X]                                      0.13726E-03 
c  Velocity[Y]                                      0.12780E-03 
c  Velocity[Z]                                      0.42380E-02 
c  Pressure     0.36237E-04     131   0.92219E-02   0.25558E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.66328E-08   0.16344E-08 0.98759E-01 
c  r22          0.10853E-01      13   0.54502E-08   0.18105E-08 0.10073E+00 
c  r33          0.21861E-01      16   0.65591E-08   0.12405E-07 0.12632E+00 
c  r12          0.93876E-03      18   0.59156E-08   0.29067E-09 0.60065E+00 
c  r13          0.46678E-02      20   0.69174E-08   0.14705E-08 0.19871E+00 
c  r23          0.39979E-02      20   0.57441E-08   0.12784E-08 0.19819E+00 
c  epsilon      0.10969E+02      11   0.34752E-08   0.97996E-02 0.16550E+00 
c  TempC        0.25716E+06      16   0.15176E-04   0.84076E-02 0.43305E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61373       0.0052574       0.0015074
v  Velocity[Y]            -0.57334          0.5441       0.0030799      0.00087285
v  Velocity[Z]              1.5657          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4405          4.3406          4.3632
v  Pressure                -36.473          360.01          87.658          169.85
v  r11                   0.0010621           0.082        0.013076        0.018287
v  r22                   0.0011157        0.082601        0.013356        0.018647
v  r33                   0.0016438         0.17437        0.027255        0.037208
v  r12                   -0.010663        0.013577     -0.00023386     -0.00030933
v  r13                   -0.045515        0.052785      9.3322e-05       0.0010139
v  r23                   -0.046711         0.05129      3.0607e-05      0.00057464
v  epsilon                0.069496           271.2          7.2636          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099182      0.00092529       0.0017428
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017876          5.2787         0.11443         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85283


 TIME FOR THE TIME STEP            11036:        0.65797E+02

===============================================================


 INSTANT    0.110370000E-01   TIME STEP NUMBER           11037
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133833061E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15641E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133616187E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15641E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.357679100E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15641E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.101160441E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15641E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.369244538E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15641E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81164E-03   0.45494E-02 0.19956E+01 
c  Velocity[X]                                      0.13882E-03 
c  Velocity[Y]                                      0.12834E-03 
c  Velocity[Z]                                      0.42822E-02 
c  Pressure     0.36142E-04     133   0.92004E-02   0.25491E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.64194E-08   0.16760E-08 0.99942E-01 
c  r22          0.10853E-01      13   0.52696E-08   0.18270E-08 0.10070E+00 
c  r33          0.21861E-01      16   0.59155E-08   0.12747E-07 0.12744E+00 
c  r12          0.93876E-03      18   0.54204E-08   0.30080E-09 0.60486E+00 
c  r13          0.46678E-02      20   0.64267E-08   0.14975E-08 0.19865E+00 
c  r23          0.39979E-02      20   0.55398E-08   0.13133E-08 0.20077E+00 
c  epsilon      0.10969E+02      11   0.34354E-08   0.10273E-01 0.17173E+00 
c  TempC        0.25716E+06      16   0.15155E-04   0.83965E-02 0.43296E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61372       0.0052574       0.0015074
v  Velocity[Y]            -0.57355          0.5441         0.00308      0.00087289
v  Velocity[Z]              1.5657          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4405          4.3406          4.3632
v  Pressure                -36.385          360.08          87.674          169.89
v  r11                   0.0010621        0.081997        0.013076        0.018287
v  r22                   0.0011157        0.082602        0.013356        0.018647
v  r33                   0.0016438         0.17439        0.027255        0.037208
v  r12                   -0.010661        0.013585     -0.00023386     -0.00030933
v  r13                   -0.045516        0.052786      9.3323e-05       0.0010139
v  r23                   -0.046713        0.051286      3.0608e-05      0.00057464
v  epsilon                0.069497          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05        0.009918      0.00092529       0.0017428
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017876          5.2781         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            11037:        0.67153E+02

===============================================================


 INSTANT    0.110380000E-01   TIME STEP NUMBER           11038
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.287581745E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.386310242E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.695602777E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.415427236E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.228716446E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81498E-03   0.44805E-02 0.19831E+01 
c  Velocity[X]                                      0.13729E-03 
c  Velocity[Y]                                      0.12721E-03 
c  Velocity[Z]                                      0.42160E-02 
c  Pressure     0.36281E-04     132   0.92343E-02   0.25591E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.63844E-08   0.16128E-08 0.98221E-01 
c  r22          0.10853E-01      13   0.55681E-08   0.18175E-08 0.10067E+00 
c  r33          0.21861E-01      15   0.71367E-08   0.12372E-07 0.12561E+00 
c  r12          0.93876E-03      18   0.58029E-08   0.29253E-09 0.59960E+00 
c  r13          0.46678E-02      20   0.60671E-08   0.15042E-08 0.19931E+00 
c  r23          0.39979E-02      20   0.61361E-08   0.12684E-08 0.19631E+00 
c  epsilon      0.10969E+02      11   0.34407E-08   0.97824E-02 0.16496E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.83978E-02 0.43224E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61369       0.0052574       0.0015074
v  Velocity[Y]             -0.5735         0.54417       0.0030799      0.00087285
v  Velocity[Z]              1.5658          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4405          4.3406          4.3632
v  Pressure                -36.445          360.06           87.68          169.88
v  r11                   0.0010621        0.081989        0.013076        0.018287
v  r22                   0.0011157        0.082603        0.013356        0.018647
v  r33                   0.0016438          0.1744        0.027255        0.037208
v  r12                   -0.010661        0.013583     -0.00023386     -0.00030933
v  r13                   -0.045518        0.052787      9.3322e-05       0.0010139
v  r23                   -0.046714        0.051279      3.0607e-05      0.00057464
v  epsilon                0.069498          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9917e-05       0.0099178      0.00092529       0.0017428
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017876           5.278         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            11038:        0.67270E+02

===============================================================


 INSTANT    0.110390000E-01   TIME STEP NUMBER           11039
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.380516215E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151089783E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.225321466E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.243839731E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.165778824E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935012E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11559E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15640E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81190E-03   0.45114E-02 0.19902E+01 
c  Velocity[X]                                      0.13761E-03 
c  Velocity[Y]                                      0.12902E-03 
c  Velocity[Z]                                      0.42448E-02 
c  Pressure     0.36215E-04     133   0.92268E-02   0.25543E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.63336E-08   0.16433E-08 0.98594E-01 
c  r22          0.10853E-01      13   0.56398E-08   0.18483E-08 0.10057E+00 
c  r33          0.21861E-01      15   0.68098E-08   0.12690E-07 0.12611E+00 
c  r12          0.93876E-03      18   0.59786E-08   0.29553E-09 0.60269E+00 
c  r13          0.46678E-02      20   0.59325E-08   0.15203E-08 0.19919E+00 
c  r23          0.39979E-02      20   0.67463E-08   0.12771E-08 0.19648E+00 
c  epsilon      0.10969E+02      11   0.34623E-08   0.10330E-01 0.16662E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.84491E-02 0.43317E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61373       0.0052575       0.0015075
v  Velocity[Y]            -0.57356          0.5443       0.0030798      0.00087283
v  Velocity[Z]              1.5659          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4406          4.3406          4.3632
v  Pressure                -36.418             360          87.633          169.84
v  r11                   0.0010621        0.081989        0.013076        0.018287
v  r22                   0.0011157        0.082605        0.013356        0.018647
v  r33                   0.0016438         0.17437        0.027255        0.037208
v  r12                   -0.010657        0.013592     -0.00023386     -0.00030933
v  r13                   -0.045515        0.052787      9.3322e-05       0.0010139
v  r23                   -0.046715        0.051293      3.0606e-05      0.00057464
v  epsilon                0.069499           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099175      0.00092529       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017876          5.2776         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11039:        0.66929E+02

===============================================================


 INSTANT    0.110400000E-01   TIME STEP NUMBER           11040
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107288319E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.139630678E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.150213803E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.381658290E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.234806984E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81391E-03   0.45197E-02 0.19893E+01 
c  Velocity[X]                                      0.13727E-03 
c  Velocity[Y]                                      0.12862E-03 
c  Velocity[Z]                                      0.42538E-02 
c  Pressure     0.36061E-04     132   0.91849E-02   0.25436E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.64505E-08   0.16472E-08 0.99387E-01 
c  r22          0.10853E-01      13   0.54755E-08   0.18259E-08 0.10071E+00 
c  r33          0.21861E-01      15   0.62677E-08   0.12477E-07 0.12643E+00 
c  r12          0.93876E-03      18   0.56548E-08   0.30674E-09 0.61197E+00 
c  r13          0.46678E-02      19   0.67993E-08   0.14988E-08 0.19926E+00 
c  r23          0.39979E-02      19   0.73479E-08   0.12771E-08 0.19789E+00 
c  epsilon      0.10969E+02      11   0.34848E-08   0.99135E-02 0.16648E+00 
c  TempC        0.25716E+06      16   0.15159E-04   0.83873E-02 0.43212E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61373       0.0052575       0.0015074
v  Velocity[Y]            -0.57346          0.5441       0.0030799      0.00087287
v  Velocity[Z]              1.5656          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4405          4.3406          4.3632
v  Pressure                -36.443          360.01           87.66          169.86
v  r11                   0.0010621        0.081985        0.013076        0.018287
v  r22                   0.0011157        0.082605        0.013356        0.018647
v  r33                   0.0016438         0.17433        0.027255        0.037208
v  r12                   -0.010658        0.013598     -0.00023386     -0.00030933
v  r13                   -0.045514        0.052784      9.3323e-05       0.0010139
v  r23                   -0.046715        0.051275      3.0607e-05      0.00057464
v  epsilon                  0.0695          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099175      0.00092529       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017876          5.2774         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            11040:        0.69976E+02

===============================================================


 INSTANT    0.110410000E-01   TIME STEP NUMBER           11041
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.732551634E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138552726E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.920038519E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935018E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.741728295E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119598592E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10219E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81334E-03   0.44752E-02 0.19790E+01 
c  Velocity[X]                                      0.13608E-03 
c  Velocity[Y]                                      0.12706E-03 
c  Velocity[Z]                                      0.42120E-02 
c  Pressure     0.35852E-04     132   0.91294E-02   0.25287E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.64651E-08   0.16839E-08 0.99910E-01 
c  r22          0.10853E-01      13   0.49881E-08   0.18710E-08 0.10140E+00 
c  r33          0.21861E-01      15   0.60571E-08   0.12856E-07 0.12755E+00 
c  r12          0.93876E-03      18   0.53374E-08   0.30418E-09 0.60656E+00 
c  r13          0.46678E-02      19   0.67584E-08   0.15197E-08 0.20034E+00 
c  r23          0.39979E-02      19   0.65502E-08   0.13115E-08 0.19953E+00 
c  epsilon      0.10969E+02      11   0.35023E-08   0.10371E-01 0.16896E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.83378E-02 0.43111E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61371       0.0052575       0.0015074
v  Velocity[Y]            -0.57361          0.5442       0.0030799      0.00087284
v  Velocity[Z]              1.5656          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4405          4.3406          4.3632
v  Pressure                -36.405          359.98          87.608          169.81
v  r11                   0.0010621         0.08198        0.013076        0.018287
v  r22                   0.0011157          0.0826        0.013356        0.018647
v  r33                   0.0016438         0.17433        0.027255        0.037208
v  r12                   -0.010663        0.013593     -0.00023386     -0.00030933
v  r13                   -0.045518        0.052784      9.3323e-05       0.0010139
v  r23                   -0.046714        0.051264      3.0606e-05      0.00057464
v  epsilon                0.069501          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099175      0.00092529       0.0017428
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017876          5.2774         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            11041:        0.67485E+02

===============================================================


 INSTANT    0.110420000E-01   TIME STEP NUMBER           11042
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.217504239E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.219240816E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117183131E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.351695874E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.127389155E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81296E-03   0.45197E-02 0.19887E+01 
c  Velocity[X]                                      0.13752E-03 
c  Velocity[Y]                                      0.12762E-03 
c  Velocity[Z]                                      0.42545E-02 
c  Pressure     0.36075E-04     133   0.91827E-02   0.25443E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.66827E-08   0.16354E-08 0.98666E-01 
c  r22          0.10853E-01      13   0.48127E-08   0.18068E-08 0.10017E+00 
c  r33          0.21861E-01      15   0.57002E-08   0.12380E-07 0.12559E+00 
c  r12          0.93876E-03      18   0.59146E-08   0.29104E-09 0.59884E+00 
c  r13          0.46678E-02      19   0.57492E-08   0.14674E-08 0.19723E+00 
c  r23          0.39979E-02      19   0.57830E-08   0.12851E-08 0.19731E+00 
c  epsilon      0.10969E+02      11   0.34248E-08   0.96861E-02 0.16369E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.84011E-02 0.43262E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63358         0.61371       0.0052574       0.0015074
v  Velocity[Y]            -0.57358         0.54433       0.0030798      0.00087279
v  Velocity[Z]              1.5656          5.4405          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4405          4.3406          4.3632
v  Pressure                -36.451          359.99          87.643          169.83
v  r11                   0.0010621         0.08197        0.013076        0.018287
v  r22                   0.0011157        0.082601        0.013356        0.018647
v  r33                   0.0016438         0.17434        0.027255        0.037208
v  r12                   -0.010665        0.013594     -0.00023386     -0.00030933
v  r13                   -0.045515        0.052786      9.3323e-05       0.0010139
v  r23                   -0.046713        0.051285      3.0606e-05      0.00057464
v  epsilon                0.069502          271.17          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099176      0.00092529       0.0017428
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017876          5.2776         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11042:        0.66136E+02

===============================================================


 INSTANT    0.110430000E-01   TIME STEP NUMBER           11043
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.257345859E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.572021481E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.450360407E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.854830020E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.537412546E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81285E-03   0.45416E-02 0.19942E+01 
c  Velocity[X]                                      0.13922E-03 
c  Velocity[Y]                                      0.12877E-03 
c  Velocity[Z]                                      0.42736E-02 
c  Pressure     0.36308E-04     133   0.92494E-02   0.25609E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61001E-08   0.16533E-08 0.99462E-01 
c  r22          0.10853E-01      13   0.54669E-08   0.18176E-08 0.10052E+00 
c  r33          0.21861E-01      14   0.66698E-08   0.12603E-07 0.12699E+00 
c  r12          0.93876E-03      18   0.65122E-08   0.29525E-09 0.60519E+00 
c  r13          0.46678E-02      18   0.71293E-08   0.14859E-08 0.19928E+00 
c  r23          0.39979E-02      19   0.50668E-08   0.12925E-08 0.19959E+00 
c  epsilon      0.10969E+02      11   0.30914E-08   0.10312E-01 0.17240E+00 
c  TempC        0.25716E+06      16   0.15127E-04   0.84786E-02 0.43444E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61374       0.0052575       0.0015074
v  Velocity[Y]            -0.57366         0.54405       0.0030799      0.00087283
v  Velocity[Z]              1.5657          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4406          4.3406          4.3632
v  Pressure                -36.399          360.08          87.693          169.91
v  r11                   0.0010621        0.081979        0.013076        0.018287
v  r22                   0.0011157          0.0826        0.013356        0.018647
v  r33                   0.0016438         0.17436        0.027255        0.037208
v  r12                   -0.010663        0.013598     -0.00023386     -0.00030933
v  r13                   -0.045514        0.052785      9.3323e-05       0.0010139
v  r23                   -0.046712        0.051267      3.0606e-05      0.00057464
v  epsilon                0.069503          271.18          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099176      0.00092529       0.0017428
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017877          5.2779         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            11043:        0.67994E+02

===============================================================


 INSTANT    0.110440000E-01   TIME STEP NUMBER           11044
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155182253E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.223685350E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.422791191E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.719681938E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294594803E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81355E-03   0.44802E-02 0.19839E+01 
c  Velocity[X]                                      0.13684E-03 
c  Velocity[Y]                                      0.12684E-03 
c  Velocity[Z]                                      0.42165E-02 
c  Pressure     0.36058E-04     132   0.91739E-02   0.25432E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55236E-08   0.16294E-08 0.98762E-01 
c  r22          0.10853E-01      13   0.50632E-08   0.18155E-08 0.10054E+00 
c  r33          0.21861E-01      14   0.64691E-08   0.12480E-07 0.12643E+00 
c  r12          0.93876E-03      18   0.53301E-08   0.29850E-09 0.60427E+00 
c  r13          0.46678E-02      18   0.72018E-08   0.14931E-08 0.19909E+00 
c  r23          0.39979E-02      19   0.49603E-08   0.12772E-08 0.19781E+00 
c  epsilon      0.10969E+02      11   0.33293E-08   0.98194E-02 0.16614E+00 
c  TempC        0.25716E+06      16   0.15175E-04   0.84026E-02 0.43280E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61371       0.0052574       0.0015074
v  Velocity[Y]            -0.57356         0.54409       0.0030799      0.00087285
v  Velocity[Z]              1.5657          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4406          4.3406          4.3632
v  Pressure                -36.473          360.04          87.659          169.87
v  r11                   0.0010621        0.081978        0.013076        0.018287
v  r22                   0.0011157        0.082604        0.013356        0.018647
v  r33                   0.0016438         0.17438        0.027255        0.037208
v  r12                    -0.01066        0.013603     -0.00023386     -0.00030933
v  r13                   -0.045516        0.052783      9.3323e-05       0.0010139
v  r23                   -0.046711        0.051251      3.0606e-05      0.00057464
v  epsilon                0.069505           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099176      0.00092529       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017877          5.2776         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11044:        0.67816E+02

===============================================================


 INSTANT    0.110450000E-01   TIME STEP NUMBER           11045
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.372900401E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.329942153E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.241352750E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.240453603E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.171649924E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81227E-03   0.45160E-02 0.19887E+01 
c  Velocity[X]                                      0.13728E-03 
c  Velocity[Y]                                      0.12767E-03 
c  Velocity[Z]                                      0.42511E-02 
c  Pressure     0.36194E-04     132   0.92102E-02   0.25528E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60637E-08   0.16195E-08 0.98314E-01 
c  r22          0.10853E-01      13   0.47269E-08   0.18462E-08 0.10049E+00 
c  r33          0.21861E-01      15   0.63419E-08   0.12535E-07 0.12579E+00 
c  r12          0.93876E-03      18   0.49728E-08   0.29689E-09 0.60214E+00 
c  r13          0.46678E-02      19   0.67673E-08   0.15300E-08 0.19980E+00 
c  r23          0.39979E-02      19   0.52896E-08   0.12668E-08 0.19610E+00 
c  epsilon      0.10969E+02      11   0.34891E-08   0.10136E-01 0.16568E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.83870E-02 0.43168E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61374       0.0052575       0.0015075
v  Velocity[Y]             -0.5736         0.54419       0.0030799      0.00087282
v  Velocity[Z]              1.5656          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4406          4.3406          4.3632
v  Pressure                -36.431          359.96          87.602           169.8
v  r11                   0.0010621        0.081978        0.013076        0.018287
v  r22                   0.0011157        0.082606        0.013356        0.018647
v  r33                   0.0016438         0.17439        0.027255        0.037208
v  r12                    -0.01066        0.013603     -0.00023386     -0.00030933
v  r13                   -0.045516         0.05278      9.3323e-05       0.0010139
v  r23                    -0.04671        0.051272      3.0605e-05      0.00057464
v  epsilon                0.069506          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099174      0.00092529       0.0017428
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017877          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            11045:        0.68636E+02

===============================================================


 INSTANT    0.110460000E-01   TIME STEP NUMBER           11046
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.804117467E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168518269E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.401232489E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.303637901E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.173319962E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81319E-03   0.45292E-02 0.19911E+01 
c  Velocity[X]                                      0.13783E-03 
c  Velocity[Y]                                      0.12861E-03 
c  Velocity[Z]                                      0.42627E-02 
c  Pressure     0.36500E-04     132   0.92931E-02   0.25744E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.62026E-08   0.16675E-08 0.99730E-01 
c  r22          0.10853E-01      13   0.48355E-08   0.18344E-08 0.10114E+00 
c  r33          0.21861E-01      15   0.53111E-08   0.12681E-07 0.12743E+00 
c  r12          0.93876E-03      18   0.52761E-08   0.30080E-09 0.60681E+00 
c  r13          0.46678E-02      19   0.69057E-08   0.14997E-08 0.19976E+00 
c  r23          0.39979E-02      19   0.52259E-08   0.13076E-08 0.20021E+00 
c  epsilon      0.10969E+02      11   0.34050E-08   0.10218E-01 0.16847E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.84002E-02 0.43243E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63356         0.61373       0.0052575       0.0015074
v  Velocity[Y]            -0.57351          0.5443       0.0030798      0.00087282
v  Velocity[Z]              1.5654          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4406          4.3406          4.3632
v  Pressure                -36.439             360          87.649          169.84
v  r11                   0.0010621        0.081976        0.013076        0.018287
v  r22                   0.0011158        0.082606        0.013356        0.018647
v  r33                   0.0016438          0.1744        0.027255        0.037208
v  r12                    -0.01066        0.013601     -0.00023386     -0.00030933
v  r13                   -0.045514        0.052777      9.3324e-05       0.0010139
v  r23                   -0.046709        0.051268      3.0605e-05      0.00057464
v  epsilon                0.069507          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099174       0.0009253       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017877          5.2774         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            11046:        0.67205E+02

===============================================================


 INSTANT    0.110470000E-01   TIME STEP NUMBER           11047
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.943372604E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.623897101E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.456110279E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.298004312E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184819279E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81304E-03   0.45085E-02 0.19891E+01 
c  Velocity[X]                                      0.13770E-03 
c  Velocity[Y]                                      0.12782E-03 
c  Velocity[Z]                                      0.42430E-02 
c  Pressure     0.36056E-04     131   0.91839E-02   0.25431E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57953E-08   0.16155E-08 0.98707E-01 
c  r22          0.10853E-01      13   0.51686E-08   0.18410E-08 0.10155E+00 
c  r33          0.21861E-01      14   0.70895E-08   0.12399E-07 0.12683E+00 
c  r12          0.93876E-03      18   0.57512E-08   0.29940E-09 0.60639E+00 
c  r13          0.46678E-02      19   0.66523E-08   0.14863E-08 0.19977E+00 
c  r23          0.39979E-02      19   0.52606E-08   0.12734E-08 0.19802E+00 
c  epsilon      0.10969E+02      11   0.33571E-08   0.94904E-02 0.16351E+00 
c  TempC        0.25716E+06      16   0.15118E-04   0.83756E-02 0.43209E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63332         0.61372       0.0052575       0.0015075
v  Velocity[Y]            -0.57351         0.54412       0.0030798      0.00087283
v  Velocity[Z]              1.5656          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4406          4.3406          4.3632
v  Pressure                -36.407          360.04          87.646          169.86
v  r11                   0.0010621        0.081972        0.013076        0.018287
v  r22                   0.0011158        0.082604        0.013356        0.018647
v  r33                   0.0016439         0.17437        0.027255        0.037208
v  r12                   -0.010663        0.013601     -0.00023386     -0.00030933
v  r13                   -0.045517        0.052775      9.3325e-05       0.0010139
v  r23                   -0.046708         0.05126      3.0606e-05      0.00057464
v  epsilon                0.069508          271.18          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9917e-05       0.0099174       0.0009253       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017877          5.2767         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767         0.71352         0.85284


 TIME FOR THE TIME STEP            11047:        0.67064E+02

===============================================================


 INSTANT    0.110480000E-01   TIME STEP NUMBER           11048
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.255794688E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.366683412E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934906E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.305297854E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.352024248E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.247176852E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81369E-03   0.45238E-02 0.19891E+01 
c  Velocity[X]                                      0.13699E-03 
c  Velocity[Y]                                      0.12755E-03 
c  Velocity[Z]                                      0.42593E-02 
c  Pressure     0.36341E-04     133   0.92513E-02   0.25632E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55111E-08   0.16449E-08 0.99815E-01 
c  r22          0.10853E-01      13   0.50342E-08   0.18675E-08 0.10208E+00 
c  r33          0.21861E-01      14   0.66814E-08   0.12651E-07 0.12801E+00 
c  r12          0.93876E-03      17   0.68997E-08   0.30238E-09 0.61325E+00 
c  r13          0.46678E-02      19   0.54262E-08   0.14904E-08 0.20047E+00 
c  r23          0.39979E-02      19   0.52345E-08   0.12853E-08 0.19976E+00 
c  epsilon      0.10969E+02      11   0.31162E-08   0.96667E-02 0.16429E+00 
c  TempC        0.25716E+06      16   0.15179E-04   0.83855E-02 0.43239E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61376       0.0052575       0.0015075
v  Velocity[Y]            -0.57345         0.54425       0.0030799      0.00087282
v  Velocity[Z]              1.5655          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4406          4.3406          4.3632
v  Pressure                -36.435          360.03          87.667          169.87
v  r11                   0.0010621        0.081966        0.013076        0.018287
v  r22                   0.0011158        0.082601        0.013356        0.018647
v  r33                   0.0016439         0.17433        0.027255        0.037208
v  r12                   -0.010663        0.013597     -0.00023386     -0.00030933
v  r13                   -0.045515        0.052775      9.3325e-05       0.0010139
v  r23                   -0.046708        0.051253      3.0605e-05      0.00057464
v  epsilon                0.069509           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099173       0.0009253       0.0017428
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017877          5.2772         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85284


 TIME FOR THE TIME STEP            11048:        0.66158E+02

===============================================================


 INSTANT    0.110490000E-01   TIME STEP NUMBER           11049
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.342680332E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.219626039E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.230397070E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205782165E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.342600111E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81211E-03   0.45172E-02 0.19920E+01 
c  Velocity[X]                                      0.13867E-03 
c  Velocity[Y]                                      0.12792E-03 
c  Velocity[Z]                                      0.42506E-02 
c  Pressure     0.36483E-04     131   0.92812E-02   0.25733E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57477E-08   0.16315E-08 0.99504E-01 
c  r22          0.10853E-01      13   0.54614E-08   0.18236E-08 0.10112E+00 
c  r33          0.21861E-01      14   0.70018E-08   0.12505E-07 0.12738E+00 
c  r12          0.93876E-03      18   0.59181E-08   0.29887E-09 0.60733E+00 
c  r13          0.46678E-02      19   0.59493E-08   0.14957E-08 0.19996E+00 
c  r23          0.39979E-02      19   0.51100E-08   0.12776E-08 0.19906E+00 
c  epsilon      0.10969E+02      11   0.32349E-08   0.99005E-02 0.16872E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.84441E-02 0.43367E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61376       0.0052574       0.0015075
v  Velocity[Y]             -0.5736          0.5443       0.0030799      0.00087286
v  Velocity[Z]              1.5658          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4406          4.3406          4.3632
v  Pressure                -36.409          360.03          87.645          169.85
v  r11                   0.0010621        0.081962        0.013076        0.018287
v  r22                   0.0011158          0.0826        0.013356        0.018647
v  r33                   0.0016439         0.17435        0.027255        0.037208
v  r12                    -0.01066        0.013598     -0.00023386     -0.00030933
v  r13                   -0.045516        0.052777      9.3326e-05       0.0010139
v  r23                   -0.046707        0.051281      3.0605e-05      0.00057464
v  epsilon                 0.06951          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099173       0.0009253       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017877          5.2776         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85283


 TIME FOR THE TIME STEP            11049:        0.67259E+02

===============================================================


 INSTANT    0.110500000E-01   TIME STEP NUMBER           11050
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.744551985E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201420164E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.493816361E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.339089280E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.574605261E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81297E-03   0.45014E-02 0.19859E+01 
c  Velocity[X]                                      0.13638E-03 
c  Velocity[Y]                                      0.12725E-03 
c  Velocity[Z]                                      0.42378E-02 
c  Pressure     0.36068E-04     133   0.91816E-02   0.25441E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.64144E-08   0.16531E-08 0.99169E-01 
c  r22          0.10853E-01      13   0.56415E-08   0.18428E-08 0.10119E+00 
c  r33          0.21861E-01      15   0.71557E-08   0.12623E-07 0.12641E+00 
c  r12          0.93876E-03      18   0.53090E-08   0.30238E-09 0.60754E+00 
c  r13          0.46678E-02      19   0.70923E-08   0.14991E-08 0.19899E+00 
c  r23          0.39980E-02      18   0.64175E-08   0.12826E-08 0.19707E+00 
c  epsilon      0.10969E+02      11   0.34132E-08   0.99310E-02 0.16507E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.83810E-02 0.43166E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63335         0.61374       0.0052575       0.0015075
v  Velocity[Y]            -0.57354         0.54436       0.0030798      0.00087285
v  Velocity[Z]              1.5658          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4406          4.3406          4.3632
v  Pressure                -36.437          360.08           87.69           169.9
v  r11                   0.0010621        0.081963        0.013076        0.018287
v  r22                   0.0011158          0.0826        0.013356        0.018647
v  r33                   0.0016439         0.17435        0.027255        0.037208
v  r12                   -0.010658        0.013597     -0.00023386     -0.00030933
v  r13                   -0.045517         0.05278      9.3326e-05       0.0010139
v  r23                   -0.046707        0.051267      3.0606e-05      0.00057464
v  epsilon                0.069511          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099174       0.0009253       0.0017428
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017877          5.2776         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11050:        0.68186E+02

===============================================================


 INSTANT    0.110510000E-01   TIME STEP NUMBER           11051
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166390870E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.326161789E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.715884027E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.162149255E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.565786963E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81273E-03   0.45010E-02 0.19870E+01 
c  Velocity[X]                                      0.13730E-03 
c  Velocity[Y]                                      0.12798E-03 
c  Velocity[Z]                                      0.42357E-02 
c  Pressure     0.36054E-04     132   0.91761E-02   0.25430E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58689E-08   0.16642E-08 0.99199E-01 
c  r22          0.10853E-01      13   0.55847E-08   0.18511E-08 0.10122E+00 
c  r33          0.21861E-01      15   0.55221E-08   0.12654E-07 0.12654E+00 
c  r12          0.93876E-03      18   0.53101E-08   0.30248E-09 0.60857E+00 
c  r13          0.46678E-02      19   0.53856E-08   0.14980E-08 0.19891E+00 
c  r23          0.39979E-02      19   0.54729E-08   0.13004E-08 0.19844E+00 
c  epsilon      0.10969E+02      11   0.35089E-08   0.10206E-01 0.16790E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.83953E-02 0.43194E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61377       0.0052574       0.0015074
v  Velocity[Y]            -0.57357         0.54445       0.0030799      0.00087287
v  Velocity[Z]              1.5657          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4406          4.3406          4.3632
v  Pressure                -36.381          360.02          87.627          169.83
v  r11                   0.0010621        0.081962        0.013076        0.018287
v  r22                   0.0011158        0.082597        0.013356        0.018647
v  r33                   0.0016439         0.17437        0.027255        0.037208
v  r12                   -0.010662        0.013597     -0.00023386     -0.00030933
v  r13                   -0.045515        0.052783      9.3327e-05       0.0010139
v  r23                   -0.046706        0.051259      3.0605e-05      0.00057464
v  epsilon                0.069512          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099174       0.0009253       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017878          5.2773         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            11051:        0.67298E+02

===============================================================


 INSTANT    0.110520000E-01   TIME STEP NUMBER           11052
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.223586661E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.337093232E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.300714998E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.326540241E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110113509E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81288E-03   0.45223E-02 0.19913E+01 
c  Velocity[X]                                      0.13828E-03 
c  Velocity[Y]                                      0.12886E-03 
c  Velocity[Z]                                      0.42552E-02 
c  Pressure     0.35962E-04     132   0.91570E-02   0.25365E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58904E-08   0.16466E-08 0.99188E-01 
c  r22          0.10853E-01      13   0.56018E-08   0.18519E-08 0.10159E+00 
c  r33          0.21861E-01      15   0.54338E-08   0.12609E-07 0.12714E+00 
c  r12          0.93876E-03      18   0.55864E-08   0.30294E-09 0.60850E+00 
c  r13          0.46678E-02      19   0.54975E-08   0.14982E-08 0.19950E+00 
c  r23          0.39980E-02      19   0.53290E-08   0.13024E-08 0.19981E+00 
c  epsilon      0.10969E+02      11   0.34548E-08   0.98025E-02 0.16502E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.84299E-02 0.43335E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347          0.6138       0.0052575       0.0015074
v  Velocity[Y]            -0.57352          0.5442       0.0030799      0.00087286
v  Velocity[Z]              1.5656          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4406          4.3406          4.3632
v  Pressure                -36.458             360          87.627          169.82
v  r11                   0.0010621        0.081966        0.013076        0.018287
v  r22                   0.0011158        0.082601        0.013356        0.018647
v  r33                   0.0016439         0.17439        0.027255        0.037208
v  r12                   -0.010659        0.013601     -0.00023386     -0.00030933
v  r13                   -0.045513        0.052783      9.3327e-05       0.0010139
v  r23                   -0.046706         0.05126      3.0605e-05      0.00057464
v  epsilon                0.069514          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099175       0.0009253       0.0017428
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017877          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            11052:        0.66387E+02

===============================================================


 INSTANT    0.110530000E-01   TIME STEP NUMBER           11053
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.706306676E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.377820363E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.110576943E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.784220285E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.287148568E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81365E-03   0.44917E-02 0.19837E+01 
c  Velocity[X]                                      0.13714E-03 
c  Velocity[Y]                                      0.12756E-03 
c  Velocity[Z]                                      0.42270E-02 
c  Pressure     0.36370E-04     133   0.92504E-02   0.25653E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53520E-08   0.16737E-08 0.99961E-01 
c  r22          0.10853E-01      13   0.53283E-08   0.18703E-08 0.10185E+00 
c  r33          0.21861E-01      15   0.54073E-08   0.12872E-07 0.12830E+00 
c  r12          0.93876E-03      18   0.55426E-08   0.29528E-09 0.60419E+00 
c  r13          0.46678E-02      18   0.71230E-08   0.15115E-08 0.20025E+00 
c  r23          0.39980E-02      18   0.64638E-08   0.12921E-08 0.20046E+00 
c  epsilon      0.10969E+02      11   0.34934E-08   0.10302E-01 0.16857E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.83585E-02 0.43166E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61376       0.0052574       0.0015075
v  Velocity[Y]            -0.57354         0.54426       0.0030799      0.00087286
v  Velocity[Z]              1.5657          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4406          4.3406          4.3632
v  Pressure                -36.441          360.05          87.664          169.88
v  r11                   0.0010621        0.081986        0.013076        0.018287
v  r22                   0.0011158        0.082603        0.013356        0.018647
v  r33                   0.0016439          0.1744        0.027255        0.037208
v  r12                   -0.010656        0.013598     -0.00023386     -0.00030933
v  r13                   -0.045517        0.052781      9.3326e-05       0.0010139
v  r23                   -0.046706        0.051287      3.0604e-05      0.00057464
v  epsilon                0.069515          271.25          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9917e-05       0.0099177       0.0009253       0.0017428
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017878          5.2775         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71352         0.85284


 TIME FOR THE TIME STEP            11053:        0.66328E+02

===============================================================


 INSTANT    0.110540000E-01   TIME STEP NUMBER           11054
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.268601700E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.809352388E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.258858436E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.482518785E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.538626035E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81222E-03   0.45263E-02 0.19900E+01 
c  Velocity[X]                                      0.13841E-03 
c  Velocity[Y]                                      0.12755E-03 
c  Velocity[Z]                                      0.42603E-02 
c  Pressure     0.36086E-04     132   0.91885E-02   0.25452E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53996E-08   0.16542E-08 0.99564E-01 
c  r22          0.10853E-01      13   0.47693E-08   0.18540E-08 0.10158E+00 
c  r33          0.21861E-01      15   0.53745E-08   0.12707E-07 0.12769E+00 
c  r12          0.93877E-03      18   0.57267E-08   0.29643E-09 0.60499E+00 
c  r13          0.46678E-02      19   0.60189E-08   0.15052E-08 0.19963E+00 
c  r23          0.39980E-02      19   0.63267E-08   0.12908E-08 0.19960E+00 
c  epsilon      0.10969E+02      11   0.35079E-08   0.10103E-01 0.16780E+00 
c  TempC        0.25716E+06      16   0.15185E-04   0.84293E-02 0.43272E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61378       0.0052574       0.0015074
v  Velocity[Y]            -0.57344         0.54436       0.0030798      0.00087281
v  Velocity[Z]              1.5655          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4406          4.3406          4.3632
v  Pressure                -36.434          359.94          87.617          169.79
v  r11                   0.0010621        0.081995        0.013076        0.018287
v  r22                   0.0011158        0.082604        0.013356        0.018647
v  r33                   0.0016439         0.17436        0.027255        0.037208
v  r12                   -0.010663        0.013597     -0.00023386     -0.00030933
v  r13                   -0.045514        0.052781      9.3326e-05       0.0010139
v  r23                   -0.046706        0.051272      3.0604e-05      0.00057464
v  epsilon                0.069516          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9917e-05       0.0099178       0.0009253       0.0017428
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb             0.0017878          5.2766         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71352         0.85284


 TIME FOR THE TIME STEP            11054:        0.65428E+02

===============================================================


 INSTANT    0.110550000E-01   TIME STEP NUMBER           11055
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.165231675E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.606864143E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.132189201E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.354674885E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.543549606E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81256E-03   0.45304E-02 0.19909E+01 
c  Velocity[X]                                      0.13865E-03 
c  Velocity[Y]                                      0.12823E-03 
c  Velocity[Z]                                      0.42635E-02 
c  Pressure     0.36393E-04     133   0.92592E-02   0.25669E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55454E-08   0.16481E-08 0.99740E-01 
c  r22          0.10853E-01      13   0.48478E-08   0.18118E-08 0.10075E+00 
c  r33          0.21861E-01      15   0.55860E-08   0.12445E-07 0.12725E+00 
c  r12          0.93877E-03      18   0.59508E-08   0.29544E-09 0.60542E+00 
c  r13          0.46678E-02      19   0.65422E-08   0.14770E-08 0.19908E+00 
c  r23          0.39980E-02      19   0.68436E-08   0.12790E-08 0.19933E+00 
c  epsilon      0.10969E+02      11   0.33495E-08   0.98562E-02 0.16966E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.84533E-02 0.43403E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61378       0.0052574       0.0015074
v  Velocity[Y]            -0.57365         0.54416       0.0030799      0.00087282
v  Velocity[Z]              1.5654          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4407          4.3406          4.3632
v  Pressure                  -36.4          360.09          87.687          169.92
v  r11                   0.0010621        0.081994        0.013076        0.018287
v  r22                   0.0011158        0.082603        0.013356        0.018647
v  r33                   0.0016439         0.17433        0.027255        0.037208
v  r12                   -0.010661        0.013598     -0.00023386     -0.00030933
v  r13                   -0.045513        0.052778      9.3327e-05       0.0010139
v  r23                   -0.046705        0.051257      3.0604e-05      0.00057464
v  epsilon                0.069517          271.16          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099179       0.0009253       0.0017428
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017878          5.2769         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71352         0.85284


 TIME FOR THE TIME STEP            11055:        0.65643E+02

===============================================================


 INSTANT    0.110560000E-01   TIME STEP NUMBER           11056
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.283391262E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183107042E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107500029E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.367277904E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.108350127E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81436E-03   0.44774E-02 0.19797E+01 
c  Velocity[X]                                      0.13592E-03 
c  Velocity[Y]                                      0.12655E-03 
c  Velocity[Z]                                      0.42149E-02 
c  Pressure     0.36007E-04     132   0.91578E-02   0.25397E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53220E-08   0.16343E-08 0.98731E-01 
c  r22          0.10853E-01      13   0.51045E-08   0.18113E-08 0.10028E+00 
c  r33          0.21861E-01      14   0.71167E-08   0.12478E-07 0.12619E+00 
c  r12          0.93877E-03      18   0.56060E-08   0.29444E-09 0.60310E+00 
c  r13          0.46678E-02      19   0.71716E-08   0.14853E-08 0.19884E+00 
c  r23          0.39980E-02      19   0.69020E-08   0.12833E-08 0.19794E+00 
c  epsilon      0.10969E+02      11   0.32651E-08   0.98425E-02 0.16496E+00 
c  TempC        0.25716E+06      16   0.15193E-04   0.83860E-02 0.43213E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61375       0.0052574       0.0015074
v  Velocity[Y]            -0.57341         0.54424       0.0030798      0.00087281
v  Velocity[Z]              1.5656          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4407          4.3406          4.3632
v  Pressure                -36.447          360.03          87.678          169.88
v  r11                   0.0010621        0.082011        0.013076        0.018287
v  r22                   0.0011158        0.082603        0.013356        0.018647
v  r33                   0.0016439         0.17433        0.027255        0.037208
v  r12                   -0.010662        0.013591     -0.00023386     -0.00030933
v  r13                   -0.045515        0.052779      9.3327e-05       0.0010139
v  r23                   -0.046706         0.05128      3.0604e-05      0.00057464
v  epsilon                0.069518          271.16          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9917e-05       0.0099179       0.0009253       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017878          5.2778         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85284


 TIME FOR THE TIME STEP            11056:        0.66074E+02

===============================================================


 INSTANT    0.110570000E-01   TIME STEP NUMBER           11057
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285236734E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.238833612E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158013778E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.278678251E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.230016046E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81231E-03   0.45204E-02 0.19909E+01 
c  Velocity[X]                                      0.13810E-03 
c  Velocity[Y]                                      0.12789E-03 
c  Velocity[Z]                                      0.42544E-02 
c  Pressure     0.36154E-04     132   0.92055E-02   0.25499E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57502E-08   0.16287E-08 0.98747E-01 
c  r22          0.10853E-01      13   0.55607E-08   0.18374E-08 0.10105E+00 
c  r33          0.21861E-01      15   0.59937E-08   0.12559E-07 0.12689E+00 
c  r12          0.93877E-03      18   0.54737E-08   0.30119E-09 0.60554E+00 
c  r13          0.46678E-02      19   0.70055E-08   0.15180E-08 0.19954E+00 
c  r23          0.39980E-02      19   0.68164E-08   0.12929E-08 0.19877E+00 
c  epsilon      0.10969E+02      11   0.33795E-08   0.97615E-02 0.16290E+00 
c  TempC        0.25716E+06      16   0.15166E-04   0.84058E-02 0.43305E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61375       0.0052574       0.0015075
v  Velocity[Y]            -0.57346         0.54439       0.0030798       0.0008728
v  Velocity[Z]              1.5658          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4407          4.3406          4.3632
v  Pressure                -36.411          359.99          87.628          169.83
v  r11                   0.0010621        0.082013        0.013076        0.018287
v  r22                   0.0011158        0.082602        0.013356        0.018647
v  r33                   0.0016439         0.17435        0.027255        0.037208
v  r12                   -0.010662        0.013592     -0.00023386     -0.00030933
v  r13                   -0.045514        0.052782      9.3328e-05       0.0010139
v  r23                   -0.046705        0.051267      3.0604e-05      0.00057464
v  epsilon                0.069519           271.2          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099179       0.0009253       0.0017428
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017878          5.2783         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71352         0.85284


 TIME FOR THE TIME STEP            11057:        0.67217E+02

===============================================================


 INSTANT    0.110580000E-01   TIME STEP NUMBER           11058
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115724649E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.344630713E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.655811463E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.576783776E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181825368E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81329E-03   0.45169E-02 0.19899E+01 
c  Velocity[X]                                      0.13826E-03 
c  Velocity[Y]                                      0.12809E-03 
c  Velocity[Z]                                      0.42505E-02 
c  Pressure     0.36164E-04     133   0.92056E-02   0.25508E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55096E-08   0.16825E-08 0.10032E+00 
c  r22          0.10853E-01      13   0.53934E-08   0.18189E-08 0.10095E+00 
c  r33          0.21861E-01      15   0.57512E-08   0.12597E-07 0.12769E+00 
c  r12          0.93877E-03      18   0.52362E-08   0.30080E-09 0.60862E+00 
c  r13          0.46678E-02      19   0.68371E-08   0.14759E-08 0.19929E+00 
c  r23          0.39980E-02      18   0.70154E-08   0.13106E-08 0.20089E+00 
c  epsilon      0.10969E+02      11   0.33951E-08   0.97173E-02 0.16394E+00 
c  TempC        0.25716E+06      16   0.15124E-04   0.84709E-02 0.43380E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61375       0.0052574       0.0015075
v  Velocity[Y]            -0.57349         0.54424       0.0030798      0.00087278
v  Velocity[Z]              1.5657          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4406          4.3406          4.3632
v  Pressure                -36.442          359.98          87.629          169.82
v  r11                   0.0010621        0.082013        0.013076        0.018287
v  r22                   0.0011158        0.082603        0.013356        0.018647
v  r33                    0.001644         0.17436        0.027255        0.037208
v  r12                    -0.01066        0.013595     -0.00023386     -0.00030933
v  r13                   -0.045513        0.052781      9.3329e-05       0.0010139
v  r23                   -0.046706         0.05125      3.0604e-05      0.00057464
v  epsilon                 0.06952           271.2          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099176       0.0009253       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017878          5.2776         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11058:        0.66797E+02

===============================================================


 INSTANT    0.110590000E-01   TIME STEP NUMBER           11059
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.303196340E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130063197E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.923845112E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.447764291E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.338286289E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81322E-03   0.45018E-02 0.19861E+01 
c  Velocity[X]                                      0.13759E-03 
c  Velocity[Y]                                      0.12798E-03 
c  Velocity[Z]                                      0.42362E-02 
c  Pressure     0.36416E-04     133   0.92738E-02   0.25685E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52391E-08   0.16156E-08 0.98368E-01 
c  r22          0.10853E-01      13   0.57800E-08   0.18287E-08 0.10078E+00 
c  r33          0.21861E-01      15   0.62671E-08   0.12500E-07 0.12642E+00 
c  r12          0.93877E-03      18   0.61569E-08   0.29673E-09 0.60360E+00 
c  r13          0.46678E-02      20   0.58750E-08   0.15132E-08 0.19991E+00 
c  r23          0.39980E-02      19   0.62074E-08   0.12665E-08 0.19654E+00 
c  epsilon      0.10969E+02      11   0.34555E-08   0.10089E-01 0.16698E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.83724E-02 0.43108E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61372       0.0052574       0.0015075
v  Velocity[Y]            -0.57351         0.54417       0.0030798      0.00087279
v  Velocity[Z]              1.5657          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4406          4.3406          4.3632
v  Pressure                -36.422          360.04          87.631          169.85
v  r11                   0.0010621        0.082004        0.013076        0.018287
v  r22                   0.0011158        0.082602        0.013356        0.018647
v  r33                    0.001644         0.17438        0.027255        0.037208
v  r12                   -0.010658        0.013591     -0.00023386     -0.00030933
v  r13                   -0.045515        0.052779      9.3329e-05       0.0010139
v  r23                   -0.046706        0.051242      3.0603e-05      0.00057464
v  epsilon                0.069522          271.22          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099174       0.0009253       0.0017428
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017878          5.2777         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            11059:        0.65512E+02

===============================================================


 INSTANT    0.110600000E-01   TIME STEP NUMBER           11060
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.326607094E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155145474E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.996325184E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.866164438E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.333597814E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81337E-03   0.45080E-02 0.19888E+01 
c  Velocity[X]                                      0.13692E-03 
c  Velocity[Y]                                      0.12797E-03 
c  Velocity[Z]                                      0.42431E-02 
c  Pressure     0.36522E-04     133   0.92855E-02   0.25760E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55126E-08   0.16241E-08 0.99413E-01 
c  r22          0.10853E-01      13   0.56765E-08   0.17949E-08 0.10044E+00 
c  r33          0.21861E-01      15   0.59027E-08   0.12292E-07 0.12663E+00 
c  r12          0.93877E-03      18   0.67180E-08   0.29611E-09 0.60622E+00 
c  r13          0.46678E-02      19   0.62972E-08   0.14853E-08 0.19917E+00 
c  r23          0.39980E-02      18   0.70623E-08   0.12732E-08 0.19893E+00 
c  epsilon      0.10969E+02      11   0.33996E-08   0.94018E-02 0.16292E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.83630E-02 0.43158E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63355         0.61373       0.0052575       0.0015075
v  Velocity[Y]            -0.57348         0.54423       0.0030797      0.00087276
v  Velocity[Z]              1.5656          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4406          4.3406          4.3632
v  Pressure                -36.456          360.03          87.668          169.86
v  r11                   0.0010621        0.082007        0.013076        0.018287
v  r22                   0.0011158        0.082601        0.013356        0.018647
v  r33                    0.001644         0.17439        0.027255        0.037208
v  r12                    -0.01066        0.013592     -0.00023386     -0.00030933
v  r13                   -0.045513        0.052778       9.333e-05       0.0010139
v  r23                   -0.046706        0.051267      3.0603e-05      0.00057464
v  epsilon                0.069523          271.22          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9912e-05       0.0099175       0.0009253       0.0017428
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017879          5.2773         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            11060:        0.67451E+02

===============================================================


 INSTANT    0.110610000E-01   TIME STEP NUMBER           11061
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.853836230E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.235841088E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.118160347E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935014E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.316208327E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168001710E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81286E-03   0.45188E-02 0.19913E+01 
c  Velocity[X]                                      0.13812E-03 
c  Velocity[Y]                                      0.12757E-03 
c  Velocity[Z]                                      0.42532E-02 
c  Pressure     0.36001E-04     134   0.91673E-02   0.25393E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51753E-08   0.16314E-08 0.99428E-01 
c  r22          0.10853E-01      13   0.58299E-08   0.17797E-08 0.10002E+00 
c  r33          0.21861E-01      15   0.71488E-08   0.12344E-07 0.12666E+00 
c  r12          0.93877E-03      18   0.74498E-08   0.29431E-09 0.60537E+00 
c  r13          0.46678E-02      19   0.72911E-08   0.14587E-08 0.19857E+00 
c  r23          0.39980E-02      19   0.58848E-08   0.12775E-08 0.19928E+00 
c  epsilon      0.10969E+02      11   0.33827E-08   0.99169E-02 0.16798E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.83906E-02 0.43257E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61375       0.0052575       0.0015075
v  Velocity[Y]            -0.57351         0.54434       0.0030798      0.00087279
v  Velocity[Z]              1.5655          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4406          4.3406          4.3632
v  Pressure                -36.399          360.03          87.637          169.85
v  r11                   0.0010621        0.082008        0.013076        0.018287
v  r22                   0.0011158          0.0826        0.013356        0.018647
v  r33                    0.001644          0.1744        0.027255        0.037208
v  r12                   -0.010662        0.013594     -0.00023386     -0.00030933
v  r13                   -0.045513         0.05278       9.333e-05       0.0010139
v  r23                   -0.046706        0.051264      3.0604e-05      0.00057464
v  epsilon                0.069524          271.23          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099176       0.0009253       0.0017428
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017879          5.2766         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71352         0.85284


 TIME FOR THE TIME STEP            11061:        0.67075E+02

===============================================================


 INSTANT    0.110620000E-01   TIME STEP NUMBER           11062
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.115928748E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.185559059E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.234311512E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.804843378E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.237319418E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81365E-03   0.44846E-02 0.19833E+01 
c  Velocity[X]                                      0.13718E-03 
c  Velocity[Y]                                      0.12824E-03 
c  Velocity[Z]                                      0.42192E-02 
c  Pressure     0.36454E-04     133   0.92714E-02   0.25712E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55522E-08   0.16218E-08 0.99005E-01 
c  r22          0.10853E-01      13   0.61847E-08   0.18146E-08 0.10084E+00 
c  r33          0.21861E-01      15   0.73769E-08   0.12485E-07 0.12679E+00 
c  r12          0.93877E-03      19   0.58186E-08   0.29492E-09 0.60553E+00 
c  r13          0.46678E-02      20   0.60442E-08   0.15049E-08 0.20028E+00 
c  r23          0.39980E-02      18   0.71287E-08   0.12828E-08 0.19843E+00 
c  epsilon      0.10969E+02      11   0.34356E-08   0.99081E-02 0.16636E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.83339E-02 0.43089E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61373       0.0052574       0.0015075
v  Velocity[Y]            -0.57334         0.54411       0.0030797      0.00087278
v  Velocity[Z]              1.5658          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4406          4.3406          4.3632
v  Pressure                 -36.46          360.04          87.667          169.87
v  r11                   0.0010621        0.082006        0.013076        0.018287
v  r22                   0.0011158        0.082599        0.013356        0.018647
v  r33                    0.001644         0.17436        0.027255        0.037208
v  r12                   -0.010667        0.013589     -0.00023386     -0.00030933
v  r13                   -0.045515        0.052781       9.333e-05       0.0010139
v  r23                   -0.046706        0.051251      3.0603e-05      0.00057464
v  epsilon                0.069525          271.22          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9912e-05       0.0099176       0.0009253       0.0017428
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017879          5.2768         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71352         0.85284


 TIME FOR THE TIME STEP            11062:        0.67234E+02

===============================================================


 INSTANT    0.110630000E-01   TIME STEP NUMBER           11063
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.771852206E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.331848900E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.919655663E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173473480E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.355266514E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81210E-03   0.45430E-02 0.19978E+01 
c  Velocity[X]                                      0.13834E-03 
c  Velocity[Y]                                      0.12812E-03 
c  Velocity[Z]                                      0.42766E-02 
c  Pressure     0.36744E-04     131   0.93573E-02   0.25916E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60239E-08   0.16198E-08 0.99362E-01 
c  r22          0.10853E-01      13   0.61782E-08   0.18415E-08 0.10136E+00 
c  r33          0.21861E-01      15   0.71511E-08   0.12395E-07 0.12709E+00 
c  r12          0.93877E-03      18   0.71244E-08   0.30730E-09 0.61250E+00 
c  r13          0.46678E-02      20   0.61162E-08   0.14983E-08 0.19966E+00 
c  r23          0.39980E-02      18   0.71092E-08   0.12671E-08 0.19852E+00 
c  epsilon      0.10969E+02      11   0.33107E-08   0.97455E-02 0.16465E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84392E-02 0.43358E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61374       0.0052575       0.0015075
v  Velocity[Y]            -0.57355          0.5442       0.0030797      0.00087279
v  Velocity[Z]              1.5657          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4406          4.3406          4.3632
v  Pressure                -36.384          360.01          87.643          169.85
v  r11                   0.0010621        0.082004        0.013076        0.018287
v  r22                   0.0011158        0.082593        0.013356        0.018647
v  r33                    0.001644         0.17432        0.027255        0.037208
v  r12                   -0.010666        0.013591     -0.00023386     -0.00030933
v  r13                   -0.045513        0.052782      9.3331e-05       0.0010139
v  r23                   -0.046706        0.051264      3.0603e-05      0.00057464
v  epsilon                0.069526          271.24          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099177       0.0009253       0.0017428
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017879          5.2773         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85283


 TIME FOR THE TIME STEP            11063:        0.66234E+02

===============================================================


 INSTANT    0.110640000E-01   TIME STEP NUMBER           11064
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.299726886E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.712850844E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.395295140E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.129262652E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.260346875E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81313E-03   0.45232E-02 0.19909E+01 
c  Velocity[X]                                      0.13721E-03 
c  Velocity[Y]                                      0.12767E-03 
c  Velocity[Z]                                      0.42583E-02 
c  Pressure     0.36148E-04     132   0.91998E-02   0.25497E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60432E-08   0.16400E-08 0.99075E-01 
c  r22          0.10853E-01      13   0.61418E-08   0.18417E-08 0.10101E+00 
c  r33          0.21861E-01      15   0.66618E-08   0.12632E-07 0.12743E+00 
c  r12          0.93877E-03      18   0.72850E-08   0.29762E-09 0.60797E+00 
c  r13          0.46678E-02      19   0.66844E-08   0.15172E-08 0.20043E+00 
c  r23          0.39980E-02      19   0.55593E-08   0.12812E-08 0.19856E+00 
c  epsilon      0.10969E+02      11   0.33333E-08   0.10155E-01 0.16812E+00 
c  TempC        0.25716E+06      16   0.15187E-04   0.84210E-02 0.43281E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61376       0.0052575       0.0015075
v  Velocity[Y]            -0.57345         0.54436       0.0030797      0.00087278
v  Velocity[Z]              1.5657          5.4406          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4406          4.3406          4.3632
v  Pressure                -36.458          359.97          87.633          169.82
v  r11                   0.0010621        0.081993        0.013076        0.018287
v  r22                   0.0011158        0.082596        0.013356        0.018647
v  r33                    0.001644         0.17432        0.027255        0.037208
v  r12                   -0.010665        0.013595     -0.00023386     -0.00030933
v  r13                   -0.045511        0.052785      9.3332e-05       0.0010139
v  r23                   -0.046706         0.05125      3.0604e-05      0.00057464
v  epsilon                0.069527          271.18          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9912e-05       0.0099177      0.00092531       0.0017428
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017879          5.2774         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            11064:        0.64774E+02

===============================================================


 INSTANT    0.110650000E-01   TIME STEP NUMBER           11065
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.118134001E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.176103166E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.197246881E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935018E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.245132914E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.298752306E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81310E-03   0.44672E-02 0.19782E+01 
c  Velocity[X]                                      0.13640E-03 
c  Velocity[Y]                                      0.12712E-03 
c  Velocity[Z]                                      0.42037E-02 
c  Pressure     0.35654E-04     133   0.90739E-02   0.25148E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53977E-08   0.16386E-08 0.99041E-01 
c  r22          0.10853E-01      13   0.60853E-08   0.17853E-08 0.99974E-01 
c  r33          0.21861E-01      15   0.64228E-08   0.12372E-07 0.12649E+00 
c  r12          0.93877E-03      19   0.55789E-08   0.29042E-09 0.60233E+00 
c  r13          0.46678E-02      19   0.58712E-08   0.14802E-08 0.19871E+00 
c  r23          0.39980E-02      19   0.55312E-08   0.12768E-08 0.19833E+00 
c  epsilon      0.10969E+02      11   0.34189E-08   0.96911E-02 0.16350E+00 
c  TempC        0.25716E+06      16   0.15120E-04   0.84477E-02 0.43344E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61372       0.0052575       0.0015075
v  Velocity[Y]            -0.57344         0.54405       0.0030797      0.00087278
v  Velocity[Z]              1.5658          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4407          4.3406          4.3632
v  Pressure                -36.418             360          87.611          169.82
v  r11                   0.0010621        0.081982        0.013076        0.018287
v  r22                   0.0011158        0.082599        0.013356        0.018647
v  r33                    0.001644         0.17433        0.027255        0.037208
v  r12                   -0.010669        0.013591     -0.00023386     -0.00030933
v  r13                   -0.045515        0.052784      9.3332e-05       0.0010139
v  r23                   -0.046705        0.051236      3.0604e-05      0.00057464
v  epsilon                0.069528          271.19          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099177      0.00092531       0.0017428
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017879          5.2774         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            11065:        0.70197E+02

===============================================================


 INSTANT    0.110660000E-01   TIME STEP NUMBER           11066
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.142123857E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.317882801E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.640589812E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138059902E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.104580143E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81229E-03   0.45096E-02 0.19883E+01 
c  Velocity[X]                                      0.13808E-03 
c  Velocity[Y]                                      0.12809E-03 
c  Velocity[Z]                                      0.42434E-02 
c  Pressure     0.36339E-04     132   0.92472E-02   0.25630E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56710E-08   0.16188E-08 0.98460E-01 
c  r22          0.10853E-01      13   0.64007E-08   0.18013E-08 0.10035E+00 
c  r33          0.21861E-01      15   0.59916E-08   0.12414E-07 0.12635E+00 
c  r12          0.93877E-03      19   0.57217E-08   0.29249E-09 0.60156E+00 
c  r13          0.46678E-02      19   0.64150E-08   0.14686E-08 0.19821E+00 
c  r23          0.39980E-02      18   0.71118E-08   0.12826E-08 0.19765E+00 
c  epsilon      0.10969E+02      11   0.34275E-08   0.98285E-02 0.16484E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.84032E-02 0.43203E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61378       0.0052575       0.0015075
v  Velocity[Y]            -0.57339         0.54405       0.0030797      0.00087273
v  Velocity[Z]              1.5655          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4407          4.3406          4.3632
v  Pressure                -36.432          360.02          87.659          169.85
v  r11                   0.0010621        0.081973        0.013076        0.018287
v  r22                   0.0011158        0.082601        0.013356        0.018647
v  r33                    0.001644         0.17435        0.027255        0.037208
v  r12                   -0.010672        0.013591     -0.00023386     -0.00030933
v  r13                   -0.045512        0.052786      9.3331e-05       0.0010139
v  r23                   -0.046706        0.051235      3.0604e-05      0.00057464
v  epsilon                0.069529          271.22          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099175      0.00092531       0.0017428
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017879          5.2779         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            11066:        0.67888E+02

===============================================================


 INSTANT    0.110670000E-01   TIME STEP NUMBER           11067
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200153528E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.809930982E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162199480E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.681562738E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184648985E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81278E-03   0.45190E-02 0.19903E+01 
c  Velocity[X]                                      0.13798E-03 
c  Velocity[Y]                                      0.12802E-03 
c  Velocity[Z]                                      0.42530E-02 
c  Pressure     0.36216E-04     133   0.92142E-02   0.25543E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58421E-08   0.16207E-08 0.98948E-01 
c  r22          0.10853E-01      13   0.65759E-08   0.18030E-08 0.10052E+00 
c  r33          0.21861E-01      15   0.64843E-08   0.12429E-07 0.12697E+00 
c  r12          0.93877E-03      18   0.70526E-08   0.29529E-09 0.60880E+00 
c  r13          0.46678E-02      19   0.69382E-08   0.14872E-08 0.19918E+00 
c  r23          0.39980E-02      19   0.57319E-08   0.12597E-08 0.19824E+00 
c  epsilon      0.10969E+02      11   0.34065E-08   0.99196E-02 0.16918E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.84338E-02 0.43321E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61378       0.0052575       0.0015075
v  Velocity[Y]            -0.57339         0.54414       0.0030797      0.00087278
v  Velocity[Z]              1.5657          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4407          4.3406          4.3632
v  Pressure                -36.411          360.04          87.649          169.86
v  r11                   0.0010621        0.081967        0.013076        0.018287
v  r22                   0.0011159        0.082601        0.013356        0.018647
v  r33                    0.001644         0.17438        0.027255        0.037208
v  r12                   -0.010672        0.013595     -0.00023386     -0.00030933
v  r13                   -0.045511        0.052784      9.3332e-05       0.0010139
v  r23                   -0.046706        0.051264      3.0604e-05      0.00057464
v  epsilon                 0.06953          271.23          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099175      0.00092531       0.0017428
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017879          5.2783         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71352         0.85284


 TIME FOR THE TIME STEP            11067:        0.65124E+02

===============================================================


 INSTANT    0.110680000E-01   TIME STEP NUMBER           11068
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.891086866E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.349482741E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.451226719E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.989030414E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186673101E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81410E-03   0.44735E-02 0.19804E+01 
c  Velocity[X]                                      0.13745E-03 
c  Velocity[Y]                                      0.12718E-03 
c  Velocity[Z]                                      0.42089E-02 
c  Pressure     0.36425E-04     132   0.92695E-02   0.25692E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59847E-08   0.16508E-08 0.99341E-01 
c  r22          0.10853E-01      14   0.54185E-08   0.18354E-08 0.10071E+00 
c  r33          0.21861E-01      15   0.60665E-08   0.12691E-07 0.12712E+00 
c  r12          0.93877E-03      19   0.58708E-08   0.29770E-09 0.60495E+00 
c  r13          0.46678E-02      19   0.68637E-08   0.15197E-08 0.19970E+00 
c  r23          0.39980E-02      19   0.55011E-08   0.12925E-08 0.19882E+00 
c  epsilon      0.10969E+02      11   0.33257E-08   0.10355E-01 0.16863E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.83594E-02 0.43191E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61378       0.0052574       0.0015075
v  Velocity[Y]            -0.57341         0.54423       0.0030797      0.00087276
v  Velocity[Z]              1.5655          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4407          4.3406          4.3632
v  Pressure                -36.423          360.04          87.662          169.87
v  r11                   0.0010621        0.081971        0.013076        0.018287
v  r22                   0.0011159        0.082599        0.013356        0.018647
v  r33                   0.0016441          0.1744        0.027255        0.037208
v  r12                   -0.010674        0.013588     -0.00023386     -0.00030933
v  r13                   -0.045513        0.052783      9.3332e-05       0.0010139
v  r23                   -0.046707        0.051258      3.0604e-05      0.00057464
v  epsilon                0.069532          271.23          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099176      0.00092531       0.0017428
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb              0.001788          5.2785         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            11068:        0.68407E+02

===============================================================


 INSTANT    0.110690000E-01   TIME STEP NUMBER           11069
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.692784057E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.167880524E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.784228110E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.776506131E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.264430211E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81165E-03   0.45183E-02 0.19904E+01 
c  Velocity[X]                                      0.13747E-03 
c  Velocity[Y]                                      0.12799E-03 
c  Velocity[Z]                                      0.42528E-02 
c  Pressure     0.36678E-04     133   0.93420E-02   0.25870E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59073E-08   0.16156E-08 0.98456E-01 
c  r22          0.10853E-01      13   0.66150E-08   0.18239E-08 0.10043E+00 
c  r33          0.21861E-01      15   0.66834E-08   0.12440E-07 0.12593E+00 
c  r12          0.93877E-03      18   0.70597E-08   0.29862E-09 0.60307E+00 
c  r13          0.46678E-02      19   0.62501E-08   0.15017E-08 0.19893E+00 
c  r23          0.39980E-02      19   0.59837E-08   0.12733E-08 0.19670E+00 
c  epsilon      0.10969E+02      11   0.34027E-08   0.98610E-02 0.16371E+00 
c  TempC        0.25716E+06      16   0.15155E-04   0.84068E-02 0.43242E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63334         0.61378       0.0052575       0.0015075
v  Velocity[Y]            -0.57352         0.54406       0.0030797      0.00087278
v  Velocity[Z]              1.5655          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4407          4.3406          4.3632
v  Pressure                -36.405          360.05           87.65          169.86
v  r11                   0.0010621        0.081964        0.013076        0.018287
v  r22                   0.0011159        0.082594        0.013356        0.018647
v  r33                   0.0016441         0.17436        0.027255        0.037208
v  r12                   -0.010678        0.013588     -0.00023386     -0.00030933
v  r13                   -0.045513        0.052785      9.3332e-05       0.0010139
v  r23                   -0.046707        0.051246      3.0603e-05      0.00057464
v  epsilon                0.069533          271.18          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099175      0.00092531       0.0017428
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb              0.001788          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            11069:        0.68985E+02

===============================================================


 INSTANT    0.110700000E-01   TIME STEP NUMBER           11070
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.947898883E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111917188E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.852416613E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.331498106E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.235149243E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81344E-03   0.45096E-02 0.19871E+01 
c  Velocity[X]                                      0.13785E-03 
c  Velocity[Y]                                      0.12821E-03 
c  Velocity[Z]                                      0.42436E-02 
c  Pressure     0.36134E-04     133   0.92055E-02   0.25487E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55883E-08   0.16404E-08 0.99107E-01 
c  r22          0.10853E-01      13   0.64344E-08   0.18267E-08 0.10087E+00 
c  r33          0.21861E-01      15   0.57097E-08   0.12543E-07 0.12681E+00 
c  r12          0.93877E-03      18   0.72732E-08   0.29718E-09 0.60272E+00 
c  r13          0.46678E-02      19   0.61689E-08   0.15092E-08 0.20010E+00 
c  r23          0.39980E-02      19   0.64699E-08   0.12801E-08 0.19796E+00 
c  epsilon      0.10969E+02      11   0.33411E-08   0.99460E-02 0.16714E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.84624E-02 0.43403E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61379       0.0052575       0.0015076
v  Velocity[Y]            -0.57346         0.54411       0.0030797      0.00087277
v  Velocity[Z]              1.5652          5.4407          4.3387          4.3625
v  ǁVelocityǁ                1.579          5.4407          4.3406          4.3632
v  Pressure                -36.445             360          87.648          169.84
v  r11                   0.0010621        0.081964        0.013076        0.018287
v  r22                   0.0011159        0.082595        0.013356        0.018647
v  r33                   0.0016441         0.17432        0.027255        0.037208
v  r12                    -0.01068        0.013591     -0.00023386     -0.00030933
v  r13                   -0.045512        0.052785      9.3332e-05       0.0010139
v  r23                   -0.046708         0.05126      3.0604e-05      0.00057464
v  epsilon                0.069534           271.2          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099174      0.00092531       0.0017428
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb              0.001788          5.2788         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71352         0.85284


 TIME FOR THE TIME STEP            11070:        0.70571E+02

===============================================================


 INSTANT    0.110710000E-01   TIME STEP NUMBER           11071
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.719854838E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.579539548E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.277028889E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.476923698E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.520595756E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81360E-03   0.44902E-02 0.19856E+01 
c  Velocity[X]                                      0.13746E-03 
c  Velocity[Y]                                      0.12753E-03 
c  Velocity[Z]                                      0.42252E-02 
c  Pressure     0.36112E-04     133   0.91864E-02   0.25471E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54312E-08   0.16416E-08 0.98848E-01 
c  r22          0.10853E-01      13   0.66192E-08   0.18142E-08 0.10051E+00 
c  r33          0.21861E-01      15   0.61500E-08   0.12529E-07 0.12653E+00 
c  r12          0.93877E-03      19   0.57200E-08   0.29317E-09 0.60168E+00 
c  r13          0.46678E-02      19   0.61239E-08   0.14839E-08 0.19899E+00 
c  r23          0.39980E-02      19   0.58578E-08   0.12879E-08 0.19792E+00 
c  epsilon      0.10969E+02      11   0.33861E-08   0.99813E-02 0.16694E+00 
c  TempC        0.25716E+06      16   0.15142E-04   0.83415E-02 0.43101E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61377       0.0052576       0.0015076
v  Velocity[Y]            -0.57353          0.5438       0.0030797      0.00087281
v  Velocity[Z]              1.5654          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4407          4.3406          4.3632
v  Pressure                 -36.42          360.04          87.643          169.86
v  r11                   0.0010621        0.081954        0.013076        0.018287
v  r22                   0.0011159        0.082596        0.013356        0.018647
v  r33                   0.0016441         0.17432        0.027255        0.037208
v  r12                   -0.010683        0.013589     -0.00023386     -0.00030933
v  r13                   -0.045514        0.052783      9.3332e-05       0.0010139
v  r23                   -0.046708        0.051257      3.0603e-05      0.00057464
v  epsilon                0.069535          271.23          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099174      0.00092531       0.0017428
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb              0.001788          5.2782         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            11071:        0.66558E+02

===============================================================


 INSTANT    0.110720000E-01   TIME STEP NUMBER           11072
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.292153503E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184652796E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.903605666E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.281290374E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117390493E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81250E-03   0.45100E-02 0.19862E+01 
c  Velocity[X]                                      0.13756E-03 
c  Velocity[Y]                                      0.12793E-03 
c  Velocity[Z]                                      0.42445E-02 
c  Pressure     0.36233E-04     132   0.92198E-02   0.25555E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52294E-08   0.16161E-08 0.98252E-01 
c  r22          0.10853E-01      13   0.60356E-08   0.18143E-08 0.10018E+00 
c  r33          0.21861E-01      15   0.58537E-08   0.12448E-07 0.12584E+00 
c  r12          0.93877E-03      18   0.69385E-08   0.29883E-09 0.60234E+00 
c  r13          0.46678E-02      19   0.54000E-08   0.14971E-08 0.19834E+00 
c  r23          0.39980E-02      19   0.57650E-08   0.12771E-08 0.19720E+00 
c  epsilon      0.10969E+02      11   0.35708E-08   0.99410E-02 0.16621E+00 
c  TempC        0.25716E+06      16   0.15164E-04   0.84027E-02 0.43272E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61374       0.0052574       0.0015075
v  Velocity[Y]            -0.57342         0.54388       0.0030797      0.00087278
v  Velocity[Z]              1.5656          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4407          4.3406          4.3632
v  Pressure                -36.437          360.02          87.672          169.86
v  r11                   0.0010621        0.081956        0.013076        0.018287
v  r22                   0.0011159        0.082596        0.013356        0.018647
v  r33                   0.0016441         0.17433        0.027255        0.037208
v  r12                   -0.010683        0.013589     -0.00023386     -0.00030933
v  r13                   -0.045512        0.052782      9.3331e-05       0.0010139
v  r23                   -0.046708        0.051252      3.0603e-05      0.00057464
v  epsilon                0.069536          271.22          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099173      0.00092531       0.0017428
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb              0.001788          5.2779         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            11072:        0.65779E+02

===============================================================


 INSTANT    0.110730000E-01   TIME STEP NUMBER           11073
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.909221473E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.214693400E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.313891498E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.378396988E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.465981416E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81275E-03   0.45287E-02 0.19922E+01 
c  Velocity[X]                                      0.13871E-03 
c  Velocity[Y]                                      0.12766E-03 
c  Velocity[Z]                                      0.42623E-02 
c  Pressure     0.36285E-04     133   0.92360E-02   0.25593E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.50893E-08   0.16548E-08 0.99591E-01 
c  r22          0.10853E-01      13   0.56136E-08   0.18409E-08 0.10089E+00 
c  r33          0.21861E-01      15   0.59275E-08   0.12712E-07 0.12722E+00 
c  r12          0.93877E-03      18   0.59128E-08   0.29380E-09 0.60490E+00 
c  r13          0.46678E-02      19   0.67221E-08   0.15037E-08 0.19957E+00 
c  r23          0.39980E-02      19   0.62211E-08   0.12865E-08 0.19886E+00 
c  epsilon      0.10969E+02      11   0.34923E-08   0.10347E-01 0.17209E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.84505E-02 0.43417E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63336         0.61373       0.0052576       0.0015075
v  Velocity[Y]            -0.57351         0.54401       0.0030797      0.00087279
v  Velocity[Z]              1.5653          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4407          4.3406          4.3632
v  Pressure                -36.439          360.02          87.638          169.85
v  r11                   0.0010621        0.081953        0.013076        0.018287
v  r22                   0.0011159        0.082596        0.013356        0.018647
v  r33                   0.0016441         0.17436        0.027255        0.037208
v  r12                   -0.010684         0.01359     -0.00023386     -0.00030933
v  r13                   -0.045513        0.052782      9.3332e-05       0.0010139
v  r23                   -0.046708        0.051243      3.0603e-05      0.00057464
v  epsilon                0.069537          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9912e-05       0.0099175      0.00092531       0.0017428
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb              0.001788          5.2782         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            11073:        0.69043E+02

===============================================================


 INSTANT    0.110740000E-01   TIME STEP NUMBER           11074
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.256390034E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.262508500E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.142104484E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.156686520E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.916496014E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81389E-03   0.44880E-02 0.19827E+01 
c  Velocity[X]                                      0.13665E-03 
c  Velocity[Y]                                      0.12796E-03 
c  Velocity[Z]                                      0.42234E-02 
c  Pressure     0.36060E-04     133   0.91759E-02   0.25435E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51111E-08   0.16518E-08 0.99281E-01 
c  r22          0.10853E-01      13   0.55196E-08   0.18642E-08 0.10119E+00 
c  r33          0.21861E-01      15   0.63376E-08   0.12709E-07 0.12662E+00 
c  r12          0.93877E-03      18   0.59857E-08   0.29972E-09 0.60676E+00 
c  r13          0.46678E-02      19   0.70347E-08   0.15044E-08 0.19948E+00 
c  r23          0.39980E-02      19   0.61484E-08   0.12696E-08 0.19670E+00 
c  epsilon      0.10969E+02      11   0.33112E-08   0.10233E-01 0.16750E+00 
c  TempC        0.25716E+06      16   0.15181E-04   0.84044E-02 0.43191E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61372       0.0052575       0.0015075
v  Velocity[Y]            -0.57353         0.54414       0.0030797      0.00087277
v  Velocity[Z]              1.5654          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4407          4.3406          4.3632
v  Pressure                -36.448             360          87.642          169.84
v  r11                   0.0010621        0.081954        0.013076        0.018287
v  r22                   0.0011159        0.082597        0.013356        0.018647
v  r33                   0.0016441         0.17437        0.027255        0.037208
v  r12                   -0.010682        0.013585     -0.00023386     -0.00030933
v  r13                   -0.045515        0.052782      9.3332e-05       0.0010139
v  r23                   -0.046707        0.051247      3.0603e-05      0.00057464
v  epsilon                0.069538          271.19          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.991e-05       0.0099176      0.00092531       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb              0.001788          5.2771         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71352         0.85284


 TIME FOR THE TIME STEP            11074:        0.67722E+02

===============================================================


 INSTANT    0.110750000E-01   TIME STEP NUMBER           11075
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.399408853E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.934597266E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.473613723E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157890508E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.214010659E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81216E-03   0.45200E-02 0.19903E+01 
c  Velocity[X]                                      0.13693E-03 
c  Velocity[Y]                                      0.12750E-03 
c  Velocity[Z]                                      0.42555E-02 
c  Pressure     0.36209E-04     131   0.92231E-02   0.25539E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52231E-08   0.16313E-08 0.98606E-01 
c  r22          0.10853E-01      13   0.58133E-08   0.18279E-08 0.10051E+00 
c  r33          0.21861E-01      15   0.65300E-08   0.12553E-07 0.12626E+00 
c  r12          0.93877E-03      18   0.61466E-08   0.29770E-09 0.60391E+00 
c  r13          0.46678E-02      19   0.75590E-08   0.14946E-08 0.19858E+00 
c  r23          0.39980E-02      19   0.65798E-08   0.12887E-08 0.19729E+00 
c  epsilon      0.10969E+02      11   0.34236E-08   0.98355E-02 0.16377E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.84121E-02 0.43200E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61367       0.0052575       0.0015075
v  Velocity[Y]            -0.57354         0.54395       0.0030797      0.00087278
v  Velocity[Z]              1.5653          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4407          4.3406          4.3632
v  Pressure                -36.372          360.02          87.645          169.85
v  r11                   0.0010621        0.081967        0.013076        0.018287
v  r22                   0.0011159        0.082597        0.013356        0.018647
v  r33                   0.0016441         0.17439        0.027255        0.037208
v  r12                   -0.010688        0.013586     -0.00023386     -0.00030933
v  r13                   -0.045512         0.05278      9.3331e-05       0.0010139
v  r23                   -0.046707        0.051241      3.0602e-05      0.00057464
v  epsilon                0.069539          271.24          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9909e-05       0.0099176      0.00092531       0.0017428
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb              0.001788           5.277         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71352         0.85284


 TIME FOR THE TIME STEP            11075:        0.68559E+02

===============================================================


 INSTANT    0.110760000E-01   TIME STEP NUMBER           11076
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.257424710E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.223052342E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.257415714E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.330254048E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.138365814E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81321E-03   0.45010E-02 0.19876E+01 
c  Velocity[X]                                      0.13691E-03 
c  Velocity[Y]                                      0.12761E-03 
c  Velocity[Z]                                      0.42365E-02 
c  Pressure     0.36186E-04     132   0.92052E-02   0.25523E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55812E-08   0.16224E-08 0.98799E-01 
c  r22          0.10853E-01      13   0.53261E-08   0.17980E-08 0.10015E+00 
c  r33          0.21861E-01      15   0.71600E-08   0.12415E-07 0.12616E+00 
c  r12          0.93877E-03      18   0.60314E-08   0.29228E-09 0.59893E+00 
c  r13          0.46678E-02      20   0.65449E-08   0.14842E-08 0.19901E+00 
c  r23          0.39980E-02      19   0.73755E-08   0.12930E-08 0.19836E+00 
c  epsilon      0.10969E+02      11   0.35237E-08   0.98155E-02 0.16490E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.83464E-02 0.43201E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61375       0.0052576       0.0015075
v  Velocity[Y]            -0.57356         0.54411       0.0030797      0.00087277
v  Velocity[Z]              1.5654          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4407          4.3406          4.3632
v  Pressure                -36.444          360.07          87.688          169.89
v  r11                   0.0010621         0.08197        0.013076        0.018287
v  r22                   0.0011159        0.082596        0.013356        0.018647
v  r33                   0.0016441          0.1744        0.027255        0.037208
v  r12                   -0.010684        0.013588     -0.00023386     -0.00030933
v  r13                   -0.045511        0.052778      9.3332e-05       0.0010139
v  r23                   -0.046705        0.051241      3.0602e-05      0.00057464
v  epsilon                0.069541          271.23          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9906e-05       0.0099176      0.00092531       0.0017428
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb              0.001788          5.2773         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            11076:        0.71252E+02

===============================================================


 INSTANT    0.110770000E-01   TIME STEP NUMBER           11077
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179045715E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.620752299E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.366986257E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.204568225E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.744015005E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81276E-03   0.44784E-02 0.19795E+01 
c  Velocity[X]                                      0.13756E-03 
c  Velocity[Y]                                      0.12726E-03 
c  Velocity[Z]                                      0.42135E-02 
c  Pressure     0.36097E-04     131   0.91931E-02   0.25460E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57023E-08   0.16517E-08 0.99371E-01 
c  r22          0.10853E-01      13   0.49593E-08   0.17923E-08 0.10017E+00 
c  r33          0.21861E-01      15   0.59778E-08   0.12425E-07 0.12629E+00 
c  r12          0.93877E-03      18   0.57855E-08   0.29569E-09 0.60402E+00 
c  r13          0.46678E-02      20   0.61972E-08   0.14534E-08 0.19783E+00 
c  r23          0.39980E-02      19   0.65880E-08   0.12889E-08 0.19834E+00 
c  epsilon      0.10969E+02      11   0.34988E-08   0.96977E-02 0.16372E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.83845E-02 0.43214E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61372       0.0052574       0.0015075
v  Velocity[Y]            -0.57358         0.54406       0.0030796      0.00087274
v  Velocity[Z]              1.5657          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4407          4.3406          4.3632
v  Pressure                -36.399          360.04          87.651          169.86
v  r11                   0.0010621        0.081966        0.013076        0.018287
v  r22                   0.0011159        0.082594        0.013356        0.018647
v  r33                   0.0016441         0.17436        0.027255        0.037208
v  r12                    -0.01068        0.013579     -0.00023386     -0.00030933
v  r13                   -0.045515        0.052775      9.3331e-05       0.0010139
v  r23                   -0.046704        0.051242      3.0601e-05      0.00057464
v  epsilon                0.069542          271.18          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9906e-05       0.0099175      0.00092531       0.0017428
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017881          5.2774         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            11077:        0.72933E+02

===============================================================


 INSTANT    0.110780000E-01   TIME STEP NUMBER           11078
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.648665556E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237101739E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.335314876E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.352280256E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.696992740E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81365E-03   0.45085E-02 0.19882E+01 
c  Velocity[X]                                      0.13793E-03 
c  Velocity[Y]                                      0.12800E-03 
c  Velocity[Z]                                      0.42426E-02 
c  Pressure     0.36509E-04     133   0.92996E-02   0.25751E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.63842E-08   0.16036E-08 0.97743E-01 
c  r22          0.10853E-01      13   0.49257E-08   0.18447E-08 0.10046E+00 
c  r33          0.21861E-01      15   0.53376E-08   0.12554E-07 0.12575E+00 
c  r12          0.93877E-03      18   0.58142E-08   0.29171E-09 0.59744E+00 
c  r13          0.46678E-02      19   0.74502E-08   0.15259E-08 0.19945E+00 
c  r23          0.39980E-02      19   0.64305E-08   0.12666E-08 0.19582E+00 
c  epsilon      0.10969E+02      11   0.34101E-08   0.10269E-01 0.16768E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.83829E-02 0.43183E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63354         0.61368       0.0052575       0.0015075
v  Velocity[Y]            -0.57354         0.54397       0.0030796      0.00087271
v  Velocity[Z]              1.5656          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4407          4.3406          4.3632
v  Pressure                -36.447             360          87.642          169.83
v  r11                   0.0010622        0.081966        0.013076        0.018287
v  r22                   0.0011159        0.082592        0.013356        0.018647
v  r33                   0.0016442         0.17432        0.027255        0.037208
v  r12                   -0.010678        0.013581     -0.00023386     -0.00030933
v  r13                   -0.045512        0.052776      9.3331e-05       0.0010139
v  r23                   -0.046702        0.051243      3.0601e-05      0.00057464
v  epsilon                0.069543           271.2          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9905e-05       0.0099176      0.00092531       0.0017428
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017881          5.2768         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71352         0.85284


 TIME FOR THE TIME STEP            11078:        0.70066E+02

===============================================================


 INSTANT    0.110790000E-01   TIME STEP NUMBER           11079
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.408119758E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.704405410E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178236457E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.293456603E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.392057720E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81174E-03   0.45186E-02 0.19912E+01 
c  Velocity[X]                                      0.13763E-03 
c  Velocity[Y]                                      0.12811E-03 
c  Velocity[Z]                                      0.42528E-02 
c  Pressure     0.36286E-04     132   0.92343E-02   0.25594E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61248E-08   0.16454E-08 0.99689E-01 
c  r22          0.10853E-01      13   0.47037E-08   0.17852E-08 0.10016E+00 
c  r33          0.21861E-01      15   0.54367E-08   0.12330E-07 0.12651E+00 
c  r12          0.93877E-03      18   0.57180E-08   0.29351E-09 0.60512E+00 
c  r13          0.46678E-02      20   0.63100E-08   0.14630E-08 0.19773E+00 
c  r23          0.39980E-02      19   0.65445E-08   0.12741E-08 0.19888E+00 
c  epsilon      0.10969E+02      11   0.33645E-08   0.95882E-02 0.16594E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.84589E-02 0.43345E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61374       0.0052575       0.0015075
v  Velocity[Y]            -0.57368          0.5441       0.0030797      0.00087277
v  Velocity[Z]              1.5657          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4407          4.3406          4.3632
v  Pressure                -36.376          360.02          87.629          169.84
v  r11                   0.0010622        0.081968        0.013076        0.018287
v  r22                   0.0011159        0.082592        0.013356        0.018647
v  r33                   0.0016442         0.17433        0.027255        0.037208
v  r12                   -0.010686        0.013577     -0.00023386     -0.00030933
v  r13                   -0.045511        0.052778      9.3331e-05       0.0010139
v  r23                   -0.046701        0.051279      3.0601e-05      0.00057464
v  epsilon                0.069544          271.22          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9905e-05       0.0099177      0.00092531       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017881          5.2771         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71352         0.85284


 TIME FOR THE TIME STEP            11079:        0.70380E+02

===============================================================


 INSTANT    0.110800000E-01   TIME STEP NUMBER           11080
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.104576629E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178096579E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145916021E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.127591001E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282732261E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81377E-03   0.44817E-02 0.19814E+01 
c  Velocity[X]                                      0.13656E-03 
c  Velocity[Y]                                      0.12770E-03 
c  Velocity[Z]                                      0.42174E-02 
c  Pressure     0.36372E-04     132   0.92609E-02   0.25654E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.65606E-08   0.16532E-08 0.99216E-01 
c  r22          0.10853E-01      13   0.48820E-08   0.18599E-08 0.10137E+00 
c  r33          0.21861E-01      15   0.63474E-08   0.12732E-07 0.12717E+00 
c  r12          0.93877E-03      18   0.63454E-08   0.29944E-09 0.60494E+00 
c  r13          0.46678E-02      20   0.59301E-08   0.15027E-08 0.19901E+00 
c  r23          0.39980E-02      19   0.62505E-08   0.12932E-08 0.19895E+00 
c  epsilon      0.10969E+02      11   0.35516E-08   0.10038E-01 0.16551E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.83548E-02 0.43158E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162019


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345          0.6137       0.0052575       0.0015075
v  Velocity[Y]            -0.57367         0.54388       0.0030797      0.00087273
v  Velocity[Z]              1.5656          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4407          4.3406          4.3632
v  Pressure                -36.418          360.04          87.659          169.86
v  r11                   0.0010622        0.081976        0.013076        0.018287
v  r22                   0.0011159        0.082593        0.013356        0.018647
v  r33                   0.0016442         0.17433        0.027255        0.037208
v  r12                   -0.010682        0.013581     -0.00023386     -0.00030933
v  r13                   -0.045514        0.052779      9.3332e-05       0.0010139
v  r23                     -0.0467        0.051274      3.0601e-05      0.00057464
v  epsilon                0.069545          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9902e-05       0.0099178      0.00092531       0.0017428
v  CourantNb                0.4422             0.6         0.59908         0.59839
v  FourierNb             0.0017881          5.2771         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71353         0.85285


 TIME FOR THE TIME STEP            11080:        0.71032E+02

===============================================================


 INSTANT    0.110810000E-01   TIME STEP NUMBER           11081
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.371300761E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199923100E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.672284454E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.251918065E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.126126459E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81262E-03   0.44929E-02 0.19868E+01 
c  Velocity[X]                                      0.13719E-03 
c  Velocity[Y]                                      0.12747E-03 
c  Velocity[Z]                                      0.42282E-02 
c  Pressure     0.36361E-04     136   0.92482E-02   0.25646E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.65852E-08   0.16798E-08 0.99839E-01 
c  r22          0.10853E-01      13   0.49318E-08   0.18708E-08 0.10171E+00 
c  r33          0.21861E-01      15   0.56806E-08   0.12870E-07 0.12800E+00 
c  r12          0.93877E-03      18   0.61708E-08   0.31199E-09 0.61406E+00 
c  r13          0.46678E-02      19   0.72723E-08   0.15192E-08 0.20005E+00 
c  r23          0.39980E-02      19   0.62614E-08   0.13157E-08 0.20088E+00 
c  epsilon      0.10969E+02      11   0.36904E-08   0.99723E-02 0.16491E+00 
c  TempC        0.25716E+06      16   0.15169E-04   0.84177E-02 0.43277E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61365       0.0052574       0.0015075
v  Velocity[Y]             -0.5737         0.54401       0.0030796      0.00087273
v  Velocity[Z]              1.5659          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4407          4.3406          4.3632
v  Pressure                -36.406          360.01          87.629          169.83
v  r11                   0.0010622        0.081981        0.013076        0.018287
v  r22                   0.0011159        0.082593        0.013356        0.018647
v  r33                   0.0016442         0.17435        0.027255        0.037208
v  r12                   -0.010678        0.013577     -0.00023387     -0.00030933
v  r13                   -0.045514        0.052779      9.3331e-05       0.0010139
v  r23                     -0.0467        0.051261        3.06e-05      0.00057464
v  epsilon                0.069546          271.18          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9899e-05       0.0099179      0.00092531       0.0017428
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017881          5.2778         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85284


 TIME FOR THE TIME STEP            11081:        0.70998E+02

===============================================================


 INSTANT    0.110820000E-01   TIME STEP NUMBER           11082
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.125347542E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.400285254E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.317937150E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.252039077E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.925817972E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81271E-03   0.45229E-02 0.19922E+01 
c  Velocity[X]                                      0.13831E-03 
c  Velocity[Y]                                      0.12918E-03 
c  Velocity[Z]                                      0.42554E-02 
c  Pressure     0.36367E-04     132   0.92588E-02   0.25649E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.65173E-08   0.16933E-08 0.10017E+00 
c  r22          0.10853E-01      13   0.47145E-08   0.18280E-08 0.10120E+00 
c  r33          0.21861E-01      15   0.58802E-08   0.12693E-07 0.12767E+00 
c  r12          0.93877E-03      18   0.62486E-08   0.30002E-09 0.60485E+00 
c  r13          0.46678E-02      19   0.71896E-08   0.14863E-08 0.19933E+00 
c  r23          0.39980E-02      19   0.54991E-08   0.13142E-08 0.20006E+00 
c  epsilon      0.10969E+02      11   0.37667E-08   0.97342E-02 0.16408E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.84316E-02 0.43265E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63354         0.61371       0.0052574       0.0015074
v  Velocity[Y]            -0.57366         0.54417       0.0030796      0.00087269
v  Velocity[Z]              1.5659          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4407          4.3406          4.3632
v  Pressure                -36.464          360.03          87.666          169.86
v  r11                   0.0010622         0.08199        0.013076        0.018287
v  r22                   0.0011159        0.082593        0.013356        0.018647
v  r33                   0.0016442         0.17437        0.027255        0.037208
v  r12                   -0.010674        0.013578     -0.00023387     -0.00030934
v  r13                   -0.045512         0.05278      9.3332e-05       0.0010139
v  r23                   -0.046701        0.051266      3.0599e-05      0.00057464
v  epsilon                0.069547           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9896e-05       0.0099179      0.00092531       0.0017428
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017881          5.2782         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            11082:        0.70906E+02

===============================================================


 INSTANT    0.110830000E-01   TIME STEP NUMBER           11083
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.218946248E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125209999E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.233292762E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116897816E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.258593350E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81379E-03   0.45237E-02 0.19917E+01 
c  Velocity[X]                                      0.13805E-03 
c  Velocity[Y]                                      0.12771E-03 
c  Velocity[Z]                                      0.42580E-02 
c  Pressure     0.36198E-04     133   0.92204E-02   0.25532E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61562E-08   0.16715E-08 0.99616E-01 
c  r22          0.10853E-01      13   0.47922E-08   0.18432E-08 0.10114E+00 
c  r33          0.21861E-01      15   0.53981E-08   0.12683E-07 0.12718E+00 
c  r12          0.93877E-03      18   0.62071E-08   0.30112E-09 0.60697E+00 
c  r13          0.46678E-02      19   0.60309E-08   0.15040E-08 0.19953E+00 
c  r23          0.39980E-02      19   0.55857E-08   0.12876E-08 0.19828E+00 
c  epsilon      0.10969E+02      11   0.34823E-08   0.10090E-01 0.16670E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.84063E-02 0.43255E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63336          0.6137       0.0052575       0.0015075
v  Velocity[Y]            -0.57384         0.54405       0.0030797      0.00087274
v  Velocity[Z]               1.566          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4407          4.3406          4.3632
v  Pressure                -36.425          360.06          87.659          169.88
v  r11                   0.0010622        0.081987        0.013076        0.018287
v  r22                   0.0011159        0.082589        0.013356        0.018647
v  r33                   0.0016442         0.17439        0.027255        0.037208
v  r12                   -0.010672        0.013581     -0.00023387     -0.00030934
v  r13                   -0.045514         0.05278      9.3332e-05       0.0010139
v  r23                   -0.046701        0.051247      3.0599e-05      0.00057464
v  epsilon                0.069548          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9895e-05       0.0099179      0.00092532       0.0017428
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017881          5.2784         0.11444         0.25446
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85285


 TIME FOR THE TIME STEP            11083:        0.72075E+02

===============================================================


 INSTANT    0.110840000E-01   TIME STEP NUMBER           11084
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.270918972E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.600362196E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158273810E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935011E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229489881E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.705076679E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81245E-03   0.45300E-02 0.19919E+01 
c  Velocity[X]                                      0.13672E-03 
c  Velocity[Y]                                      0.12772E-03 
c  Velocity[Z]                                      0.42656E-02 
c  Pressure     0.36141E-04     133   0.92050E-02   0.25491E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58881E-08   0.16855E-08 0.10000E+00 
c  r22          0.10853E-01      13   0.51055E-08   0.18545E-08 0.10155E+00 
c  r33          0.21861E-01      14   0.71402E-08   0.12709E-07 0.12744E+00 
c  r12          0.93877E-03      18   0.59465E-08   0.29820E-09 0.60397E+00 
c  r13          0.46678E-02      19   0.60279E-08   0.14813E-08 0.19827E+00 
c  r23          0.39980E-02      19   0.55645E-08   0.12940E-08 0.19928E+00 
c  epsilon      0.10969E+02      11   0.34064E-08   0.10189E-01 0.16737E+00 
c  TempC        0.25716E+06      16   0.15178E-04   0.84082E-02 0.43248E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61365       0.0052574       0.0015075
v  Velocity[Y]            -0.57381         0.54413       0.0030796      0.00087274
v  Velocity[Z]              1.5661          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5799          5.4407          4.3406          4.3632
v  Pressure                 -36.43          359.96          87.612           169.8
v  r11                   0.0010622        0.081981        0.013076        0.018287
v  r22                   0.0011159         0.08259        0.013356        0.018647
v  r33                   0.0016442         0.17436        0.027255        0.037208
v  r12                    -0.01067        0.013583     -0.00023387     -0.00030934
v  r13                   -0.045512        0.052781      9.3331e-05       0.0010139
v  r23                   -0.046701        0.051224      3.0598e-05      0.00057464
v  epsilon                 0.06955          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9893e-05       0.0099177      0.00092532       0.0017428
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017882          5.2787         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85284


 TIME FOR THE TIME STEP            11084:        0.70745E+02

===============================================================


 INSTANT    0.110850000E-01   TIME STEP NUMBER           11085
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.320974492E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12302E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.178812723E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12302E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.144803989E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12302E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.843778202E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12302E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.112830126E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12302E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81291E-03   0.44998E-02 0.19848E+01 
c  Velocity[X]                                      0.13812E-03 
c  Velocity[Y]                                      0.12862E-03 
c  Velocity[Z]                                      0.42330E-02 
c  Pressure     0.35870E-04     133   0.91343E-02   0.25300E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57389E-08   0.16579E-08 0.99989E-01 
c  r22          0.10853E-01      13   0.47649E-08   0.18392E-08 0.10127E+00 
c  r33          0.21861E-01      15   0.52224E-08   0.12661E-07 0.12784E+00 
c  r12          0.93877E-03      18   0.60508E-08   0.29881E-09 0.60750E+00 
c  r13          0.46678E-02      19   0.53832E-08   0.14988E-08 0.20019E+00 
c  r23          0.39980E-02      19   0.55045E-08   0.13128E-08 0.20153E+00 
c  epsilon      0.10969E+02      11   0.33169E-08   0.10293E-01 0.17151E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.83944E-02 0.43248E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349          0.6137       0.0052574       0.0015075
v  Velocity[Y]            -0.57378         0.54392       0.0030796      0.00087269
v  Velocity[Z]              1.5661          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5799          5.4407          4.3406          4.3632
v  Pressure                -36.414          360.06          87.654          169.87
v  r11                   0.0010622        0.081974        0.013076        0.018287
v  r22                    0.001116        0.082593        0.013356        0.018647
v  r33                   0.0016442         0.17432        0.027255        0.037208
v  r12                   -0.010671        0.013586     -0.00023387     -0.00030934
v  r13                   -0.045513         0.05278      9.3332e-05       0.0010139
v  r23                   -0.046701        0.051218      3.0598e-05      0.00057464
v  epsilon                0.069551          271.18          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9893e-05       0.0099177      0.00092532       0.0017428
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017882          5.2787         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85284


 TIME FOR THE TIME STEP            11085:        0.70673E+02

===============================================================


 INSTANT    0.110860000E-01   TIME STEP NUMBER           11086
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.300264119E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.785418590E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.199637564E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.134266946E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.719312204E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81420E-03   0.44755E-02 0.19812E+01 
c  Velocity[X]                                      0.13752E-03 
c  Velocity[Y]                                      0.12698E-03 
c  Velocity[Z]                                      0.42110E-02 
c  Pressure     0.36010E-04     133   0.91630E-02   0.25398E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51501E-08   0.16216E-08 0.98708E-01 
c  r22          0.10853E-01      13   0.49256E-08   0.18181E-08 0.10051E+00 
c  r33          0.21861E-01      14   0.65061E-08   0.12387E-07 0.12592E+00 
c  r12          0.93877E-03      18   0.58256E-08   0.29065E-09 0.59729E+00 
c  r13          0.46678E-02      18   0.69754E-08   0.14873E-08 0.19831E+00 
c  r23          0.39980E-02      19   0.60211E-08   0.12634E-08 0.19707E+00 
c  epsilon      0.10969E+02      11   0.33410E-08   0.97329E-02 0.16424E+00 
c  TempC        0.25716E+06      16   0.15177E-04   0.83563E-02 0.43152E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61369       0.0052574       0.0015075
v  Velocity[Y]            -0.57375         0.54389       0.0030795      0.00087265
v  Velocity[Z]              1.5661          5.4407          4.3387          4.3625
v  ǁVelocityǁ                 1.58          5.4407          4.3406          4.3632
v  Pressure                -36.481          360.02          87.644          169.84
v  r11                   0.0010622        0.081969        0.013076        0.018287
v  r22                    0.001116        0.082594        0.013356        0.018647
v  r33                   0.0016442         0.17432        0.027255        0.037208
v  r12                   -0.010676        0.013593     -0.00023387     -0.00030934
v  r13                   -0.045515        0.052781      9.3332e-05       0.0010139
v  r23                   -0.046702        0.051237      3.0597e-05      0.00057464
v  epsilon                0.069552           271.2          7.2637          7.8885
v  TempC                       300          311.65          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9892e-05       0.0099178      0.00092532       0.0017428
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017882          5.2782         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            11086:        0.70118E+02

===============================================================


 INSTANT    0.110870000E-01   TIME STEP NUMBER           11087
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136733426E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.508188340E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.148789534E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.773685786E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282810590E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81169E-03   0.45142E-02 0.19907E+01 
c  Velocity[X]                                      0.13726E-03 
c  Velocity[Y]                                      0.12725E-03 
c  Velocity[Z]                                      0.42497E-02 
c  Pressure     0.36024E-04     133   0.91762E-02   0.25408E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53335E-08   0.16498E-08 0.99068E-01 
c  r22          0.10853E-01      13   0.46268E-08   0.18107E-08 0.10047E+00 
c  r33          0.21861E-01      15   0.50995E-08   0.12553E-07 0.12661E+00 
c  r12          0.93877E-03      18   0.54496E-08   0.30044E-09 0.60654E+00 
c  r13          0.46678E-02      19   0.55741E-08   0.14737E-08 0.19830E+00 
c  r23          0.39980E-02      19   0.54867E-08   0.12860E-08 0.19828E+00 
c  epsilon      0.10969E+02      11   0.33915E-08   0.99330E-02 0.16470E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.83843E-02 0.43230E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61366       0.0052575       0.0015075
v  Velocity[Y]            -0.57374         0.54399       0.0030796      0.00087269
v  Velocity[Z]               1.566          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5798          5.4408          4.3406          4.3632
v  Pressure                -36.444          359.98          87.607           169.8
v  r11                   0.0010622        0.081964        0.013076        0.018287
v  r22                    0.001116        0.082595        0.013356        0.018647
v  r33                   0.0016443         0.17433        0.027255        0.037208
v  r12                   -0.010677        0.013589     -0.00023387     -0.00030934
v  r13                   -0.045512         0.05278      9.3332e-05       0.0010139
v  r23                   -0.046703        0.051227      3.0597e-05      0.00057464
v  epsilon                0.069553          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9894e-05       0.0099177      0.00092532       0.0017428
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017882          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            11087:        0.68927E+02

===============================================================


 INSTANT    0.110880000E-01   TIME STEP NUMBER           11088
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.400264136E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12302E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.230530142E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12302E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116209860E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12302E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183875273E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12302E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.145538108E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12302E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81317E-03   0.45125E-02 0.19877E+01 
c  Velocity[X]                                      0.13722E-03 
c  Velocity[Y]                                      0.12780E-03 
c  Velocity[Z]                                      0.42475E-02 
c  Pressure     0.36350E-04     133   0.92521E-02   0.25638E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57757E-08   0.16356E-08 0.98689E-01 
c  r22          0.10853E-01      13   0.46338E-08   0.18539E-08 0.10110E+00 
c  r33          0.21861E-01      14   0.70468E-08   0.12663E-07 0.12688E+00 
c  r12          0.93877E-03      17   0.69799E-08   0.30009E-09 0.60610E+00 
c  r13          0.46678E-02      19   0.66907E-08   0.15162E-08 0.20017E+00 
c  r23          0.39980E-02      19   0.58746E-08   0.12797E-08 0.19739E+00 
c  epsilon      0.10969E+02      11   0.34049E-08   0.10275E-01 0.16770E+00 
c  TempC        0.25716E+06      16   0.15155E-04   0.84953E-02 0.43467E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63358         0.61374       0.0052574       0.0015075
v  Velocity[Y]            -0.57366         0.54417       0.0030796      0.00087269
v  Velocity[Z]              1.5659          5.4407          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4408          4.3406          4.3632
v  Pressure                -36.479          359.97          87.625           169.8
v  r11                   0.0010622        0.081974        0.013076        0.018287
v  r22                    0.001116        0.082595        0.013356        0.018647
v  r33                   0.0016443         0.17435        0.027255        0.037208
v  r12                   -0.010676        0.013591     -0.00023387     -0.00030934
v  r13                   -0.045511        0.052779      9.3332e-05       0.0010139
v  r23                   -0.046703        0.051217      3.0597e-05      0.00057464
v  epsilon                0.069554          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9892e-05       0.0099177      0.00092532       0.0017428
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017882           5.279         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71352         0.85284


 TIME FOR THE TIME STEP            11088:        0.71178E+02

===============================================================


 INSTANT    0.110890000E-01   TIME STEP NUMBER           11089
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.312565802E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.905541476E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.253536301E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.253634388E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.384070803E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81251E-03   0.44912E-02 0.19841E+01 
c  Velocity[X]                                      0.13715E-03 
c  Velocity[Y]                                      0.12706E-03 
c  Velocity[Z]                                      0.42270E-02 
c  Pressure     0.36422E-04     132   0.92665E-02   0.25689E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61731E-08   0.16517E-08 0.99331E-01 
c  r22          0.10853E-01      13   0.48842E-08   0.18242E-08 0.10078E+00 
c  r33          0.21861E-01      14   0.68080E-08   0.12559E-07 0.12693E+00 
c  r12          0.93877E-03      18   0.56563E-08   0.29780E-09 0.60510E+00 
c  r13          0.46678E-02      19   0.60720E-08   0.14967E-08 0.19940E+00 
c  r23          0.39980E-02      19   0.56077E-08   0.12788E-08 0.19869E+00 
c  epsilon      0.10969E+02      11   0.33230E-08   0.99595E-02 0.16612E+00 
c  TempC        0.25716E+06      16   0.15167E-04   0.84034E-02 0.43197E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61372       0.0052575       0.0015075
v  Velocity[Y]            -0.57369         0.54395       0.0030796       0.0008727
v  Velocity[Z]               1.566          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5798          5.4408          4.3406          4.3632
v  Pressure                 -36.42          360.08          87.658          169.89
v  r11                   0.0010622         0.08198        0.013076        0.018287
v  r22                    0.001116        0.082595        0.013356        0.018647
v  r33                   0.0016443         0.17437        0.027255        0.037208
v  r12                   -0.010675        0.013594     -0.00023387     -0.00030934
v  r13                   -0.045515        0.052781      9.3332e-05       0.0010139
v  r23                   -0.046703        0.051233      3.0596e-05      0.00057464
v  epsilon                0.069555           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9893e-05       0.0099177      0.00092532       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017882          5.2788         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71352         0.85284


 TIME FOR THE TIME STEP            11089:        0.70099E+02

===============================================================


 INSTANT    0.110900000E-01   TIME STEP NUMBER           11090
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.134340318E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.129376401E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934907E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.704320612E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209335454E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.867211548E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81372E-03   0.44869E-02 0.19845E+01 
c  Velocity[X]                                      0.13674E-03 
c  Velocity[Y]                                      0.12794E-03 
c  Velocity[Z]                                      0.42222E-02 
c  Pressure     0.36093E-04     131   0.91833E-02   0.25458E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58843E-08   0.16690E-08 0.10023E+00 
c  r22          0.10853E-01      13   0.49221E-08   0.18340E-08 0.10091E+00 
c  r33          0.21861E-01      15   0.63338E-08   0.12726E-07 0.12772E+00 
c  r12          0.93877E-03      18   0.53688E-08   0.29944E-09 0.60845E+00 
c  r13          0.46678E-02      19   0.67993E-08   0.14864E-08 0.19898E+00 
c  r23          0.39980E-02      19   0.54610E-08   0.12956E-08 0.20081E+00 
c  epsilon      0.10969E+02      11   0.34288E-08   0.99614E-02 0.16653E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.83485E-02 0.43090E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61369       0.0052575       0.0015075
v  Velocity[Y]            -0.57363         0.54409       0.0030795      0.00087267
v  Velocity[Z]               1.566          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5798          5.4408          4.3406          4.3632
v  Pressure                -36.465          360.01          87.639          169.83
v  r11                   0.0010622        0.081974        0.013076        0.018287
v  r22                    0.001116        0.082596        0.013356        0.018647
v  r33                   0.0016443         0.17438        0.027255        0.037208
v  r12                   -0.010674        0.013591     -0.00023387     -0.00030934
v  r13                   -0.045512        0.052782      9.3333e-05       0.0010139
v  r23                   -0.046703        0.051224      3.0596e-05      0.00057464
v  epsilon                0.069556          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9892e-05       0.0099178      0.00092532       0.0017428
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017882          5.2796         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8796         0.71352         0.85284


 TIME FOR THE TIME STEP            11090:        0.68628E+02

===============================================================


 INSTANT    0.110910000E-01   TIME STEP NUMBER           11091
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.271309054E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.402833892E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141079464E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.450048276E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.554951941E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      45   0.81306E-03   0.45275E-02 0.19935E+01 
c  Velocity[X]                                      0.13841E-03 
c  Velocity[Y]                                      0.12833E-03 
c  Velocity[Z]                                      0.42608E-02 
c  Pressure     0.36472E-04     132   0.92870E-02   0.25725E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.62536E-08   0.17135E-08 0.10112E+00 
c  r22          0.10853E-01      13   0.56735E-08   0.18431E-08 0.10164E+00 
c  r33          0.21861E-01      15   0.70102E-08   0.12860E-07 0.12883E+00 
c  r12          0.93877E-03      18   0.69196E-08   0.30028E-09 0.60678E+00 
c  r13          0.46678E-02      19   0.68865E-08   0.14936E-08 0.19980E+00 
c  r23          0.39980E-02      19   0.55559E-08   0.13242E-08 0.20224E+00 
c  epsilon      0.10969E+02      11   0.34403E-08   0.10277E-01 0.17121E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.84159E-02 0.43298E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61374       0.0052576       0.0015076
v  Velocity[Y]            -0.57373         0.54386       0.0030795      0.00087268
v  Velocity[Z]              1.5661          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5799          5.4408          4.3406          4.3632
v  Pressure                -36.388          360.04           87.65          169.86
v  r11                   0.0010622         0.08197        0.013076        0.018287
v  r22                    0.001116        0.082596        0.013356        0.018647
v  r33                   0.0016443          0.1744        0.027255        0.037208
v  r12                   -0.010672        0.013592     -0.00023387     -0.00030934
v  r13                   -0.045511        0.052781      9.3333e-05       0.0010139
v  r23                   -0.046703         0.05122      3.0596e-05      0.00057464
v  epsilon                0.069557          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9894e-05       0.0099179      0.00092532       0.0017428
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017883          5.2795         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8795         0.71352         0.85284


 TIME FOR THE TIME STEP            11091:        0.70508E+02

===============================================================


 INSTANT    0.110920000E-01   TIME STEP NUMBER           11092
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.236051849E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.341854308E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.141486245E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.231444709E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.158434025E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81344E-03   0.44914E-02 0.19847E+01 
c  Velocity[X]                                      0.13730E-03 
c  Velocity[Y]                                      0.12761E-03 
c  Velocity[Z]                                      0.42265E-02 
c  Pressure     0.35917E-04     133   0.91451E-02   0.25332E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56000E-08   0.16280E-08 0.98852E-01 
c  r22          0.10853E-01      13   0.60980E-08   0.18103E-08 0.10090E+00 
c  r33          0.21861E-01      15   0.61884E-08   0.12333E-07 0.12618E+00 
c  r12          0.93878E-03      18   0.69750E-08   0.29239E-09 0.60128E+00 
c  r13          0.46678E-02      19   0.62868E-08   0.14723E-08 0.19859E+00 
c  r23          0.39980E-02      19   0.64444E-08   0.12682E-08 0.19722E+00 
c  epsilon      0.10969E+02      11   0.34280E-08   0.96028E-02 0.16434E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83650E-02 0.43162E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63356         0.61372       0.0052575       0.0015075
v  Velocity[Y]            -0.57361          0.5439       0.0030795      0.00087267
v  Velocity[Z]              1.5661          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5799          5.4408          4.3406          4.3632
v  Pressure                -36.481          360.04          87.663          169.87
v  r11                   0.0010622        0.081954        0.013076        0.018287
v  r22                    0.001116        0.082596        0.013356        0.018647
v  r33                   0.0016443         0.17436        0.027255        0.037208
v  r12                   -0.010678        0.013589     -0.00023387     -0.00030934
v  r13                   -0.045515        0.052781      9.3333e-05       0.0010139
v  r23                   -0.046704         0.05123      3.0596e-05      0.00057464
v  epsilon                0.069559          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9894e-05        0.009918      0.00092532       0.0017428
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017883          5.2791         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71352         0.85284


 TIME FOR THE TIME STEP            11092:        0.67177E+02

===============================================================


 INSTANT    0.110930000E-01   TIME STEP NUMBER           11093
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.238700024E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.322170154E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.264604763E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.966750573E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.457751750E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81215E-03   0.45065E-02 0.19862E+01 
c  Velocity[X]                                      0.13688E-03 
c  Velocity[Y]                                      0.12731E-03 
c  Velocity[Z]                                      0.42423E-02 
c  Pressure     0.36207E-04     131   0.92145E-02   0.25537E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54287E-08   0.16511E-08 0.99461E-01 
c  r22          0.10853E-01      13   0.62582E-08   0.18256E-08 0.10067E+00 
c  r33          0.21861E-01      15   0.65724E-08   0.12498E-07 0.12636E+00 
c  r12          0.93878E-03      18   0.62939E-08   0.29339E-09 0.60260E+00 
c  r13          0.46678E-02      19   0.73048E-08   0.14782E-08 0.19824E+00 
c  r23          0.39980E-02      20   0.58327E-08   0.12731E-08 0.19761E+00 
c  epsilon      0.10969E+02      11   0.33297E-08   0.98931E-02 0.16524E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.84018E-02 0.43255E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63339         0.61369       0.0052575       0.0015075
v  Velocity[Y]            -0.57373         0.54404       0.0030796      0.00087271
v  Velocity[Z]              1.5661          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5799          5.4408          4.3406          4.3632
v  Pressure                -36.421          360.04          87.652          169.87
v  r11                   0.0010622        0.081943        0.013076        0.018287
v  r22                    0.001116        0.082595        0.013356        0.018647
v  r33                   0.0016443         0.17432        0.027255        0.037208
v  r12                   -0.010677         0.01359     -0.00023387     -0.00030934
v  r13                   -0.045514        0.052779      9.3334e-05       0.0010139
v  r23                   -0.046704        0.051264      3.0596e-05      0.00057464
v  epsilon                 0.06956           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9896e-05        0.009918      0.00092532       0.0017428
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017883          5.2782         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85285


 TIME FOR THE TIME STEP            11093:        0.67558E+02

===============================================================


 INSTANT    0.110940000E-01   TIME STEP NUMBER           11094
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.212161268E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12302E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.853856423E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12302E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.156684811E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12302E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.769624108E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12302E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.418612414E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12302E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81329E-03   0.45166E-02 0.19904E+01 
c  Velocity[X]                                      0.13740E-03 
c  Velocity[Y]                                      0.12847E-03 
c  Velocity[Z]                                      0.42507E-02 
c  Pressure     0.36307E-04     132   0.92442E-02   0.25608E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51883E-08   0.16425E-08 0.99323E-01 
c  r22          0.10853E-01      13   0.60622E-08   0.18165E-08 0.10023E+00 
c  r33          0.21861E-01      15   0.67740E-08   0.12533E-07 0.12626E+00 
c  r12          0.93878E-03      18   0.61506E-08   0.29603E-09 0.60336E+00 
c  r13          0.46678E-02      20   0.62556E-08   0.15047E-08 0.19889E+00 
c  r23          0.39980E-02      20   0.72282E-08   0.12999E-08 0.19913E+00 
c  epsilon      0.10969E+02      11   0.34200E-08   0.10138E-01 0.16795E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84281E-02 0.43317E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162016


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61376       0.0052575       0.0015075
v  Velocity[Y]            -0.57374         0.54417       0.0030796       0.0008727
v  Velocity[Z]              1.5659          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4408          4.3406          4.3632
v  Pressure                -36.417          360.02          87.675          169.87
v  r11                   0.0010622        0.081943        0.013076        0.018287
v  r22                    0.001116        0.082595        0.013356        0.018647
v  r33                   0.0016443         0.17432        0.027255        0.037208
v  r12                   -0.010675        0.013588     -0.00023387     -0.00030934
v  r13                   -0.045512        0.052781      9.3334e-05       0.0010139
v  r23                   -0.046704        0.051265      3.0595e-05      0.00057464
v  epsilon                0.069561          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9898e-05       0.0099179      0.00092532       0.0017428
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017883          5.2775         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71352         0.85284


 TIME FOR THE TIME STEP            11094:        0.70534E+02

===============================================================


 INSTANT    0.110950000E-01   TIME STEP NUMBER           11095
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.469158235E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.438950300E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.103126295E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.211743912E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183591782E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81383E-03   0.45189E-02 0.19901E+01 
c  Velocity[X]                                      0.13808E-03 
c  Velocity[Y]                                      0.12823E-03 
c  Velocity[Z]                                      0.42525E-02 
c  Pressure     0.36308E-04     131   0.92442E-02   0.25609E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59975E-08   0.16340E-08 0.98953E-01 
c  r22          0.10853E-01      13   0.65088E-08   0.17971E-08 0.10021E+00 
c  r33          0.21861E-01      15   0.63626E-08   0.12366E-07 0.12613E+00 
c  r12          0.93878E-03      18   0.68338E-08   0.29567E-09 0.60395E+00 
c  r13          0.46678E-02      20   0.60063E-08   0.14653E-08 0.19753E+00 
c  r23          0.39980E-02      20   0.59649E-08   0.12740E-08 0.19810E+00 
c  epsilon      0.10969E+02      11   0.34046E-08   0.98093E-02 0.16585E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.83652E-02 0.43133E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61375       0.0052575       0.0015075
v  Velocity[Y]             -0.5737         0.54401       0.0030796      0.00087268
v  Velocity[Z]              1.5659          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4408          4.3406          4.3632
v  Pressure                -36.386          360.02          87.633          169.84
v  r11                   0.0010622        0.081949        0.013076        0.018287
v  r22                    0.001116        0.082595        0.013356        0.018647
v  r33                   0.0016443         0.17434        0.027255        0.037208
v  r12                   -0.010671        0.013582     -0.00023387     -0.00030934
v  r13                   -0.045514        0.052781      9.3334e-05       0.0010139
v  r23                   -0.046705        0.051259      3.0595e-05      0.00057464
v  epsilon                0.069562          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc               5.99e-05       0.0099179      0.00092532       0.0017428
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017883          5.2766         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71352         0.85284


 TIME FOR THE TIME STEP            11095:        0.70098E+02

===============================================================


 INSTANT    0.110960000E-01   TIME STEP NUMBER           11096
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.298062277E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.125012007E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934903E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.123563903E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.129766216E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.155808024E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81267E-03   0.44916E-02 0.19841E+01 
c  Velocity[X]                                      0.13652E-03 
c  Velocity[Y]                                      0.12769E-03 
c  Velocity[Z]                                      0.42274E-02 
c  Pressure     0.35925E-04     133   0.91486E-02   0.25337E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55873E-08   0.16384E-08 0.98830E-01 
c  r22          0.10853E-01      13   0.64449E-08   0.18556E-08 0.10093E+00 
c  r33          0.21861E-01      15   0.68060E-08   0.12698E-07 0.12673E+00 
c  r12          0.93878E-03      19   0.55697E-08   0.29332E-09 0.60057E+00 
c  r13          0.46678E-02      19   0.68364E-08   0.15154E-08 0.19920E+00 
c  r23          0.39980E-02      19   0.74014E-08   0.12888E-08 0.19870E+00 
c  epsilon      0.10969E+02      11   0.35163E-08   0.10431E-01 0.16974E+00 
c  TempC        0.25716E+06      16   0.15188E-04   0.84105E-02 0.43280E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61368       0.0052574       0.0015074
v  Velocity[Y]            -0.57357         0.54414       0.0030794      0.00087262
v  Velocity[Z]              1.5656          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4408          4.3406          4.3632
v  Pressure                -36.436          360.02          87.651          169.85
v  r11                   0.0010622        0.081951        0.013076        0.018287
v  r22                    0.001116        0.082595        0.013356        0.018647
v  r33                   0.0016443         0.17436        0.027256        0.037208
v  r12                   -0.010668        0.013585     -0.00023387     -0.00030934
v  r13                   -0.045512        0.052781      9.3333e-05       0.0010139
v  r23                   -0.046705        0.051262      3.0595e-05      0.00057464
v  epsilon                0.069563          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9899e-05       0.0099179      0.00092532       0.0017428
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017883          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            11096:        0.68889E+02

===============================================================


 INSTANT    0.110970000E-01   TIME STEP NUMBER           11097
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.126992702E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.594129336E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.177718304E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.990216714E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.930668842E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81241E-03   0.45149E-02 0.19900E+01 
c  Velocity[X]                                      0.13743E-03 
c  Velocity[Y]                                      0.12854E-03 
c  Velocity[Z]                                      0.42489E-02 
c  Pressure     0.36251E-04     133   0.92238E-02   0.25569E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52511E-08   0.16669E-08 0.99848E-01 
c  r22          0.10853E-01      13   0.64387E-08   0.18502E-08 0.10124E+00 
c  r33          0.21861E-01      15   0.53627E-08   0.12828E-07 0.12783E+00 
c  r12          0.93878E-03      18   0.68295E-08   0.29751E-09 0.60392E+00 
c  r13          0.46678E-02      19   0.56852E-08   0.15223E-08 0.20001E+00 
c  r23          0.39980E-02      20   0.56145E-08   0.13188E-08 0.20125E+00 
c  epsilon      0.10969E+02      11   0.33505E-08   0.10524E-01 0.17339E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84322E-02 0.43337E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61376       0.0052574       0.0015075
v  Velocity[Y]            -0.57354         0.54386       0.0030795      0.00087264
v  Velocity[Z]              1.5659          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4408          4.3406          4.3632
v  Pressure                -36.399           360.1          87.704          169.92
v  r11                   0.0010622        0.081955        0.013076        0.018287
v  r22                    0.001116        0.082597        0.013356        0.018647
v  r33                   0.0016443         0.17438        0.027256        0.037208
v  r12                    -0.01067        0.013594     -0.00023387     -0.00030934
v  r13                   -0.045513         0.05278      9.3334e-05       0.0010139
v  r23                   -0.046706        0.051293      3.0595e-05      0.00057464
v  epsilon                0.069564          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9898e-05        0.009918      0.00092532       0.0017428
v  CourantNb                0.4422             0.6         0.59908         0.59839
v  FourierNb             0.0017884          5.2779         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            11097:        0.68508E+02

===============================================================


 INSTANT    0.110980000E-01   TIME STEP NUMBER           11098
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.448465533E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.591709153E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138630484E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.692981932E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.944011980E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81353E-03   0.44601E-02 0.19775E+01 
c  Velocity[X]                                      0.13598E-03 
c  Velocity[Y]                                      0.12715E-03 
c  Velocity[Z]                                      0.41970E-02 
c  Pressure     0.35999E-04     131   0.91652E-02   0.25391E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53950E-08   0.16168E-08 0.98554E-01 
c  r22          0.10853E-01      13   0.58490E-08   0.17896E-08 0.10005E+00 
c  r33          0.21861E-01      15   0.54743E-08   0.12238E-07 0.12521E+00 
c  r12          0.93878E-03      18   0.62813E-08   0.29261E-09 0.59887E+00 
c  r13          0.46678E-02      19   0.53770E-08   0.14695E-08 0.19785E+00 
c  r23          0.39980E-02      19   0.73133E-08   0.12580E-08 0.19632E+00 
c  epsilon      0.10969E+02      11   0.32871E-08   0.95913E-02 0.16345E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.83790E-02 0.43173E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63362         0.61376       0.0052574       0.0015075
v  Velocity[Y]            -0.57354         0.54388       0.0030795      0.00087266
v  Velocity[Z]              1.5659          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4408          4.3406          4.3632
v  Pressure                -36.436          360.08          87.701          169.91
v  r11                   0.0010622        0.081971        0.013076        0.018287
v  r22                    0.001116        0.082596        0.013356        0.018647
v  r33                   0.0016444          0.1744        0.027256        0.037208
v  r12                   -0.010677        0.013593     -0.00023387     -0.00030934
v  r13                   -0.045514        0.052778      9.3335e-05       0.0010139
v  r23                   -0.046706        0.051282      3.0594e-05      0.00057464
v  epsilon                0.069565          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9894e-05        0.009918      0.00092532       0.0017428
v  CourantNb               0.44216             0.6         0.59908         0.59839
v  FourierNb             0.0017884          5.2779         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            11098:        0.68297E+02

===============================================================


 INSTANT    0.110990000E-01   TIME STEP NUMBER           11099
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.261511979E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.443387548E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.405631128E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935017E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184011651E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276765978E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81257E-03   0.45338E-02 0.19940E+01 
c  Velocity[X]                                      0.13828E-03 
c  Velocity[Y]                                      0.12803E-03 
c  Velocity[Z]                                      0.42675E-02 
c  Pressure     0.36584E-04     133   0.93162E-02   0.25804E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56458E-08   0.16241E-08 0.98473E-01 
c  r22          0.10853E-01      13   0.54327E-08   0.18375E-08 0.10070E+00 
c  r33          0.21861E-01      14   0.68017E-08   0.12510E-07 0.12597E+00 
c  r12          0.93878E-03      18   0.59561E-08   0.30120E-09 0.60679E+00 
c  r13          0.46678E-02      19   0.55700E-08   0.14938E-08 0.19886E+00 
c  r23          0.39980E-02      19   0.68040E-08   0.12756E-08 0.19728E+00 
c  epsilon      0.10969E+02      11   0.31848E-08   0.98852E-02 0.16412E+00 
c  TempC        0.25716E+06      16   0.15164E-04   0.84337E-02 0.43289E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61369       0.0052575       0.0015075
v  Velocity[Y]            -0.57373         0.54405       0.0030795      0.00087268
v  Velocity[Z]              1.5658          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4408          4.3406          4.3632
v  Pressure                -36.362          360.01          87.636          169.84
v  r11                   0.0010622        0.081984        0.013076        0.018287
v  r22                    0.001116        0.082596        0.013356        0.018647
v  r33                   0.0016444         0.17442        0.027256        0.037208
v  r12                   -0.010673        0.013601     -0.00023387     -0.00030934
v  r13                   -0.045512         0.05278      9.3336e-05       0.0010139
v  r23                   -0.046706        0.051263      3.0594e-05      0.00057464
v  epsilon                0.069566          271.27          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9891e-05       0.0099181      0.00092532       0.0017428
v  CourantNb               0.44219             0.6         0.59908         0.59839
v  FourierNb             0.0017884          5.2776         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11099:        0.67799E+02

===============================================================


 INSTANT    0.111000000E-01   TIME STEP NUMBER           11100
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229916749E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.251774389E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934904E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.820063098E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133138568E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.363396427E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81322E-03   0.45187E-02 0.19895E+01 
c  Velocity[X]                                      0.13831E-03 
c  Velocity[Y]                                      0.12786E-03 
c  Velocity[Z]                                      0.42525E-02 
c  Pressure     0.36134E-04     133   0.91944E-02   0.25486E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56257E-08   0.16226E-08 0.98680E-01 
c  r22          0.10853E-01      13   0.54727E-08   0.18217E-08 0.10054E+00 
c  r33          0.21861E-01      14   0.67624E-08   0.12514E-07 0.12614E+00 
c  r12          0.93878E-03      18   0.64175E-08   0.29673E-09 0.60364E+00 
c  r13          0.46678E-02      19   0.64309E-08   0.15063E-08 0.19909E+00 
c  r23          0.39980E-02      19   0.66443E-08   0.12783E-08 0.19747E+00 
c  epsilon      0.10969E+02      11   0.32350E-08   0.99850E-02 0.16603E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.83896E-02 0.43266E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61378       0.0052575       0.0015074
v  Velocity[Y]            -0.57369         0.54421       0.0030795       0.0008727
v  Velocity[Z]              1.5658          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4408          4.3406          4.3632
v  Pressure                  -36.4          360.03          87.647          169.85
v  r11                   0.0010622        0.082001        0.013076        0.018287
v  r22                    0.001116        0.082597        0.013356        0.018647
v  r33                   0.0016444         0.17438        0.027256        0.037208
v  r12                    -0.01067        0.013608     -0.00023387     -0.00030934
v  r13                   -0.045511        0.052781      9.3336e-05       0.0010139
v  r23                   -0.046708        0.051284      3.0594e-05      0.00057464
v  epsilon                0.069567          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9886e-05       0.0099181      0.00092532       0.0017428
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017884          5.2773         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            11100:        0.71642E+02

===============================================================


 INSTANT    0.111010000E-01   TIME STEP NUMBER           11101
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.429321389E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.368752576E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150064853E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.353580272E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.612734765E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81369E-03   0.44680E-02 0.19796E+01 
c  Velocity[X]                                      0.13723E-03 
c  Velocity[Y]                                      0.12746E-03 
c  Velocity[Z]                                      0.42033E-02 
c  Pressure     0.36191E-04     131   0.92093E-02   0.25527E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.50523E-08   0.16372E-08 0.98883E-01 
c  r22          0.10853E-01      13   0.52976E-08   0.17730E-08 0.99845E-01 
c  r33          0.21861E-01      14   0.67431E-08   0.12250E-07 0.12535E+00 
c  r12          0.93878E-03      18   0.55866E-08   0.30120E-09 0.60542E+00 
c  r13          0.46678E-02      19   0.58404E-08   0.14682E-08 0.19790E+00 
c  r23          0.39980E-02      19   0.60839E-08   0.12894E-08 0.19791E+00 
c  epsilon      0.10969E+02      11   0.33412E-08   0.94331E-02 0.16189E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.83690E-02 0.43175E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63357         0.61376       0.0052574       0.0015074
v  Velocity[Y]             -0.5737         0.54401       0.0030795      0.00087268
v  Velocity[Z]               1.566          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5798          5.4408          4.3406          4.3632
v  Pressure                -36.391          360.07          87.666          169.89
v  r11                   0.0010622        0.082013        0.013076        0.018287
v  r22                    0.001116        0.082598        0.013356        0.018647
v  r33                   0.0016444         0.17434        0.027256        0.037208
v  r12                    -0.01067        0.013611     -0.00023387     -0.00030934
v  r13                   -0.045515        0.052781      9.3337e-05       0.0010139
v  r23                   -0.046709        0.051272      3.0594e-05      0.00057464
v  epsilon                0.069569          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9885e-05        0.009918      0.00092532       0.0017428
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017884          5.2774         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71353         0.85285


 TIME FOR THE TIME STEP            11101:        0.71485E+02

===============================================================


 INSTANT    0.111020000E-01   TIME STEP NUMBER           11102
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.683209505E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.373816116E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934909E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153656757E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.956334705E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934910E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.809478758E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81239E-03   0.45166E-02 0.19904E+01 
c  Velocity[X]                                      0.13749E-03 
c  Velocity[Y]                                      0.12888E-03 
c  Velocity[Z]                                      0.42502E-02 
c  Pressure     0.36272E-04     133   0.92378E-02   0.25583E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57100E-08   0.16032E-08 0.97967E-01 
c  r22          0.10853E-01      13   0.53435E-08   0.17881E-08 0.10023E+00 
c  r33          0.21861E-01      15   0.55441E-08   0.12166E-07 0.12494E+00 
c  r12          0.93878E-03      18   0.56818E-08   0.29247E-09 0.60160E+00 
c  r13          0.46678E-02      19   0.61658E-08   0.14366E-08 0.19697E+00 
c  r23          0.39980E-02      19   0.63310E-08   0.12431E-08 0.19521E+00 
c  epsilon      0.10969E+02      11   0.32952E-08   0.96724E-02 0.16474E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.83765E-02 0.43134E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63363         0.61373       0.0052574       0.0015074
v  Velocity[Y]            -0.57358         0.54413       0.0030794      0.00087264
v  Velocity[Z]              1.5658          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4408          4.3406          4.3632
v  Pressure                -36.434          360.03          87.689          169.88
v  r11                   0.0010622        0.082017        0.013076        0.018287
v  r22                    0.001116        0.082598        0.013356        0.018647
v  r33                   0.0016444         0.17434        0.027256        0.037208
v  r12                    -0.01067        0.013613     -0.00023387     -0.00030934
v  r13                   -0.045511        0.052782      9.3337e-05       0.0010139
v  r23                    -0.04671        0.051255      3.0594e-05      0.00057464
v  epsilon                 0.06957          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9884e-05       0.0099179      0.00092533       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017884          5.2776         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11102:        0.70432E+02

===============================================================


 INSTANT    0.111030000E-01   TIME STEP NUMBER           11103
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.114016230E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.358964119E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.268020732E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935024E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.143140266E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.112444955E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81253E-03   0.45287E-02 0.19919E+01 
c  Velocity[X]                                      0.13714E-03 
c  Velocity[Y]                                      0.12776E-03 
c  Velocity[Z]                                      0.42638E-02 
c  Pressure     0.35681E-04     131   0.90837E-02   0.25167E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58552E-08   0.16402E-08 0.98974E-01 
c  r22          0.10853E-01      13   0.54033E-08   0.18161E-08 0.10023E+00 
c  r33          0.21861E-01      15   0.60306E-08   0.12689E-07 0.12703E+00 
c  r12          0.93878E-03      18   0.62324E-08   0.29871E-09 0.60230E+00 
c  r13          0.46678E-02      19   0.64229E-08   0.15049E-08 0.19968E+00 
c  r23          0.39980E-02      19   0.66178E-08   0.13082E-08 0.20024E+00 
c  epsilon      0.10969E+02      11   0.34695E-08   0.10362E-01 0.17263E+00 
c  TempC        0.25716E+06      16   0.15114E-04   0.84495E-02 0.43385E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61379       0.0052574       0.0015074
v  Velocity[Y]            -0.57369         0.54389       0.0030795      0.00087267
v  Velocity[Z]              1.5656          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4408          4.3406          4.3632
v  Pressure                -36.378          360.06           87.65          169.87
v  r11                   0.0010622        0.082016        0.013076        0.018287
v  r22                   0.0011161        0.082598        0.013356        0.018647
v  r33                   0.0016444         0.17435        0.027256        0.037208
v  r12                   -0.010667         0.01361     -0.00023387     -0.00030934
v  r13                   -0.045511        0.052783      9.3337e-05       0.0010139
v  r23                   -0.046711        0.051267      3.0594e-05      0.00057465
v  epsilon                0.069571          271.26          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9885e-05       0.0099178      0.00092533       0.0017428
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017885          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            11103:        0.66351E+02

===============================================================


 INSTANT    0.111040000E-01   TIME STEP NUMBER           11104
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.969526639E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.306882043E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179279019E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.260483336E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.288270320E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81275E-03   0.44775E-02 0.19796E+01 
c  Velocity[X]                                      0.13682E-03 
c  Velocity[Y]                                      0.12637E-03 
c  Velocity[Z]                                      0.42143E-02 
c  Pressure     0.35952E-04     131   0.91506E-02   0.25357E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61739E-08   0.16492E-08 0.98935E-01 
c  r22          0.10853E-01      13   0.53362E-08   0.18417E-08 0.10096E+00 
c  r33          0.21861E-01      15   0.61427E-08   0.12640E-07 0.12662E+00 
c  r12          0.93878E-03      18   0.65923E-08   0.30198E-09 0.60642E+00 
c  r13          0.46678E-02      19   0.64333E-08   0.14977E-08 0.19910E+00 
c  r23          0.39980E-02      19   0.63262E-08   0.12903E-08 0.19884E+00 
c  epsilon      0.10969E+02      11   0.34215E-08   0.10083E-01 0.16680E+00 
c  TempC        0.25716E+06      16   0.15178E-04   0.83639E-02 0.43179E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161984


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61376       0.0052574       0.0015074
v  Velocity[Y]            -0.57373         0.54393       0.0030794      0.00087263
v  Velocity[Z]              1.5657          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4408          4.3406          4.3632
v  Pressure                -36.454          360.04          87.649          169.85
v  r11                   0.0010622        0.082012        0.013076        0.018287
v  r22                   0.0011161        0.082599        0.013356        0.018647
v  r33                   0.0016444         0.17438        0.027256        0.037208
v  r12                   -0.010673        0.013607     -0.00023387     -0.00030934
v  r13                   -0.045514        0.052783      9.3337e-05       0.0010139
v  r23                   -0.046711         0.05124      3.0594e-05      0.00057465
v  epsilon                0.069572          271.28          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9883e-05       0.0099178      0.00092533       0.0017428
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017885          5.2774         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            11104:        0.68301E+02

===============================================================


 INSTANT    0.111050000E-01   TIME STEP NUMBER           11105
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.468261637E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168742106E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.402384558E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.103619589E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205465561E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81284E-03   0.45018E-02 0.19861E+01 
c  Velocity[X]                                      0.13722E-03 
c  Velocity[Y]                                      0.12701E-03 
c  Velocity[Z]                                      0.42376E-02 
c  Pressure     0.36432E-04     133   0.92723E-02   0.25696E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.62893E-08   0.16152E-08 0.98230E-01 
c  r22          0.10853E-01      13   0.50767E-08   0.18329E-08 0.10048E+00 
c  r33          0.21861E-01      15   0.56010E-08   0.12456E-07 0.12573E+00 
c  r12          0.93878E-03      18   0.61723E-08   0.29253E-09 0.60062E+00 
c  r13          0.46678E-02      19   0.68064E-08   0.15073E-08 0.19917E+00 
c  r23          0.39980E-02      19   0.55454E-08   0.12689E-08 0.19689E+00 
c  epsilon      0.10969E+02      11   0.34098E-08   0.99490E-02 0.16475E+00 
c  TempC        0.25716E+06      16   0.15129E-04   0.83849E-02 0.43193E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63357         0.61376       0.0052574       0.0015074
v  Velocity[Y]            -0.57381         0.54408       0.0030795      0.00087266
v  Velocity[Z]              1.5659          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4408          4.3406          4.3632
v  Pressure                -36.408          360.08          87.678           169.9
v  r11                   0.0010622        0.081999        0.013076        0.018287
v  r22                   0.0011161          0.0826        0.013356        0.018647
v  r33                   0.0016444          0.1744        0.027256        0.037208
v  r12                   -0.010675        0.013609     -0.00023387     -0.00030934
v  r13                   -0.045513        0.052783      9.3338e-05       0.0010139
v  r23                   -0.046712         0.05122      3.0594e-05      0.00057465
v  epsilon                0.069573          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9884e-05       0.0099177      0.00092533       0.0017428
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017885          5.2777         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            11105:        0.68607E+02

===============================================================


 INSTANT    0.111060000E-01   TIME STEP NUMBER           11106
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.254782558E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.115286070E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.225211162E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.301656671E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.613904407E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81348E-03   0.45106E-02 0.19897E+01 
c  Velocity[X]                                      0.13785E-03 
c  Velocity[Y]                                      0.12818E-03 
c  Velocity[Z]                                      0.42446E-02 
c  Pressure     0.36196E-04     133   0.92147E-02   0.25530E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61629E-08   0.16379E-08 0.98961E-01 
c  r22          0.10853E-01      13   0.48389E-08   0.18059E-08 0.10008E+00 
c  r33          0.21861E-01      15   0.52268E-08   0.12428E-07 0.12597E+00 
c  r12          0.93878E-03      18   0.59308E-08   0.29909E-09 0.60405E+00 
c  r13          0.46678E-02      19   0.70766E-08   0.14909E-08 0.19868E+00 
c  r23          0.39980E-02      18   0.70131E-08   0.12827E-08 0.19825E+00 
c  epsilon      0.10969E+02      11   0.32418E-08   0.98013E-02 0.16445E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.84720E-02 0.43392E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361         0.61376       0.0052574       0.0015074
v  Velocity[Y]             -0.5738         0.54421       0.0030794      0.00087266
v  Velocity[Z]              1.5659          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4408          4.3406          4.3632
v  Pressure                -36.417          359.99          87.646          169.83
v  r11                   0.0010622        0.081986        0.013076        0.018287
v  r22                   0.0011161          0.0826        0.013356        0.018647
v  r33                   0.0016444         0.17441        0.027256        0.037208
v  r12                   -0.010676         0.01361     -0.00023387     -0.00030934
v  r13                   -0.045511        0.052782      9.3338e-05       0.0010139
v  r23                   -0.046713        0.051204      3.0593e-05      0.00057465
v  epsilon                0.069574          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9881e-05       0.0099177      0.00092533       0.0017428
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017885          5.2781         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            11106:        0.70106E+02

===============================================================


 INSTANT    0.111070000E-01   TIME STEP NUMBER           11107
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.249163053E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.401800906E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.306388958E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166484089E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.247307908E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81256E-03   0.45214E-02 0.19899E+01 
c  Velocity[X]                                      0.13687E-03 
c  Velocity[Y]                                      0.12824E-03 
c  Velocity[Z]                                      0.42563E-02 
c  Pressure     0.36331E-04     133   0.92470E-02   0.25625E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61931E-08   0.15939E-08 0.97437E-01 
c  r22          0.10853E-01      13   0.47562E-08   0.17915E-08 0.99886E-01 
c  r33          0.21861E-01      15   0.55923E-08   0.12219E-07 0.12496E+00 
c  r12          0.93878E-03      18   0.68783E-08   0.29210E-09 0.59898E+00 
c  r13          0.46678E-02      19   0.68340E-08   0.14558E-08 0.19721E+00 
c  r23          0.39980E-02      18   0.70279E-08   0.12589E-08 0.19528E+00 
c  epsilon      0.10969E+02      11   0.32398E-08   0.95514E-02 0.16169E+00 
c  TempC        0.25716E+06      16   0.15121E-04   0.83723E-02 0.43125E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61376       0.0052574       0.0015074
v  Velocity[Y]            -0.57378         0.54405       0.0030795      0.00087268
v  Velocity[Z]              1.5657          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4408          4.3406          4.3632
v  Pressure                -36.401          360.06          87.665          169.88
v  r11                   0.0010622        0.081972        0.013076        0.018287
v  r22                   0.0011161        0.082601        0.013356        0.018647
v  r33                   0.0016444         0.17437        0.027256        0.037208
v  r12                   -0.010672        0.013604     -0.00023387     -0.00030934
v  r13                   -0.045513        0.052782      9.3338e-05       0.0010139
v  r23                   -0.046712        0.051216      3.0593e-05      0.00057465
v  epsilon                0.069575          271.26          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.988e-05       0.0099177      0.00092533       0.0017428
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017885          5.2773         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            11107:        0.70799E+02

===============================================================


 INSTANT    0.111080000E-01   TIME STEP NUMBER           11108
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.135728974E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.257920536E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.194909672E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.121121249E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.305497049E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81319E-03   0.44699E-02 0.19790E+01 
c  Velocity[X]                                      0.13662E-03 
c  Velocity[Y]                                      0.12641E-03 
c  Velocity[Z]                                      0.42069E-02 
c  Pressure     0.36142E-04     133   0.91925E-02   0.25491E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60208E-08   0.16094E-08 0.97770E-01 
c  r22          0.10853E-01      13   0.47670E-08   0.18077E-08 0.99889E-01 
c  r33          0.21861E-01      15   0.70902E-08   0.12405E-07 0.12531E+00 
c  r12          0.93878E-03      18   0.65037E-08   0.29453E-09 0.59946E+00 
c  r13          0.46678E-02      19   0.72621E-08   0.14769E-08 0.19784E+00 
c  r23          0.39980E-02      18   0.68271E-08   0.12719E-08 0.19636E+00 
c  epsilon      0.10969E+02      11   0.35632E-08   0.99400E-02 0.16535E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.83533E-02 0.43127E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63358         0.61376       0.0052574       0.0015074
v  Velocity[Y]            -0.57378         0.54418       0.0030795      0.00087269
v  Velocity[Z]              1.5657          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4408          4.3406          4.3632
v  Pressure                -36.412          359.94          87.599          169.78
v  r11                   0.0010622         0.08196        0.013076        0.018287
v  r22                   0.0011161          0.0826        0.013356        0.018647
v  r33                   0.0016444         0.17434        0.027256        0.037208
v  r12                   -0.010678        0.013604     -0.00023387     -0.00030934
v  r13                   -0.045511        0.052781      9.3338e-05       0.0010139
v  r23                   -0.046712        0.051207      3.0593e-05      0.00057465
v  epsilon                0.069576          271.27          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9877e-05       0.0099176      0.00092533       0.0017428
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017885          5.2786         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            11108:        0.67231E+02

===============================================================


 INSTANT    0.111090000E-01   TIME STEP NUMBER           11109
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267845889E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229367217E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.146332730E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.195735389E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.691659116E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81273E-03   0.45319E-02 0.19934E+01 
c  Velocity[X]                                      0.13855E-03 
c  Velocity[Y]                                      0.12828E-03 
c  Velocity[Z]                                      0.42651E-02 
c  Pressure     0.36311E-04     133   0.92418E-02   0.25612E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.62847E-08   0.16290E-08 0.98939E-01 
c  r22          0.10853E-01      13   0.50229E-08   0.18070E-08 0.10037E+00 
c  r33          0.21861E-01      15   0.67483E-08   0.12443E-07 0.12641E+00 
c  r12          0.93878E-03      18   0.70032E-08   0.30260E-09 0.60780E+00 
c  r13          0.46678E-02      19   0.66628E-08   0.14830E-08 0.19849E+00 
c  r23          0.39980E-02      18   0.65871E-08   0.12855E-08 0.19875E+00 
c  epsilon      0.10969E+02      11   0.33331E-08   0.10005E-01 0.16929E+00 
c  TempC        0.25716E+06      16   0.15169E-04   0.84047E-02 0.43252E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161988


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6336         0.61378       0.0052574       0.0015074
v  Velocity[Y]            -0.57385         0.54418       0.0030795       0.0008727
v  Velocity[Z]              1.5657          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4408          4.3406          4.3632
v  Pressure                -36.395          360.09          87.686           169.9
v  r11                   0.0010622        0.081952        0.013076        0.018287
v  r22                   0.0011161        0.082601        0.013356        0.018647
v  r33                   0.0016445         0.17434        0.027256        0.037208
v  r12                   -0.010677          0.0136     -0.00023387     -0.00030934
v  r13                   -0.045512        0.052782      9.3339e-05       0.0010139
v  r23                   -0.046711        0.051199      3.0593e-05      0.00057465
v  epsilon                0.069577          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9875e-05       0.0099176      0.00092533       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017886          5.2789         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            11109:        0.68305E+02

===============================================================


 INSTANT    0.111100000E-01   TIME STEP NUMBER           11110
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.226410345E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.321254420E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.114334040E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.137111167E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.262467732E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81296E-03   0.44754E-02 0.19803E+01 
c  Velocity[X]                                      0.13651E-03 
c  Velocity[Y]                                      0.12694E-03 
c  Velocity[Z]                                      0.42120E-02 
c  Pressure     0.35878E-04     132   0.91302E-02   0.25304E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.62551E-08   0.16144E-08 0.98442E-01 
c  r22          0.10853E-01      13   0.54289E-08   0.17839E-08 0.10015E+00 
c  r33          0.21861E-01      15   0.56725E-08   0.12221E-07 0.12555E+00 
c  r12          0.93878E-03      19   0.55810E-08   0.29422E-09 0.60137E+00 
c  r13          0.46678E-02      19   0.73100E-08   0.14667E-08 0.19818E+00 
c  r23          0.39980E-02      19   0.56619E-08   0.12625E-08 0.19677E+00 
c  epsilon      0.10969E+02      11   0.32045E-08   0.93755E-02 0.16159E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.83706E-02 0.43177E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61378       0.0052574       0.0015074
v  Velocity[Y]            -0.57366         0.54424       0.0030794      0.00087263
v  Velocity[Z]              1.5659          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4408          4.3406          4.3632
v  Pressure                -36.443          360.04          87.666          169.87
v  r11                   0.0010622        0.081947        0.013076        0.018287
v  r22                   0.0011161        0.082602        0.013356        0.018647
v  r33                   0.0016445         0.17436        0.027256        0.037208
v  r12                   -0.010675          0.0136     -0.00023387     -0.00030934
v  r13                   -0.045514        0.052785      9.3338e-05       0.0010139
v  r23                   -0.046712        0.051219      3.0593e-05      0.00057465
v  epsilon                0.069579          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9875e-05       0.0099175      0.00092533       0.0017428
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017886           5.278         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71353         0.85284


 TIME FOR THE TIME STEP            11110:        0.70698E+02

===============================================================


 INSTANT    0.111110000E-01   TIME STEP NUMBER           11111
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.191902065E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.850484865E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.101770862E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179778711E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154084201E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81308E-03   0.45246E-02 0.19918E+01 
c  Velocity[X]                                      0.13762E-03 
c  Velocity[Y]                                      0.12815E-03 
c  Velocity[Z]                                      0.42588E-02 
c  Pressure     0.36515E-04     132   0.92957E-02   0.25754E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60705E-08   0.16227E-08 0.98151E-01 
c  r22          0.10853E-01      13   0.58068E-08   0.18603E-08 0.10126E+00 
c  r33          0.21861E-01      14   0.67250E-08   0.12727E-07 0.12675E+00 
c  r12          0.93878E-03      19   0.62160E-08   0.29868E-09 0.60085E+00 
c  r13          0.46678E-02      20   0.58357E-08   0.15323E-08 0.20044E+00 
c  r23          0.39980E-02      19   0.51949E-08   0.12789E-08 0.19702E+00 
c  epsilon      0.10969E+02      11   0.33564E-08   0.10467E-01 0.16774E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.84361E-02 0.43314E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361         0.61377       0.0052574       0.0015074
v  Velocity[Y]            -0.57367         0.54431       0.0030794      0.00087264
v  Velocity[Z]               1.566          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4408          4.3406          4.3632
v  Pressure                -36.367          360.06          87.654          169.87
v  r11                   0.0010622        0.081943        0.013076        0.018287
v  r22                   0.0011161        0.082601        0.013356        0.018647
v  r33                   0.0016445         0.17438        0.027256        0.037208
v  r12                   -0.010671        0.013607     -0.00023387     -0.00030934
v  r13                   -0.045511        0.052785       9.334e-05       0.0010139
v  r23                   -0.046712        0.051205      3.0593e-05      0.00057465
v  epsilon                 0.06958          271.26          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9876e-05       0.0099175      0.00092533       0.0017428
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017886          5.2778         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85284


 TIME FOR THE TIME STEP            11111:        0.70006E+02

===============================================================


 INSTANT    0.111120000E-01   TIME STEP NUMBER           11112
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.545722032E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.254430600E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.472710416E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.247027047E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172681311E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81333E-03   0.45068E-02 0.19886E+01 
c  Velocity[X]                                      0.13711E-03 
c  Velocity[Y]                                      0.12742E-03 
c  Velocity[Z]                                      0.42422E-02 
c  Pressure     0.35896E-04     132   0.91366E-02   0.25318E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57255E-08   0.16371E-08 0.98357E-01 
c  r22          0.10853E-01      13   0.55826E-08   0.18049E-08 0.10017E+00 
c  r33          0.21861E-01      15   0.61789E-08   0.12485E-07 0.12587E+00 
c  r12          0.93878E-03      19   0.63632E-08   0.29912E-09 0.60261E+00 
c  r13          0.46678E-02      20   0.69577E-08   0.15004E-08 0.19954E+00 
c  r23          0.39980E-02      18   0.70796E-08   0.12873E-08 0.19753E+00 
c  epsilon      0.10969E+02      11   0.35556E-08   0.99939E-02 0.16664E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.84066E-02 0.43279E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63368          0.6138       0.0052574       0.0015074
v  Velocity[Y]            -0.57357         0.54406       0.0030794      0.00087267
v  Velocity[Z]              1.5657          5.4408          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4408          4.3406          4.3632
v  Pressure                -36.464          360.06          87.688          169.89
v  r11                   0.0010622        0.081936        0.013076        0.018287
v  r22                   0.0011161        0.082604        0.013356        0.018647
v  r33                   0.0016445         0.17439        0.027256        0.037208
v  r12                   -0.010667        0.013604     -0.00023387     -0.00030934
v  r13                    -0.04551        0.052782       9.334e-05       0.0010139
v  r23                   -0.046712        0.051187      3.0593e-05      0.00057465
v  epsilon                0.069581          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9874e-05       0.0099175      0.00092533       0.0017428
v  CourantNb                0.4422             0.6         0.59908         0.59839
v  FourierNb             0.0017886           5.278         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            11112:        0.69337E+02

===============================================================


 INSTANT    0.111130000E-01   TIME STEP NUMBER           11113
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.279619188E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.726230584E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.307368162E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.290249319E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.305455204E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81286E-03   0.44708E-02 0.19809E+01 
c  Velocity[X]                                      0.13684E-03 
c  Velocity[Y]                                      0.12678E-03 
c  Velocity[Z]                                      0.42071E-02 
c  Pressure     0.36079E-04     131   0.91847E-02   0.25446E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58741E-08   0.16146E-08 0.97961E-01 
c  r22          0.10853E-01      13   0.51155E-08   0.17825E-08 0.99447E-01 
c  r33          0.21861E-01      15   0.60090E-08   0.12300E-07 0.12485E+00 
c  r12          0.93878E-03      19   0.61105E-08   0.29433E-09 0.59831E+00 
c  r13          0.46678E-02      20   0.67927E-08   0.14704E-08 0.19737E+00 
c  r23          0.39980E-02      19   0.54994E-08   0.12841E-08 0.19730E+00 
c  epsilon      0.10969E+02      11   0.35250E-08   0.98872E-02 0.16538E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.83479E-02 0.43150E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61379       0.0052574       0.0015074
v  Velocity[Y]            -0.57376         0.54412       0.0030794      0.00087266
v  Velocity[Z]              1.5658          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4409          4.3406          4.3632
v  Pressure                -36.406          360.02          87.641          169.85
v  r11                   0.0010622        0.081926        0.013076        0.018287
v  r22                   0.0011161        0.082605        0.013356        0.018647
v  r33                   0.0016445         0.17441        0.027256        0.037208
v  r12                   -0.010664        0.013605     -0.00023387     -0.00030934
v  r13                   -0.045513         0.05278       9.334e-05       0.0010139
v  r23                   -0.046712        0.051202      3.0592e-05      0.00057465
v  epsilon                0.069582          271.26          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9879e-05       0.0099174      0.00092533       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017886          5.2782         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            11113:        0.69047E+02

===============================================================


 INSTANT    0.111140000E-01   TIME STEP NUMBER           11114
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.587196178E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.230019380E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934913E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.152847814E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.118891862E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.287406581E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81358E-03   0.45047E-02 0.19902E+01 
c  Velocity[X]                                      0.13734E-03 
c  Velocity[Y]                                      0.12763E-03 
c  Velocity[Z]                                      0.42397E-02 
c  Pressure     0.36403E-04     133   0.92613E-02   0.25676E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56230E-08   0.16101E-08 0.98104E-01 
c  r22          0.10853E-01      13   0.52355E-08   0.18018E-08 0.99854E-01 
c  r33          0.21861E-01      15   0.63773E-08   0.12283E-07 0.12510E+00 
c  r12          0.93878E-03      19   0.55818E-08   0.29160E-09 0.59971E+00 
c  r13          0.46678E-02      20   0.63083E-08   0.14596E-08 0.19712E+00 
c  r23          0.39980E-02      19   0.56046E-08   0.12462E-08 0.19589E+00 
c  epsilon      0.10969E+02      11   0.34221E-08   0.97609E-02 0.16389E+00 
c  TempC        0.25716E+06      16   0.15173E-04   0.84332E-02 0.43205E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61379       0.0052574       0.0015074
v  Velocity[Y]            -0.57373          0.5443       0.0030794      0.00087264
v  Velocity[Z]               1.566          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5798          5.4409          4.3406          4.3632
v  Pressure                -36.432          359.99          87.644          169.83
v  r11                   0.0010622        0.081923        0.013076        0.018287
v  r22                   0.0011161        0.082605        0.013356        0.018647
v  r33                   0.0016445         0.17442        0.027256        0.037208
v  r12                   -0.010666         0.01361     -0.00023387     -0.00030934
v  r13                    -0.04551        0.052779       9.334e-05       0.0010139
v  r23                   -0.046712        0.051188      3.0592e-05      0.00057465
v  epsilon                0.069583          271.28          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9882e-05       0.0099175      0.00092533       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017887          5.2783         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71352         0.85284


 TIME FOR THE TIME STEP            11114:        0.71249E+02

===============================================================


 INSTANT    0.111150000E-01   TIME STEP NUMBER           11115
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.686133220E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.104301903E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.131051714E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.350321254E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.249391902E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81271E-03   0.45106E-02 0.19868E+01 
c  Velocity[X]                                      0.13780E-03 
c  Velocity[Y]                                      0.12742E-03 
c  Velocity[Z]                                      0.42454E-02 
c  Pressure     0.36255E-04     132   0.92283E-02   0.25573E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54964E-08   0.16299E-08 0.98865E-01 
c  r22          0.10853E-01      13   0.51942E-08   0.18082E-08 0.10056E+00 
c  r33          0.21861E-01      15   0.56214E-08   0.12416E-07 0.12630E+00 
c  r12          0.93878E-03      19   0.52790E-08   0.29324E-09 0.60279E+00 
c  r13          0.46678E-02      20   0.60597E-08   0.14758E-08 0.19840E+00 
c  r23          0.39980E-02      19   0.58733E-08   0.12661E-08 0.19866E+00 
c  epsilon      0.10969E+02      11   0.33322E-08   0.99352E-02 0.16814E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.84354E-02 0.43376E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61381       0.0052574       0.0015074
v  Velocity[Y]            -0.57381           0.544       0.0030795      0.00087273
v  Velocity[Z]              1.5658          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4409          4.3406          4.3632
v  Pressure                -36.402          360.05          87.654          169.88
v  r11                   0.0010622        0.081912        0.013076        0.018287
v  r22                   0.0011161        0.082604        0.013356        0.018647
v  r33                   0.0016445         0.17443        0.027256        0.037208
v  r12                   -0.010669        0.013604     -0.00023387     -0.00030934
v  r13                    -0.04551        0.052779       9.334e-05       0.0010139
v  r23                   -0.046712         0.05118      3.0591e-05      0.00057465
v  epsilon                0.069584          271.29          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9888e-05       0.0099177      0.00092533       0.0017428
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017887          5.2782         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            11115:        0.68355E+02

===============================================================


 INSTANT    0.111160000E-01   TIME STEP NUMBER           11116
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.142843438E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.260249696E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.425240773E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.466389493E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276165131E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81425E-03   0.44685E-02 0.19777E+01 
c  Velocity[X]                                      0.13652E-03 
c  Velocity[Y]                                      0.12779E-03 
c  Velocity[Z]                                      0.42041E-02 
c  Pressure     0.36070E-04     133   0.91876E-02   0.25441E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54394E-08   0.16288E-08 0.98232E-01 
c  r22          0.10853E-01      13   0.54497E-08   0.18179E-08 0.10063E+00 
c  r33          0.21861E-01      14   0.67924E-08   0.12510E-07 0.12623E+00 
c  r12          0.93878E-03      18   0.67591E-08   0.29352E-09 0.60130E+00 
c  r13          0.46678E-02      19   0.70356E-08   0.14852E-08 0.19907E+00 
c  r23          0.39980E-02      19   0.58291E-08   0.12837E-08 0.19846E+00 
c  epsilon      0.10969E+02      11   0.32116E-08   0.10103E-01 0.16674E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.83512E-02 0.43188E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63358          0.6138       0.0052575       0.0015075
v  Velocity[Y]            -0.57379         0.54401       0.0030794      0.00087268
v  Velocity[Z]              1.5656          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4409          4.3406          4.3632
v  Pressure                -36.452          359.96          87.606           169.8
v  r11                   0.0010622        0.081909        0.013076        0.018287
v  r22                   0.0011161        0.082603        0.013356        0.018647
v  r33                   0.0016445         0.17439        0.027256        0.037208
v  r12                    -0.01067        0.013601     -0.00023387     -0.00030934
v  r13                   -0.045513        0.052782      9.3341e-05       0.0010139
v  r23                   -0.046713        0.051201      3.0591e-05      0.00057465
v  epsilon                0.069586          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9894e-05       0.0099174      0.00092533       0.0017428
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017887          5.2792         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8792         0.71352         0.85284


 TIME FOR THE TIME STEP            11116:        0.70948E+02

===============================================================


 INSTANT    0.111170000E-01   TIME STEP NUMBER           11117
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.987521905E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.416977679E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.104917149E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130764061E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108363337E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81202E-03   0.45111E-02 0.19901E+01 
c  Velocity[X]                                      0.13676E-03 
c  Velocity[Y]                                      0.12797E-03 
c  Velocity[Z]                                      0.42464E-02 
c  Pressure     0.36460E-04     133   0.92888E-02   0.25716E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51325E-08   0.16268E-08 0.98566E-01 
c  r22          0.10853E-01      13   0.56258E-08   0.18148E-08 0.10053E+00 
c  r33          0.21861E-01      15   0.53981E-08   0.12473E-07 0.12583E+00 
c  r12          0.93878E-03      18   0.68724E-08   0.29442E-09 0.60200E+00 
c  r13          0.46678E-02      19   0.61211E-08   0.14842E-08 0.19902E+00 
c  r23          0.39980E-02      19   0.56125E-08   0.12928E-08 0.19857E+00 
c  epsilon      0.10969E+02      11   0.33500E-08   0.98274E-02 0.16341E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.84194E-02 0.43281E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61379       0.0052574       0.0015074
v  Velocity[Y]            -0.57364         0.54411       0.0030794      0.00087265
v  Velocity[Z]              1.5657          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4409          4.3406          4.3632
v  Pressure                 -36.42          360.04          87.643          169.86
v  r11                   0.0010622        0.081915        0.013076        0.018287
v  r22                   0.0011161        0.082599        0.013356        0.018647
v  r33                   0.0016445         0.17435        0.027256        0.037208
v  r12                   -0.010671        0.013605     -0.00023387     -0.00030934
v  r13                   -0.045512        0.052787      9.3341e-05       0.0010139
v  r23                   -0.046713        0.051186       3.059e-05      0.00057465
v  epsilon                0.069587           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc               5.99e-05       0.0099174      0.00092533       0.0017428
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017887          5.2793         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8793         0.71352         0.85284


 TIME FOR THE TIME STEP            11117:        0.71173E+02

===============================================================


 INSTANT    0.111180000E-01   TIME STEP NUMBER           11118
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.177405734E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.627692017E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.251380756E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.144738550E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.299719718E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      39   0.81352E-03   0.45227E-02 0.19909E+01 
c  Velocity[X]                                      0.13786E-03 
c  Velocity[Y]                                      0.12802E-03 
c  Velocity[Z]                                      0.42568E-02 
c  Pressure     0.35938E-04     131   0.91527E-02   0.25347E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.50876E-08   0.16316E-08 0.98171E-01 
c  r22          0.10853E-01      13   0.56004E-08   0.18218E-08 0.10006E+00 
c  r33          0.21861E-01      15   0.67091E-08   0.12547E-07 0.12580E+00 
c  r12          0.93878E-03      18   0.68233E-08   0.29063E-09 0.59851E+00 
c  r13          0.46678E-02      20   0.58117E-08   0.14945E-08 0.19936E+00 
c  r23          0.39980E-02      19   0.65823E-08   0.12839E-08 0.19787E+00 
c  epsilon      0.10969E+02      11   0.35862E-08   0.10179E-01 0.16609E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.84201E-02 0.43254E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61382       0.0052574       0.0015074
v  Velocity[Y]            -0.57358         0.54425       0.0030794      0.00087265
v  Velocity[Z]              1.5656          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4409          4.3406          4.3632
v  Pressure                 -36.46          360.02          87.658          169.85
v  r11                   0.0010622        0.081917        0.013076        0.018287
v  r22                   0.0011161        0.082602        0.013356        0.018647
v  r33                   0.0016445         0.17434        0.027256        0.037208
v  r12                   -0.010671        0.013606     -0.00023387     -0.00030934
v  r13                    -0.04551        0.052788      9.3342e-05       0.0010139
v  r23                   -0.046714        0.051168      3.0591e-05      0.00057465
v  epsilon                0.069588          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9905e-05       0.0099174      0.00092533       0.0017428
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017887          5.2789         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            11118:        0.71621E+02

===============================================================


 INSTANT    0.111190000E-01   TIME STEP NUMBER           11119
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.264011344E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.131664778E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.172420754E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.151712425E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.297047303E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81270E-03   0.44704E-02 0.19806E+01 
c  Velocity[X]                                      0.13623E-03 
c  Velocity[Y]                                      0.12707E-03 
c  Velocity[Z]                                      0.42071E-02 
c  Pressure     0.36374E-04     133   0.92639E-02   0.25655E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53273E-08   0.16379E-08 0.98860E-01 
c  r22          0.10853E-01      13   0.54899E-08   0.17844E-08 0.99904E-01 
c  r33          0.21861E-01      15   0.64884E-08   0.12289E-07 0.12574E+00 
c  r12          0.93878E-03      18   0.71913E-08   0.30349E-09 0.60714E+00 
c  r13          0.46678E-02      20   0.67279E-08   0.14571E-08 0.19746E+00 
c  r23          0.39980E-02      19   0.70865E-08   0.12812E-08 0.19909E+00 
c  epsilon      0.10969E+02      11   0.35338E-08   0.97210E-02 0.16485E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.84092E-02 0.43239E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63355         0.61382       0.0052575       0.0015075
v  Velocity[Y]            -0.57354         0.54404       0.0030794      0.00087269
v  Velocity[Z]              1.5658          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4409          4.3406          4.3632
v  Pressure                -36.408          360.04          87.643          169.86
v  r11                   0.0010622        0.081927        0.013076        0.018287
v  r22                   0.0011161        0.082604        0.013356        0.018647
v  r33                   0.0016445         0.17435        0.027256        0.037208
v  r12                   -0.010672        0.013607     -0.00023387     -0.00030934
v  r13                   -0.045512        0.052786      9.3342e-05       0.0010139
v  r23                   -0.046715        0.051195       3.059e-05      0.00057465
v  epsilon                0.069589          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9909e-05       0.0099174      0.00092533       0.0017429
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017887          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            11119:        0.71470E+02

===============================================================


 INSTANT    0.111200000E-01   TIME STEP NUMBER           11120
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.324108410E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.872175531E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934918E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.345336948E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.449768831E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.370841203E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81342E-03   0.45393E-02 0.19945E+01 
c  Velocity[X]                                      0.13651E-03 
c  Velocity[Y]                                      0.12782E-03 
c  Velocity[Z]                                      0.42749E-02 
c  Pressure     0.36690E-04     133   0.93376E-02   0.25878E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56896E-08   0.16069E-08 0.97930E-01 
c  r22          0.10853E-01      13   0.50641E-08   0.18213E-08 0.10036E+00 
c  r33          0.21861E-01      15   0.57133E-08   0.12394E-07 0.12562E+00 
c  r12          0.93878E-03      18   0.63810E-08   0.29410E-09 0.60033E+00 
c  r13          0.46678E-02      20   0.75122E-08   0.14951E-08 0.19862E+00 
c  r23          0.39980E-02      19   0.72357E-08   0.12682E-08 0.19734E+00 
c  epsilon      0.10969E+02      11   0.34914E-08   0.99570E-02 0.16695E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.83828E-02 0.43218E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63363         0.61379       0.0052575       0.0015075
v  Velocity[Y]            -0.57343         0.54412       0.0030794      0.00087267
v  Velocity[Z]              1.5658          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4409          4.3406          4.3632
v  Pressure                -36.447          360.01          87.646          169.85
v  r11                   0.0010622         0.08193        0.013076        0.018287
v  r22                   0.0011161        0.082606        0.013356        0.018647
v  r33                   0.0016445         0.17438        0.027256        0.037208
v  r12                   -0.010679        0.013607     -0.00023387     -0.00030934
v  r13                    -0.04551        0.052786      9.3342e-05       0.0010139
v  r23                   -0.046716         0.05119       3.059e-05      0.00057465
v  epsilon                 0.06959          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9908e-05       0.0099174      0.00092533       0.0017429
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017887          5.2776         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11120:        0.70297E+02

===============================================================


 INSTANT    0.111210000E-01   TIME STEP NUMBER           11121
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.704828923E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158440791E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.674895081E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.185790854E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.112916513E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81288E-03   0.45047E-02 0.19891E+01 
c  Velocity[X]                                      0.13821E-03 
c  Velocity[Y]                                      0.12748E-03 
c  Velocity[Z]                                      0.42390E-02 
c  Pressure     0.36147E-04     132   0.91934E-02   0.25496E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55903E-08   0.16284E-08 0.98794E-01 
c  r22          0.10853E-01      13   0.51558E-08   0.17939E-08 0.10014E+00 
c  r33          0.21861E-01      15   0.55404E-08   0.12390E-07 0.12620E+00 
c  r12          0.93878E-03      18   0.63987E-08   0.29776E-09 0.60455E+00 
c  r13          0.46678E-02      20   0.70043E-08   0.14872E-08 0.19901E+00 
c  r23          0.39980E-02      19   0.66963E-08   0.12861E-08 0.19964E+00 
c  epsilon      0.10969E+02      11   0.33598E-08   0.10066E-01 0.16961E+00 
c  TempC        0.25716E+06      16   0.15142E-04   0.84188E-02 0.43307E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61381       0.0052574       0.0015074
v  Velocity[Y]            -0.57356         0.54429       0.0030794      0.00087269
v  Velocity[Z]              1.5657          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4409          4.3406          4.3632
v  Pressure                -36.418          359.95          87.596          169.79
v  r11                   0.0010622        0.081938        0.013076        0.018287
v  r22                   0.0011161        0.082604        0.013356        0.018647
v  r33                   0.0016445          0.1744        0.027256        0.037208
v  r12                   -0.010677         0.01361     -0.00023387     -0.00030934
v  r13                   -0.045511        0.052787      9.3343e-05       0.0010139
v  r23                   -0.046717        0.051183      3.0591e-05      0.00057465
v  epsilon                0.069591          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9907e-05       0.0099175      0.00092534       0.0017429
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017888           5.277         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.877         0.71352         0.85284


 TIME FOR THE TIME STEP            11121:        0.67796E+02

===============================================================


 INSTANT    0.111220000E-01   TIME STEP NUMBER           11122
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.440877927E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.200905893E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934906E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.189459533E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.342522340E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.894050109E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81367E-03   0.44598E-02 0.19775E+01 
c  Velocity[X]                                      0.13610E-03 
c  Velocity[Y]                                      0.12754E-03 
c  Velocity[Z]                                      0.41962E-02 
c  Pressure     0.36238E-04     131   0.92187E-02   0.25559E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54608E-08   0.16280E-08 0.97880E-01 
c  r22          0.10853E-01      13   0.53410E-08   0.18049E-08 0.99914E-01 
c  r33          0.21861E-01      15   0.56603E-08   0.12430E-07 0.12529E+00 
c  r12          0.93878E-03      18   0.58675E-08   0.29349E-09 0.59980E+00 
c  r13          0.46678E-02      20   0.74469E-08   0.14961E-08 0.19838E+00 
c  r23          0.39980E-02      19   0.62656E-08   0.12844E-08 0.19707E+00 
c  epsilon      0.10969E+02      11   0.32214E-08   0.10063E-01 0.16613E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83836E-02 0.43206E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63355          0.6138       0.0052575       0.0015075
v  Velocity[Y]            -0.57352         0.54401       0.0030794      0.00087264
v  Velocity[Z]              1.5655          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4409          4.3406          4.3632
v  Pressure                -36.448          360.01          87.652          169.85
v  r11                   0.0010622        0.081945        0.013076        0.018287
v  r22                   0.0011161        0.082607        0.013356        0.018647
v  r33                   0.0016445         0.17441        0.027256        0.037208
v  r12                   -0.010677        0.013607     -0.00023387     -0.00030934
v  r13                   -0.045513        0.052787      9.3343e-05       0.0010139
v  r23                   -0.046718        0.051204       3.059e-05      0.00057465
v  epsilon                0.069593          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9903e-05       0.0099175      0.00092534       0.0017429
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017888          5.2765         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8765         0.71352         0.85284


 TIME FOR THE TIME STEP            11122:        0.68913E+02

===============================================================


 INSTANT    0.111230000E-01   TIME STEP NUMBER           11123
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.142939290E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.436705413E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.187443362E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.269100083E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155799536E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33839E+00
   Friction velocity        uk    :  0.11554E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81273E-03   0.45076E-02 0.19855E+01 
c  Velocity[X]                                      0.13755E-03 
c  Velocity[Y]                                      0.12720E-03 
c  Velocity[Z]                                      0.42429E-02 
c  Pressure     0.36302E-04     131   0.92415E-02   0.25604E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57288E-08   0.16027E-08 0.97238E-01 
c  r22          0.10853E-01      13   0.54675E-08   0.18105E-08 0.10013E+00 
c  r33          0.21861E-01      14   0.67411E-08   0.12390E-07 0.12537E+00 
c  r12          0.93878E-03      18   0.55611E-08   0.29195E-09 0.59876E+00 
c  r13          0.46678E-02      20   0.70846E-08   0.14840E-08 0.19844E+00 
c  r23          0.39980E-02      19   0.63463E-08   0.12732E-08 0.19660E+00 
c  epsilon      0.10969E+02      11   0.31839E-08   0.98492E-02 0.16386E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.83936E-02 0.43198E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63363         0.61379       0.0052575       0.0015074
v  Velocity[Y]            -0.57367         0.54402       0.0030793      0.00087264
v  Velocity[Z]              1.5657          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4409          4.3406          4.3632
v  Pressure                -36.409          360.03          87.656          169.87
v  r11                   0.0010622        0.081954        0.013076        0.018287
v  r22                   0.0011161        0.082609        0.013356        0.018647
v  r33                   0.0016446         0.17442        0.027256        0.037208
v  r12                   -0.010675         0.01361     -0.00023387     -0.00030934
v  r13                   -0.045511        0.052784      9.3344e-05       0.0010139
v  r23                   -0.046719        0.051186      3.0591e-05      0.00057465
v  epsilon                0.069594          271.27          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc               5.99e-05       0.0099176      0.00092534       0.0017429
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017888          5.2763         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8763         0.71352         0.85285


 TIME FOR THE TIME STEP            11123:        0.69726E+02

===============================================================


 INSTANT    0.111240000E-01   TIME STEP NUMBER           11124
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.788025613E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.288085845E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.359944382E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.242244591E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.130399933E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81327E-03   0.45236E-02 0.19906E+01 
c  Velocity[X]                                      0.13690E-03 
c  Velocity[Y]                                      0.12776E-03 
c  Velocity[Z]                                      0.42589E-02 
c  Pressure     0.36618E-04     132   0.93183E-02   0.25828E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56448E-08   0.16518E-08 0.98393E-01 
c  r22          0.10853E-01      13   0.55605E-08   0.18602E-08 0.10062E+00 
c  r33          0.21861E-01      15   0.68495E-08   0.12872E-07 0.12697E+00 
c  r12          0.93878E-03      18   0.57092E-08   0.30128E-09 0.60232E+00 
c  r13          0.46678E-02      20   0.69391E-08   0.15323E-08 0.20012E+00 
c  r23          0.39980E-02      19   0.59599E-08   0.13129E-08 0.19946E+00 
c  epsilon      0.10969E+02      11   0.35288E-08   0.10804E-01 0.17079E+00 
c  TempC        0.25716E+06      16   0.15184E-04   0.84337E-02 0.43293E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61382       0.0052575       0.0015074
v  Velocity[Y]            -0.57369         0.54409       0.0030794      0.00087266
v  Velocity[Z]              1.5658          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4409          4.3406          4.3632
v  Pressure                -36.455          360.03          87.664          169.87
v  r11                   0.0010622         0.08195        0.013076        0.018287
v  r22                   0.0011161        0.082609        0.013356        0.018647
v  r33                   0.0016446         0.17439        0.027256        0.037208
v  r12                    -0.01067        0.013612     -0.00023387     -0.00030934
v  r13                    -0.04551        0.052783      9.3345e-05       0.0010139
v  r23                    -0.04672        0.051174      3.0591e-05      0.00057465
v  epsilon                0.069595          271.27          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9896e-05       0.0099175      0.00092534       0.0017429
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017888          5.2764         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8764         0.71352         0.85284


 TIME FOR THE TIME STEP            11124:        0.71180E+02

===============================================================


 INSTANT    0.111250000E-01   TIME STEP NUMBER           11125
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181104344E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.663785685E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.408530433E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.316574213E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157597390E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81282E-03   0.44873E-02 0.19840E+01 
c  Velocity[X]                                      0.13652E-03 
c  Velocity[Y]                                      0.12796E-03 
c  Velocity[Z]                                      0.42228E-02 
c  Pressure     0.35961E-04     131   0.91573E-02   0.25364E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60549E-08   0.16138E-08 0.97990E-01 
c  r22          0.10853E-01      13   0.59805E-08   0.17851E-08 0.99848E-01 
c  r33          0.21861E-01      16   0.59282E-08   0.12195E-07 0.12523E+00 
c  r12          0.93879E-03      18   0.67743E-08   0.29845E-09 0.60050E+00 
c  r13          0.46678E-02      20   0.71543E-08   0.14750E-08 0.19803E+00 
c  r23          0.39980E-02      19   0.60819E-08   0.12732E-08 0.19703E+00 
c  epsilon      0.10969E+02      11   0.37330E-08   0.94620E-02 0.16154E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.83404E-02 0.43072E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344          0.6138       0.0052575       0.0015074
v  Velocity[Y]            -0.57382         0.54421       0.0030793      0.00087261
v  Velocity[Z]              1.5656          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4409          4.3406          4.3632
v  Pressure                -36.402          360.04           87.65          169.86
v  r11                   0.0010623        0.081956        0.013076        0.018287
v  r22                   0.0011161        0.082609        0.013356        0.018647
v  r33                   0.0016446         0.17435        0.027256        0.037208
v  r12                   -0.010671        0.013609     -0.00023387     -0.00030934
v  r13                   -0.045514        0.052782      9.3345e-05       0.0010139
v  r23                   -0.046721          0.0512      3.0591e-05      0.00057465
v  epsilon                0.069596          271.26          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9895e-05       0.0099176      0.00092534       0.0017429
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017888          5.2766         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71352         0.85284


 TIME FOR THE TIME STEP            11125:        0.71791E+02

===============================================================


 INSTANT    0.111260000E-01   TIME STEP NUMBER           11126
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.242769076E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117675801E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.333502177E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.361792026E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.451795702E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81360E-03   0.45000E-02 0.19875E+01 
c  Velocity[X]                                      0.13752E-03 
c  Velocity[Y]                                      0.12763E-03 
c  Velocity[Z]                                      0.42348E-02 
c  Pressure     0.36140E-04     133   0.91962E-02   0.25490E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61345E-08   0.15950E-08 0.97604E-01 
c  r22          0.10853E-01      13   0.55838E-08   0.17833E-08 0.99814E-01 
c  r33          0.21861E-01      16   0.60275E-08   0.12176E-07 0.12491E+00 
c  r12          0.93879E-03      18   0.65264E-08   0.28698E-09 0.59594E+00 
c  r13          0.46678E-02      20   0.65432E-08   0.14557E-08 0.19741E+00 
c  r23          0.39980E-02      19   0.74162E-08   0.12502E-08 0.19601E+00 
c  epsilon      0.10969E+02      11   0.38367E-08   0.96418E-02 0.16325E+00 
c  TempC        0.25716E+06      16   0.15177E-04   0.83576E-02 0.43164E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353          0.6138       0.0052574       0.0015074
v  Velocity[Y]             -0.5737         0.54405       0.0030793      0.00087264
v  Velocity[Z]              1.5657          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4409          4.3406          4.3632
v  Pressure                -36.441          360.02          87.654          169.85
v  r11                   0.0010623        0.081954        0.013076        0.018287
v  r22                   0.0011161        0.082608        0.013356        0.018647
v  r33                   0.0016446         0.17434        0.027256        0.037208
v  r12                   -0.010671        0.013613     -0.00023387     -0.00030934
v  r13                   -0.045511        0.052784      9.3345e-05       0.0010139
v  r23                   -0.046721        0.051198       3.059e-05      0.00057465
v  epsilon                0.069597          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9893e-05       0.0099176      0.00092534       0.0017429
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017888          5.2768         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71352         0.85284


 TIME FOR THE TIME STEP            11126:        0.70597E+02

===============================================================


 INSTANT    0.111270000E-01   TIME STEP NUMBER           11127
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.185216917E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.502036930E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.263084297E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.498148467E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.104159164E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81297E-03   0.45201E-02 0.19908E+01 
c  Velocity[X]                                      0.13813E-03 
c  Velocity[Y]                                      0.12785E-03 
c  Velocity[Z]                                      0.42541E-02 
c  Pressure     0.36131E-04     132   0.91996E-02   0.25483E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59472E-08   0.16322E-08 0.98363E-01 
c  r22          0.10853E-01      13   0.54158E-08   0.18298E-08 0.10018E+00 
c  r33          0.21861E-01      15   0.56523E-08   0.12613E-07 0.12643E+00 
c  r12          0.93879E-03      18   0.61508E-08   0.29272E-09 0.59971E+00 
c  r13          0.46678E-02      20   0.57461E-08   0.14974E-08 0.19867E+00 
c  r23          0.39980E-02      19   0.65016E-08   0.13026E-08 0.19952E+00 
c  epsilon      0.10969E+02      11   0.35643E-08   0.10251E-01 0.17044E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.84818E-02 0.43455E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63357         0.61382       0.0052575       0.0015074
v  Velocity[Y]             -0.5737         0.54407       0.0030793      0.00087264
v  Velocity[Z]              1.5657          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4409          4.3406          4.3632
v  Pressure                -36.404          360.05          87.657          169.87
v  r11                   0.0010623        0.081955        0.013076        0.018287
v  r22                   0.0011161        0.082609        0.013356        0.018647
v  r33                   0.0016446         0.17436        0.027256        0.037208
v  r12                   -0.010668        0.013619     -0.00023387     -0.00030934
v  r13                   -0.045509        0.052786      9.3346e-05       0.0010139
v  r23                   -0.046722        0.051189      3.0591e-05      0.00057465
v  epsilon                0.069598          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9891e-05       0.0099176      0.00092534       0.0017429
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017889          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            11127:        0.71462E+02

===============================================================


 INSTANT    0.111280000E-01   TIME STEP NUMBER           11128
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115576444E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.313844136E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.806035982E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.651887312E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.406990801E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81360E-03   0.44539E-02 0.19741E+01 
c  Velocity[X]                                      0.13656E-03 
c  Velocity[Y]                                      0.12709E-03 
c  Velocity[Z]                                      0.41903E-02 
c  Pressure     0.36093E-04     133   0.91924E-02   0.25455E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59711E-08   0.16058E-08 0.97351E-01 
c  r22          0.10853E-01      13   0.57335E-08   0.17956E-08 0.99794E-01 
c  r33          0.21861E-01      15   0.58932E-08   0.12310E-07 0.12509E+00 
c  r12          0.93879E-03      18   0.60912E-08   0.29542E-09 0.59912E+00 
c  r13          0.46678E-02      19   0.74150E-08   0.14819E-08 0.19867E+00 
c  r23          0.39980E-02      19   0.66996E-08   0.12697E-08 0.19629E+00 
c  epsilon      0.10969E+02      11   0.33775E-08   0.97946E-02 0.16344E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.83931E-02 0.43264E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61386       0.0052574       0.0015073
v  Velocity[Y]            -0.57359         0.54407       0.0030793      0.00087262
v  Velocity[Z]              1.5657          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4409          4.3406          4.3632
v  Pressure                -36.445          360.02           87.64          169.85
v  r11                   0.0010623        0.081948        0.013076        0.018287
v  r22                   0.0011161         0.08261        0.013356        0.018647
v  r33                   0.0016446         0.17438        0.027256        0.037208
v  r12                   -0.010667        0.013617     -0.00023387     -0.00030934
v  r13                   -0.045512        0.052788      9.3346e-05       0.0010139
v  r23                   -0.046722         0.05119      3.0591e-05      0.00057465
v  epsilon                  0.0696          271.27          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9887e-05       0.0099176      0.00092534       0.0017429
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017889          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            11128:        0.72800E+02

===============================================================


 INSTANT    0.111290000E-01   TIME STEP NUMBER           11129
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.380104326E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108280087E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172336795E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.655352728E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.404791529E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69773E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81228E-03   0.45507E-02 0.19967E+01 
c  Velocity[X]                                      0.13816E-03 
c  Velocity[Y]                                      0.12849E-03 
c  Velocity[Z]                                      0.42841E-02 
c  Pressure     0.36783E-04     132   0.93622E-02   0.25945E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55186E-08   0.16074E-08 0.97752E-01 
c  r22          0.10853E-01      13   0.57115E-08   0.18089E-08 0.99905E-01 
c  r33          0.21861E-01      15   0.57853E-08   0.12424E-07 0.12544E+00 
c  r12          0.93879E-03      18   0.62087E-08   0.28973E-09 0.59576E+00 
c  r13          0.46678E-02      19   0.65983E-08   0.14880E-08 0.19810E+00 
c  r23          0.39980E-02      19   0.61442E-08   0.12833E-08 0.19725E+00 
c  epsilon      0.10969E+02      11   0.32580E-08   0.99774E-02 0.16503E+00 
c  TempC        0.25716E+06      16   0.15166E-04   0.84222E-02 0.43246E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63344         0.61393       0.0052573       0.0015073
v  Velocity[Y]            -0.57353         0.54417       0.0030793      0.00087262
v  Velocity[Z]              1.5657          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4409          4.3406          4.3632
v  Pressure                -36.407          360.05          87.676          169.88
v  r11                   0.0010623        0.081941        0.013076        0.018287
v  r22                   0.0011161        0.082609        0.013356        0.018647
v  r33                   0.0016446          0.1744        0.027256        0.037208
v  r12                   -0.010665         0.01362     -0.00023387     -0.00030934
v  r13                   -0.045512        0.052789      9.3347e-05       0.0010139
v  r23                   -0.046722        0.051216      3.0591e-05      0.00057465
v  epsilon                0.069601           271.3          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9885e-05       0.0099177      0.00092534       0.0017429
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017889          5.2777         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            11129:        0.71075E+02

===============================================================


 INSTANT    0.111300000E-01   TIME STEP NUMBER           11130
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.308436148E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.344915219E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.512387986E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133241103E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.885634386E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81322E-03   0.45123E-02 0.19913E+01 
c  Velocity[X]                                      0.13690E-03 
c  Velocity[Y]                                      0.12770E-03 
c  Velocity[Z]                                      0.42477E-02 
c  Pressure     0.35949E-04     132   0.91538E-02   0.25355E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56300E-08   0.16228E-08 0.98295E-01 
c  r22          0.10853E-01      13   0.53110E-08   0.18300E-08 0.10032E+00 
c  r33          0.21861E-01      15   0.59742E-08   0.12523E-07 0.12610E+00 
c  r12          0.93879E-03      18   0.59689E-08   0.29440E-09 0.60139E+00 
c  r13          0.46678E-02      19   0.70299E-08   0.15176E-08 0.19956E+00 
c  r23          0.39980E-02      19   0.65357E-08   0.12783E-08 0.19782E+00 
c  epsilon      0.10969E+02      11   0.33047E-08   0.99963E-02 0.16518E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.84266E-02 0.43279E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63354         0.61394       0.0052573       0.0015073
v  Velocity[Y]            -0.57351         0.54424       0.0030793      0.00087261
v  Velocity[Z]              1.5655          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4409          4.3406          4.3632
v  Pressure                -36.445          359.99           87.65          169.84
v  r11                   0.0010623         0.08193        0.013076        0.018287
v  r22                   0.0011161        0.082612        0.013356        0.018647
v  r33                   0.0016446         0.17441        0.027256        0.037208
v  r12                   -0.010668        0.013621     -0.00023387     -0.00030934
v  r13                    -0.04551        0.052785      9.3348e-05       0.0010139
v  r23                   -0.046723        0.051216      3.0591e-05      0.00057465
v  epsilon                0.069602          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9882e-05       0.0099178      0.00092534       0.0017429
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017889           5.278         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            11130:        0.71021E+02

===============================================================


 INSTANT    0.111310000E-01   TIME STEP NUMBER           11131
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169885420E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.373640932E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.910787438E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.784449908E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153324066E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11244E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81339E-03   0.44800E-02 0.19823E+01 
c  Velocity[X]                                      0.13632E-03 
c  Velocity[Y]                                      0.12759E-03 
c  Velocity[Z]                                      0.42160E-02 
c  Pressure     0.36090E-04     137   0.91852E-02   0.25455E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57448E-08   0.15956E-08 0.97415E-01 
c  r22          0.10853E-01      13   0.54071E-08   0.17749E-08 0.99308E-01 
c  r33          0.21861E-01      15   0.62753E-08   0.12292E-07 0.12517E+00 
c  r12          0.93879E-03      18   0.58710E-08   0.29402E-09 0.60031E+00 
c  r13          0.46678E-02      19   0.59564E-08   0.14989E-08 0.19808E+00 
c  r23          0.39980E-02      19   0.65283E-08   0.12782E-08 0.19667E+00 
c  epsilon      0.10969E+02      11   0.34589E-08   0.96310E-02 0.16272E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.83506E-02 0.43126E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61397       0.0052574       0.0015074
v  Velocity[Y]            -0.57339         0.54404       0.0030793      0.00087264
v  Velocity[Z]              1.5654          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4409          4.3406          4.3632
v  Pressure                 -36.41          360.06          87.667          169.89
v  r11                   0.0010623        0.081913        0.013076        0.018287
v  r22                   0.0011161        0.082613        0.013356        0.018647
v  r33                   0.0016446         0.17442        0.027256        0.037208
v  r12                   -0.010671        0.013613     -0.00023387     -0.00030934
v  r13                   -0.045511         0.05278      9.3349e-05       0.0010139
v  r23                   -0.046723         0.05121      3.0592e-05      0.00057465
v  epsilon                0.069603          271.26          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9882e-05       0.0099176      0.00092534       0.0017429
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017889          5.2784         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85284


 TIME FOR THE TIME STEP            11131:        0.71589E+02

===============================================================


 INSTANT    0.111320000E-01   TIME STEP NUMBER           11132
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.105929079E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.297496407E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.126678998E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.174936521E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.442177166E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69772E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81312E-03   0.44847E-02 0.19827E+01 
c  Velocity[X]                                      0.13673E-03 
c  Velocity[Y]                                      0.12823E-03 
c  Velocity[Z]                                      0.42198E-02 
c  Pressure     0.36305E-04     133   0.92380E-02   0.25607E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54529E-08   0.16140E-08 0.97524E-01 
c  r22          0.10853E-01      13   0.55270E-08   0.18300E-08 0.10001E+00 
c  r33          0.21861E-01      15   0.56383E-08   0.12452E-07 0.12533E+00 
c  r12          0.93879E-03      18   0.55625E-08   0.29309E-09 0.59966E+00 
c  r13          0.46678E-02      19   0.61375E-08   0.14871E-08 0.19772E+00 
c  r23          0.39980E-02      19   0.66434E-08   0.12704E-08 0.19692E+00 
c  epsilon      0.10969E+02      11   0.33043E-08   0.10042E-01 0.16633E+00 
c  TempC        0.25716E+06      16   0.15149E-04   0.83682E-02 0.43185E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61391       0.0052574       0.0015074
v  Velocity[Y]            -0.57342         0.54403       0.0030792      0.00087261
v  Velocity[Z]              1.5658          5.4409          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4409          4.3406          4.3632
v  Pressure                -36.447          359.99          87.644          169.83
v  r11                   0.0010623        0.081904        0.013076        0.018287
v  r22                   0.0011161        0.082611        0.013356        0.018647
v  r33                   0.0016446         0.17443        0.027256        0.037208
v  r12                   -0.010671        0.013615     -0.00023387     -0.00030934
v  r13                   -0.045509        0.052778      9.3349e-05       0.0010139
v  r23                   -0.046723        0.051225      3.0592e-05      0.00057465
v  epsilon                0.069604          271.29          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.988e-05       0.0099177      0.00092534       0.0017429
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017889           5.278         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            11132:        0.70612E+02

===============================================================


 INSTANT    0.111330000E-01   TIME STEP NUMBER           11133
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136465331E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.156798588E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.293338840E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.262321408E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.158559529E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81167E-03   0.45207E-02 0.19916E+01 
c  Velocity[X]                                      0.13845E-03 
c  Velocity[Y]                                      0.12816E-03 
c  Velocity[Z]                                      0.42541E-02 
c  Pressure     0.36361E-04     132   0.92586E-02   0.25646E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53195E-08   0.16338E-08 0.98604E-01 
c  r22          0.10853E-01      13   0.55418E-08   0.17938E-08 0.99710E-01 
c  r33          0.21861E-01      15   0.60314E-08   0.12394E-07 0.12582E+00 
c  r12          0.93879E-03      18   0.56587E-08   0.30043E-09 0.60681E+00 
c  r13          0.46678E-02      19   0.61302E-08   0.14805E-08 0.19792E+00 
c  r23          0.39980E-02      19   0.61811E-08   0.12830E-08 0.19859E+00 
c  epsilon      0.10969E+02      11   0.32437E-08   0.98146E-02 0.16789E+00 
c  TempC        0.25716E+06      16   0.15147E-04   0.84224E-02 0.43347E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61391       0.0052574       0.0015074
v  Velocity[Y]            -0.57357         0.54422       0.0030793      0.00087264
v  Velocity[Z]              1.5656           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5794           5.441          4.3406          4.3632
v  Pressure                -36.433          360.08          87.681           169.9
v  r11                   0.0010623          0.0819        0.013076        0.018287
v  r22                   0.0011161        0.082609        0.013356        0.018647
v  r33                   0.0016446         0.17445        0.027256        0.037208
v  r12                   -0.010669         0.01362     -0.00023387     -0.00030934
v  r13                   -0.045509        0.052777       9.335e-05       0.0010139
v  r23                   -0.046724        0.051208      3.0592e-05      0.00057465
v  epsilon                0.069605           271.3          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.988e-05       0.0099177      0.00092534       0.0017429
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb              0.001789          5.2782         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            11133:        0.69701E+02

===============================================================


 INSTANT    0.111340000E-01   TIME STEP NUMBER           11134
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.196309898E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.354211075E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.713270704E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.134921354E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.560017693E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69771E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81335E-03   0.45008E-02 0.19863E+01 
c  Velocity[X]                                      0.13649E-03 
c  Velocity[Y]                                      0.12753E-03 
c  Velocity[Z]                                      0.42368E-02 
c  Pressure     0.36073E-04     132   0.91822E-02   0.25442E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53615E-08   0.16498E-08 0.98460E-01 
c  r22          0.10853E-01      13   0.52026E-08   0.18163E-08 0.10024E+00 
c  r33          0.21861E-01      15   0.56765E-08   0.12621E-07 0.12638E+00 
c  r12          0.93879E-03      18   0.51458E-08   0.30196E-09 0.60425E+00 
c  r13          0.46678E-02      19   0.53843E-08   0.14848E-08 0.19875E+00 
c  r23          0.39980E-02      19   0.57865E-08   0.12903E-08 0.19792E+00 
c  epsilon      0.10969E+02      11   0.32137E-08   0.10113E-01 0.16661E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.83860E-02 0.43171E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61392       0.0052573       0.0015073
v  Velocity[Y]            -0.57345         0.54404       0.0030792      0.00087261
v  Velocity[Z]              1.5656           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5794           5.441          4.3406          4.3632
v  Pressure                 -36.42          359.99          87.635          169.83
v  r11                   0.0010623        0.081896        0.013076        0.018287
v  r22                   0.0011161        0.082608        0.013356        0.018647
v  r33                   0.0016446          0.1744        0.027256        0.037208
v  r12                   -0.010675        0.013617     -0.00023387     -0.00030934
v  r13                   -0.045512         0.05278      9.3351e-05       0.0010139
v  r23                   -0.046724        0.051188      3.0592e-05      0.00057465
v  epsilon                0.069607          271.29          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9882e-05       0.0099178      0.00092534       0.0017429
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb              0.001789          5.2779         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            11134:        0.70642E+02

===============================================================


 INSTANT    0.111350000E-01   TIME STEP NUMBER           11135
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.247296002E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.823951700E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.163314423E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.194510715E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.245419801E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81255E-03   0.45046E-02 0.19879E+01 
c  Velocity[X]                                      0.13684E-03 
c  Velocity[Y]                                      0.12835E-03 
c  Velocity[Z]                                      0.42395E-02 
c  Pressure     0.36242E-04     132   0.92275E-02   0.25562E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52971E-08   0.16038E-08 0.97603E-01 
c  r22          0.10853E-01      13   0.54283E-08   0.18260E-08 0.10021E+00 
c  r33          0.21861E-01      15   0.63804E-08   0.12447E-07 0.12592E+00 
c  r12          0.93879E-03      18   0.57781E-08   0.29584E-09 0.60295E+00 
c  r13          0.46678E-02      19   0.63472E-08   0.15152E-08 0.19923E+00 
c  r23          0.39980E-02      19   0.56910E-08   0.12836E-08 0.19792E+00 
c  epsilon      0.10969E+02      11   0.34877E-08   0.98391E-02 0.16493E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84128E-02 0.43224E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61394       0.0052574       0.0015074
v  Velocity[Y]            -0.57345         0.54417       0.0030793      0.00087261
v  Velocity[Z]              1.5655           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5793           5.441          4.3406          4.3632
v  Pressure                -36.364          360.01          87.637          169.84
v  r11                   0.0010623         0.08189        0.013076        0.018287
v  r22                   0.0011161        0.082607        0.013356        0.018647
v  r33                   0.0016446         0.17435        0.027256        0.037208
v  r12                   -0.010673         0.01362     -0.00023387     -0.00030934
v  r13                    -0.04551        0.052778      9.3351e-05       0.0010139
v  r23                   -0.046724        0.051205      3.0592e-05      0.00057465
v  epsilon                0.069608          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9884e-05       0.0099178      0.00092534       0.0017429
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb              0.001789          5.2782         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            11135:        0.70591E+02

===============================================================


 INSTANT    0.111360000E-01   TIME STEP NUMBER           11136
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140230705E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.259832785E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.902808251E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.240011453E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.904737581E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81379E-03   0.44716E-02 0.19832E+01 
c  Velocity[X]                                      0.13742E-03 
c  Velocity[Y]                                      0.12724E-03 
c  Velocity[Z]                                      0.42070E-02 
c  Pressure     0.36413E-04     131   0.92679E-02   0.25683E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57199E-08   0.16490E-08 0.98474E-01 
c  r22          0.10853E-01      13   0.54325E-08   0.18236E-08 0.10021E+00 
c  r33          0.21861E-01      15   0.54800E-08   0.12607E-07 0.12618E+00 
c  r12          0.93879E-03      18   0.60396E-08   0.29880E-09 0.60325E+00 
c  r13          0.46678E-02      19   0.73406E-08   0.15144E-08 0.19992E+00 
c  r23          0.39980E-02      19   0.71220E-08   0.13004E-08 0.19829E+00 
c  epsilon      0.10969E+02      11   0.34446E-08   0.10116E-01 0.16761E+00 
c  TempC        0.25716E+06      16   0.15179E-04   0.83929E-02 0.43282E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346          0.6139       0.0052573       0.0015073
v  Velocity[Y]            -0.57326         0.54416       0.0030792      0.00087258
v  Velocity[Z]              1.5653           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5791           5.441          4.3406          4.3632
v  Pressure                -36.469          360.04          87.663          169.86
v  r11                   0.0010623        0.081886        0.013076        0.018287
v  r22                   0.0011161        0.082606        0.013356        0.018647
v  r33                   0.0016446         0.17435        0.027256        0.037208
v  r12                   -0.010669        0.013614     -0.00023387     -0.00030934
v  r13                   -0.045508         0.05278      9.3352e-05       0.0010139
v  r23                   -0.046725        0.051194      3.0593e-05      0.00057465
v  epsilon                0.069609          271.26          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9884e-05       0.0099177      0.00092534       0.0017429
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb              0.001789          5.2777         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            11136:        0.72765E+02

===============================================================


 INSTANT    0.111370000E-01   TIME STEP NUMBER           11137
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169303016E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201998069E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.233729635E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.484014367E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.131175322E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81324E-03   0.45033E-02 0.19837E+01 
c  Velocity[X]                                      0.13692E-03 
c  Velocity[Y]                                      0.12788E-03 
c  Velocity[Z]                                      0.42385E-02 
c  Pressure     0.36278E-04     131   0.92331E-02   0.25587E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58664E-08   0.16215E-08 0.97868E-01 
c  r22          0.10853E-01      13   0.53958E-08   0.18231E-08 0.10017E+00 
c  r33          0.21861E-01      15   0.54579E-08   0.12425E-07 0.12536E+00 
c  r12          0.93879E-03      18   0.64345E-08   0.30073E-09 0.60583E+00 
c  r13          0.46678E-02      19   0.70231E-08   0.14975E-08 0.19877E+00 
c  r23          0.39980E-02      20   0.60172E-08   0.12750E-08 0.19677E+00 
c  epsilon      0.10969E+02      11   0.33480E-08   0.99740E-02 0.16587E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.83734E-02 0.43180E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61395       0.0052573       0.0015073
v  Velocity[Y]            -0.57342         0.54421       0.0030792      0.00087259
v  Velocity[Z]              1.5655           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5793           5.441          4.3406          4.3632
v  Pressure                -36.351          360.04          87.655          169.86
v  r11                   0.0010623        0.081879        0.013076        0.018287
v  r22                   0.0011161        0.082603        0.013356        0.018647
v  r33                   0.0016447         0.17436        0.027256        0.037208
v  r12                   -0.010664        0.013611     -0.00023387     -0.00030934
v  r13                   -0.045512        0.052781      9.3352e-05       0.0010139
v  r23                   -0.046725        0.051182      3.0593e-05      0.00057465
v  epsilon                 0.06961          271.29          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9888e-05       0.0099177      0.00092534       0.0017429
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb              0.001789          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            11137:        0.68018E+02

===============================================================


 INSTANT    0.111380000E-01   TIME STEP NUMBER           11138
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.873504577E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.112331123E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.153257523E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282860267E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.144386749E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81303E-03   0.45182E-02 0.19910E+01 
c  Velocity[X]                                      0.13786E-03 
c  Velocity[Y]                                      0.12845E-03 
c  Velocity[Z]                                      0.42519E-02 
c  Pressure     0.37029E-04     132   0.94263E-02   0.26117E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57771E-08   0.16349E-08 0.98559E-01 
c  r22          0.10853E-01      13   0.52972E-08   0.18153E-08 0.10019E+00 
c  r33          0.21861E-01      15   0.51660E-08   0.12512E-07 0.12619E+00 
c  r12          0.93879E-03      18   0.63065E-08   0.30225E-09 0.60544E+00 
c  r13          0.46678E-02      19   0.62805E-08   0.14985E-08 0.19934E+00 
c  r23          0.39980E-02      20   0.55728E-08   0.12869E-08 0.19851E+00 
c  epsilon      0.10969E+02      11   0.32236E-08   0.10266E-01 0.17047E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.84223E-02 0.43309E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61398       0.0052573       0.0015073
v  Velocity[Y]            -0.57339         0.54424       0.0030791      0.00087258
v  Velocity[Z]              1.5656           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5793           5.441          4.3406          4.3632
v  Pressure                -36.405          360.05          87.695          169.88
v  r11                   0.0010623        0.081876        0.013076        0.018287
v  r22                   0.0011161        0.082604        0.013356        0.018647
v  r33                   0.0016447         0.17438        0.027256        0.037208
v  r12                   -0.010663        0.013609     -0.00023387     -0.00030934
v  r13                   -0.045509         0.05278      9.3352e-05       0.0010139
v  r23                   -0.046725        0.051195      3.0593e-05      0.00057465
v  epsilon                0.069611          271.29          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.989e-05       0.0099178      0.00092534       0.0017429
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb              0.001789          5.2767         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767         0.71352         0.85284


 TIME FOR THE TIME STEP            11138:        0.70270E+02

===============================================================


 INSTANT    0.111390000E-01   TIME STEP NUMBER           11139
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.689575618E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.116992092E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.236542294E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935027E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.373905256E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.156049267E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81259E-03   0.45287E-02 0.19932E+01 
c  Velocity[X]                                      0.13771E-03 
c  Velocity[Y]                                      0.12784E-03 
c  Velocity[Z]                                      0.42631E-02 
c  Pressure     0.36241E-04     132   0.92238E-02   0.25563E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55933E-08   0.16205E-08 0.98276E-01 
c  r22          0.10853E-01      13   0.53228E-08   0.17888E-08 0.99292E-01 
c  r33          0.21861E-01      15   0.56033E-08   0.12317E-07 0.12507E+00 
c  r12          0.93879E-03      18   0.64598E-08   0.29411E-09 0.60074E+00 
c  r13          0.46678E-02      19   0.63331E-08   0.14709E-08 0.19736E+00 
c  r23          0.39980E-02      19   0.70523E-08   0.12595E-08 0.19635E+00 
c  epsilon      0.10969E+02      11   0.32794E-08   0.98090E-02 0.16436E+00 
c  TempC        0.25716E+06      16   0.15124E-04   0.84423E-02 0.43333E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61402       0.0052574       0.0015074
v  Velocity[Y]            -0.57344         0.54403       0.0030792      0.00087262
v  Velocity[Z]              1.5655           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5793           5.441          4.3406          4.3632
v  Pressure                -36.411          360.06          87.657          169.87
v  r11                   0.0010623        0.081868        0.013076        0.018287
v  r22                   0.0011161        0.082606        0.013356        0.018647
v  r33                   0.0016447          0.1744        0.027256        0.037208
v  r12                   -0.010663         0.01361     -0.00023388     -0.00030934
v  r13                   -0.045508         0.05278      9.3353e-05       0.0010139
v  r23                   -0.046725        0.051174      3.0593e-05      0.00057465
v  epsilon                0.069612          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9893e-05       0.0099178      0.00092534       0.0017429
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017891          5.2764         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8764         0.71352         0.85284


 TIME FOR THE TIME STEP            11139:        0.70121E+02

===============================================================


 INSTANT    0.111400000E-01   TIME STEP NUMBER           11140
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.256418247E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.175374344E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.668397521E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.268248047E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149921727E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11245E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81307E-03   0.44722E-02 0.19788E+01 
c  Velocity[X]                                      0.13587E-03 
c  Velocity[Y]                                      0.12658E-03 
c  Velocity[Z]                                      0.42098E-02 
c  Pressure     0.36093E-04     133   0.91888E-02   0.25458E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58371E-08   0.16015E-08 0.97659E-01 
c  r22          0.10853E-01      13   0.48675E-08   0.18399E-08 0.10062E+00 
c  r33          0.21861E-01      15   0.56931E-08   0.12533E-07 0.12598E+00 
c  r12          0.93879E-03      18   0.60052E-08   0.29754E-09 0.60219E+00 
c  r13          0.46678E-02      19   0.58254E-08   0.15056E-08 0.19945E+00 
c  r23          0.39980E-02      19   0.66935E-08   0.12808E-08 0.19769E+00 
c  epsilon      0.10969E+02      11   0.34633E-08   0.10062E-01 0.16550E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.83354E-02 0.43099E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61398       0.0052573       0.0015073
v  Velocity[Y]            -0.57346         0.54406       0.0030792      0.00087258
v  Velocity[Z]              1.5654           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5792           5.441          4.3406          4.3632
v  Pressure                -36.431          360.01           87.64          169.84
v  r11                   0.0010623        0.081866        0.013076        0.018287
v  r22                   0.0011161        0.082607        0.013356        0.018647
v  r33                   0.0016447         0.17441        0.027256        0.037208
v  r12                    -0.01067        0.013602     -0.00023388     -0.00030934
v  r13                    -0.04551        0.052778      9.3353e-05       0.0010139
v  r23                   -0.046724        0.051158      3.0593e-05      0.00057465
v  epsilon                0.069614          271.27          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9896e-05       0.0099178      0.00092534       0.0017429
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017891          5.2772         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85284


 TIME FOR THE TIME STEP            11140:        0.71163E+02

===============================================================


 INSTANT    0.111410000E-01   TIME STEP NUMBER           11141
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.261059148E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.567530651E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.361027986E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.973652792E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.203961874E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81296E-03   0.45077E-02 0.19875E+01 
c  Velocity[X]                                      0.13684E-03 
c  Velocity[Y]                                      0.12832E-03 
c  Velocity[Z]                                      0.42426E-02 
c  Pressure     0.36438E-04     133   0.92736E-02   0.25700E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58579E-08   0.16267E-08 0.98281E-01 
c  r22          0.10853E-01      13   0.52633E-08   0.18027E-08 0.10018E+00 
c  r33          0.21861E-01      15   0.58872E-08   0.12447E-07 0.12585E+00 
c  r12          0.93879E-03      18   0.59213E-08   0.29628E-09 0.60188E+00 
c  r13          0.46678E-02      19   0.62698E-08   0.14816E-08 0.19867E+00 
c  r23          0.39980E-02      19   0.64640E-08   0.12844E-08 0.19783E+00 
c  epsilon      0.10969E+02      11   0.34822E-08   0.98142E-02 0.16443E+00 
c  TempC        0.25716E+06      16   0.15165E-04   0.83638E-02 0.43150E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61399       0.0052573       0.0015073
v  Velocity[Y]            -0.57351         0.54423       0.0030791      0.00087257
v  Velocity[Z]              1.5655           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5793           5.441          4.3406          4.3632
v  Pressure                -36.414          360.01          87.635          169.84
v  r11                   0.0010623        0.081853        0.013076        0.018287
v  r22                   0.0011162        0.082605        0.013356        0.018647
v  r33                   0.0016447         0.17442        0.027256        0.037208
v  r12                    -0.01067        0.013602     -0.00023388     -0.00030934
v  r13                    -0.04551        0.052776      9.3354e-05       0.0010139
v  r23                   -0.046724        0.051179      3.0593e-05      0.00057465
v  epsilon                0.069615          271.28          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9899e-05       0.0099178      0.00092535       0.0017429
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017891          5.2776         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11141:        0.72505E+02

===============================================================


 INSTANT    0.111420000E-01   TIME STEP NUMBER           11142
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.244387704E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.502041691E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.600215050E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.300065344E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.884241038E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81255E-03   0.45151E-02 0.19894E+01 
c  Velocity[X]                                      0.13764E-03 
c  Velocity[Y]                                      0.12897E-03 
c  Velocity[Z]                                      0.42485E-02 
c  Pressure     0.36068E-04     133   0.91767E-02   0.25439E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60809E-08   0.16260E-08 0.98403E-01 
c  r22          0.10853E-01      13   0.54537E-08   0.18330E-08 0.10062E+00 
c  r33          0.21861E-01      15   0.55211E-08   0.12520E-07 0.12599E+00 
c  r12          0.93879E-03      18   0.61188E-08   0.29915E-09 0.60461E+00 
c  r13          0.46678E-02      19   0.66797E-08   0.15156E-08 0.20025E+00 
c  r23          0.39980E-02      19   0.70421E-08   0.12583E-08 0.19583E+00 
c  epsilon      0.10969E+02      11   0.35048E-08   0.10008E-01 0.16614E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.84904E-02 0.43438E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61396       0.0052573       0.0015073
v  Velocity[Y]            -0.57346         0.54394       0.0030791      0.00087256
v  Velocity[Z]              1.5655           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5793           5.441          4.3406          4.3632
v  Pressure                -36.463          360.03           87.66          169.86
v  r11                   0.0010623        0.081845        0.013076        0.018287
v  r22                   0.0011162        0.082604        0.013356        0.018647
v  r33                   0.0016447         0.17442        0.027256        0.037208
v  r12                   -0.010673          0.0136     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052776      9.3355e-05       0.0010139
v  r23                   -0.046723        0.051162      3.0594e-05      0.00057465
v  epsilon                0.069616           271.3          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9902e-05       0.0099177      0.00092535       0.0017429
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017891          5.2777         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            11142:        0.69735E+02

===============================================================


 INSTANT    0.111430000E-01   TIME STEP NUMBER           11143
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.142318687E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100070777E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182364148E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.476419681E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.299842547E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81289E-03   0.44488E-02 0.19750E+01 
c  Velocity[X]                                      0.13665E-03 
c  Velocity[Y]                                      0.12618E-03 
c  Velocity[Z]                                      0.41860E-02 
c  Pressure     0.36233E-04     132   0.92281E-02   0.25555E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58373E-08   0.16450E-08 0.98599E-01 
c  r22          0.10853E-01      13   0.50282E-08   0.18456E-08 0.10094E+00 
c  r33          0.21861E-01      15   0.72865E-08   0.12649E-07 0.12653E+00 
c  r12          0.93879E-03      18   0.56277E-08   0.30541E-09 0.60745E+00 
c  r13          0.46678E-02      20   0.58399E-08   0.15186E-08 0.19964E+00 
c  r23          0.39980E-02      19   0.59947E-08   0.13026E-08 0.19888E+00 
c  epsilon      0.10969E+02      11   0.36811E-08   0.98971E-02 0.16514E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.83673E-02 0.43150E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61399       0.0052574       0.0015074
v  Velocity[Y]            -0.57359         0.54401       0.0030792       0.0008726
v  Velocity[Z]              1.5656           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5794           5.441          4.3406          4.3632
v  Pressure                -36.384          359.97          87.602           169.8
v  r11                   0.0010623         0.08184        0.013076        0.018287
v  r22                   0.0011162        0.082602        0.013356        0.018647
v  r33                   0.0016447         0.17443        0.027256        0.037208
v  r12                    -0.01067         0.01359     -0.00023388     -0.00030934
v  r13                    -0.04551        0.052779      9.3356e-05       0.0010139
v  r23                   -0.046723        0.051147      3.0594e-05      0.00057465
v  epsilon                0.069617          271.29          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9906e-05       0.0099177      0.00092535       0.0017429
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017891          5.2778         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85284


 TIME FOR THE TIME STEP            11143:        0.71188E+02

===============================================================


 INSTANT    0.111440000E-01   TIME STEP NUMBER           11144
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.236337210E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.125790488E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934904E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.281103150E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.330279644E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934913E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.177081938E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21886E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40357E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81286E-03   0.45010E-02 0.19873E+01 
c  Velocity[X]                                      0.13718E-03 
c  Velocity[Y]                                      0.12745E-03 
c  Velocity[Z]                                      0.42364E-02 
c  Pressure     0.36748E-04     131   0.93469E-02   0.25918E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56668E-08   0.16359E-08 0.98713E-01 
c  r22          0.10853E-01      13   0.53310E-08   0.18540E-08 0.10131E+00 
c  r33          0.21861E-01      15   0.64959E-08   0.12631E-07 0.12705E+00 
c  r12          0.93879E-03      18   0.65466E-08   0.30210E-09 0.60660E+00 
c  r13          0.46678E-02      19   0.56941E-08   0.15055E-08 0.19968E+00 
c  r23          0.39980E-02      19   0.59888E-08   0.12958E-08 0.19966E+00 
c  epsilon      0.10969E+02      11   0.35553E-08   0.10180E-01 0.17092E+00 
c  TempC        0.25716E+06      16   0.15213E-04   0.84003E-02 0.43235E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63354         0.61399       0.0052573       0.0015073
v  Velocity[Y]            -0.57355         0.54413       0.0030791      0.00087254
v  Velocity[Z]              1.5658           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5796           5.441          4.3406          4.3632
v  Pressure                -36.445          360.03          87.666          169.87
v  r11                   0.0010623        0.081835        0.013076        0.018287
v  r22                   0.0011162          0.0826        0.013356        0.018647
v  r33                   0.0016447         0.17444        0.027256        0.037208
v  r12                    -0.01067        0.013584     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052779      9.3355e-05       0.0010139
v  r23                   -0.046723         0.05116      3.0594e-05      0.00057465
v  epsilon                0.069618          271.27          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9908e-05       0.0099177      0.00092535       0.0017429
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017891          5.2778         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71353         0.85284


 TIME FOR THE TIME STEP            11144:        0.68265E+02

===============================================================


 INSTANT    0.111450000E-01   TIME STEP NUMBER           11145
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.624850453E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.569010680E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117456803E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227453509E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.262290457E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81240E-03   0.45324E-02 0.19935E+01 
c  Velocity[X]                                      0.13899E-03 
c  Velocity[Y]                                      0.12886E-03 
c  Velocity[Z]                                      0.42645E-02 
c  Pressure     0.35883E-04     133   0.91341E-02   0.25310E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57126E-08   0.16551E-08 0.98834E-01 
c  r22          0.10853E-01      13   0.55991E-08   0.18309E-08 0.10039E+00 
c  r33          0.21861E-01      15   0.62080E-08   0.12562E-07 0.12599E+00 
c  r12          0.93879E-03      18   0.64107E-08   0.29216E-09 0.59731E+00 
c  r13          0.46678E-02      19   0.52837E-08   0.14876E-08 0.19814E+00 
c  r23          0.39980E-02      19   0.73609E-08   0.12875E-08 0.19785E+00 
c  epsilon      0.10969E+02      11   0.34749E-08   0.10067E-01 0.16490E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.84038E-02 0.43292E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63338         0.61397       0.0052573       0.0015073
v  Velocity[Y]            -0.57355          0.5438       0.0030792      0.00087258
v  Velocity[Z]              1.5657           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5795           5.441          4.3406          4.3632
v  Pressure                -36.427          360.01          87.635          169.84
v  r11                   0.0010623        0.081831        0.013076        0.018287
v  r22                   0.0011162        0.082596        0.013356        0.018647
v  r33                   0.0016447         0.17445        0.027256        0.037208
v  r12                   -0.010668        0.013579     -0.00023388     -0.00030934
v  r13                    -0.04551        0.052782      9.3356e-05       0.0010139
v  r23                   -0.046722        0.051149      3.0594e-05      0.00057465
v  epsilon                0.069619          271.28          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9912e-05       0.0099176      0.00092535       0.0017429
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017891          5.2784         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85284


 TIME FOR THE TIME STEP            11145:        0.71801E+02

===============================================================


 INSTANT    0.111460000E-01   TIME STEP NUMBER           11146
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276981264E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.175639510E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.187130102E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.888227019E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.268398213E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81434E-03   0.45020E-02 0.19871E+01 
c  Velocity[X]                                      0.13668E-03 
c  Velocity[Y]                                      0.12807E-03 
c  Velocity[Z]                                      0.42372E-02 
c  Pressure     0.36413E-04     136   0.92656E-02   0.25682E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55537E-08   0.16401E-08 0.98340E-01 
c  r22          0.10853E-01      13   0.52385E-08   0.18305E-08 0.10051E+00 
c  r33          0.21861E-01      15   0.55514E-08   0.12482E-07 0.12562E+00 
c  r12          0.93879E-03      18   0.57585E-08   0.30273E-09 0.60077E+00 
c  r13          0.46678E-02      19   0.62388E-08   0.14937E-08 0.19863E+00 
c  r23          0.39980E-02      19   0.65545E-08   0.12943E-08 0.19806E+00 
c  epsilon      0.10969E+02      11   0.34349E-08   0.99481E-02 0.16451E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.83332E-02 0.43069E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63337         0.61396       0.0052573       0.0015074
v  Velocity[Y]            -0.57347         0.54331       0.0030791      0.00087255
v  Velocity[Z]              1.5656           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5794           5.441          4.3406          4.3632
v  Pressure                -36.444          360.06          87.677          169.88
v  r11                   0.0010623        0.081843        0.013076        0.018287
v  r22                   0.0011162        0.082598        0.013356        0.018647
v  r33                   0.0016447          0.1744        0.027256        0.037208
v  r12                   -0.010669        0.013579     -0.00023388     -0.00030934
v  r13                   -0.045511        0.052782      9.3357e-05       0.0010139
v  r23                   -0.046722        0.051142      3.0594e-05      0.00057465
v  epsilon                0.069621          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099176      0.00092535       0.0017429
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017892          5.2786         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            11146:        0.68233E+02

===============================================================


 INSTANT    0.111470000E-01   TIME STEP NUMBER           11147
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.423047892E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.286960628E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130036497E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.103590769E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.315210611E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40356E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81220E-03   0.45150E-02 0.19904E+01 
c  Velocity[X]                                      0.13730E-03 
c  Velocity[Y]                                      0.12770E-03 
c  Velocity[Z]                                      0.42500E-02 
c  Pressure     0.36464E-04     133   0.92802E-02   0.25719E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55484E-08   0.16440E-08 0.98785E-01 
c  r22          0.10853E-01      13   0.50485E-08   0.18261E-08 0.10062E+00 
c  r33          0.21861E-01      15   0.55991E-08   0.12498E-07 0.12602E+00 
c  r12          0.93879E-03      18   0.56771E-08   0.29926E-09 0.60169E+00 
c  r13          0.46678E-02      19   0.58638E-08   0.14881E-08 0.19865E+00 
c  r23          0.39980E-02      19   0.67942E-08   0.12829E-08 0.19774E+00 
c  epsilon      0.10969E+02      11   0.35585E-08   0.98932E-02 0.16512E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.84237E-02 0.43259E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61398       0.0052573       0.0015073
v  Velocity[Y]            -0.57359         0.54328       0.0030792      0.00087261
v  Velocity[Z]              1.5657           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5795           5.441          4.3406          4.3632
v  Pressure                 -36.38          360.05          87.669          169.88
v  r11                   0.0010623        0.081844        0.013076        0.018287
v  r22                   0.0011162          0.0826        0.013356        0.018647
v  r33                   0.0016447         0.17435        0.027256        0.037208
v  r12                   -0.010673        0.013576     -0.00023388     -0.00030934
v  r13                   -0.045509        0.052779      9.3357e-05       0.0010139
v  r23                   -0.046722        0.051139      3.0594e-05      0.00057465
v  epsilon                0.069622          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9924e-05       0.0099175      0.00092535       0.0017429
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017892          5.2795         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8795         0.71352         0.85283


 TIME FOR THE TIME STEP            11147:        0.70181E+02

===============================================================


 INSTANT    0.111480000E-01   TIME STEP NUMBER           11148
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106360756E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.242604175E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.904709252E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166781729E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183224054E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81336E-03   0.44803E-02 0.19823E+01 
c  Velocity[X]                                      0.13781E-03 
c  Velocity[Y]                                      0.12775E-03 
c  Velocity[Z]                                      0.42148E-02 
c  Pressure     0.36021E-04     133   0.91733E-02   0.25406E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56832E-08   0.16263E-08 0.98295E-01 
c  r22          0.10853E-01      13   0.51759E-08   0.18416E-08 0.10055E+00 
c  r33          0.21861E-01      15   0.54933E-08   0.12563E-07 0.12591E+00 
c  r12          0.93879E-03      18   0.60784E-08   0.30334E-09 0.60253E+00 
c  r13          0.46678E-02      19   0.65101E-08   0.15290E-08 0.19981E+00 
c  r23          0.39980E-02      19   0.57066E-08   0.12905E-08 0.19744E+00 
c  epsilon      0.10969E+02      11   0.34511E-08   0.10045E-01 0.16586E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.84466E-02 0.43396E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61394       0.0052573       0.0015073
v  Velocity[Y]            -0.57351         0.54295       0.0030792      0.00087259
v  Velocity[Z]              1.5657           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5795           5.441          4.3406          4.3632
v  Pressure                -36.474          360.03          87.665          169.86
v  r11                   0.0010623         0.08184        0.013076        0.018287
v  r22                   0.0011162        0.082601        0.013356        0.018647
v  r33                   0.0016447         0.17434        0.027256        0.037208
v  r12                   -0.010672        0.013572     -0.00023388     -0.00030934
v  r13                   -0.045507        0.052779      9.3357e-05       0.0010139
v  r23                   -0.046722        0.051161      3.0594e-05      0.00057465
v  epsilon                0.069623           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099175      0.00092535       0.0017429
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017892          5.2794         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8794         0.71352         0.85284


 TIME FOR THE TIME STEP            11148:        0.69374E+02

===============================================================


 INSTANT    0.111490000E-01   TIME STEP NUMBER           11149
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123044789E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.114271917E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935006E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.176878997E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.340612037E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.565014845E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81317E-03   0.45109E-02 0.19868E+01 
c  Velocity[X]                                      0.13741E-03 
c  Velocity[Y]                                      0.12696E-03 
c  Velocity[Z]                                      0.42465E-02 
c  Pressure     0.36279E-04     132   0.92405E-02   0.25588E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55618E-08   0.16242E-08 0.98158E-01 
c  r22          0.10853E-01      13   0.49468E-08   0.17899E-08 0.99519E-01 
c  r33          0.21861E-01      14   0.68315E-08   0.12298E-07 0.12498E+00 
c  r12          0.93879E-03      18   0.53305E-08   0.29862E-09 0.59991E+00 
c  r13          0.46678E-02      19   0.59391E-08   0.14744E-08 0.19702E+00 
c  r23          0.39980E-02      19   0.50567E-08   0.12764E-08 0.19709E+00 
c  epsilon      0.10969E+02      11   0.33408E-08   0.95958E-02 0.16261E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.84053E-02 0.43246E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61395       0.0052574       0.0015074
v  Velocity[Y]            -0.57359         0.54302       0.0030791      0.00087256
v  Velocity[Z]              1.5659           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5797           5.441          4.3406          4.3632
v  Pressure                -36.416          359.98            87.6          169.81
v  r11                   0.0010623        0.081832        0.013076        0.018287
v  r22                   0.0011162        0.082601        0.013356        0.018647
v  r33                   0.0016447         0.17435        0.027256        0.037208
v  r12                   -0.010671        0.013579     -0.00023388     -0.00030934
v  r13                   -0.045512         0.05278      9.3358e-05       0.0010139
v  r23                   -0.046722        0.051164      3.0594e-05      0.00057465
v  epsilon                0.069624           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05       0.0099175      0.00092535       0.0017429
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017892          5.2791         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71352         0.85284


 TIME FOR THE TIME STEP            11149:        0.71823E+02

===============================================================


 INSTANT    0.111500000E-01   TIME STEP NUMBER           11150
 ============================================================= 



 Options set or changed by "control_file":
 -----------------------------------------

  max_time_step                           11300 (current: 11150)

 Finished reading "control_file".



   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319184654E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.181978869E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934903E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.535072496E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.162123561E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.285262052E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81297E-03   0.44973E-02 0.19854E+01 
c  Velocity[X]                                      0.13673E-03 
c  Velocity[Y]                                      0.12784E-03 
c  Velocity[Z]                                      0.42327E-02 
c  Pressure     0.36008E-04     132   0.91638E-02   0.25396E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54566E-08   0.16254E-08 0.98571E-01 
c  r22          0.10853E-01      13   0.50587E-08   0.17924E-08 0.99951E-01 
c  r33          0.21861E-01      14   0.69789E-08   0.12348E-07 0.12580E+00 
c  r12          0.93879E-03      18   0.53447E-08   0.30001E-09 0.60338E+00 
c  r13          0.46678E-02      19   0.58112E-08   0.14674E-08 0.19789E+00 
c  r23          0.39980E-02      19   0.57945E-08   0.12818E-08 0.19863E+00 
c  epsilon      0.10969E+02      11   0.31597E-08   0.99848E-02 0.17080E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.83412E-02 0.43032E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63358          0.6139       0.0052573       0.0015073
v  Velocity[Y]            -0.57349         0.54279       0.0030791      0.00087252
v  Velocity[Z]              1.5657           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5795           5.441          4.3406          4.3632
v  Pressure                 -36.44          359.96          87.633          169.81
v  r11                   0.0010623        0.081829        0.013076        0.018287
v  r22                   0.0011162        0.082601        0.013356        0.018647
v  r33                   0.0016447         0.17437        0.027256        0.037208
v  r12                   -0.010674         0.01358     -0.00023388     -0.00030934
v  r13                   -0.045509        0.052782      9.3359e-05       0.0010139
v  r23                   -0.046721        0.051155      3.0595e-05      0.00057465
v  epsilon                0.069625          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099173      0.00092535       0.0017429
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017892          5.2787         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85284


 TIME FOR THE TIME STEP            11150:        0.71769E+02

===============================================================


 INSTANT    0.111510000E-01   TIME STEP NUMBER           11151
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.147001095E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.299807359E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106798919E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.300728992E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282578446E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81311E-03   0.44963E-02 0.19867E+01 
c  Velocity[X]                                      0.13805E-03 
c  Velocity[Y]                                      0.12796E-03 
c  Velocity[Z]                                      0.42303E-02 
c  Pressure     0.36328E-04     133   0.92486E-02   0.25623E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54857E-08   0.16207E-08 0.97943E-01 
c  r22          0.10853E-01      13   0.52898E-08   0.18117E-08 0.99822E-01 
c  r33          0.21861E-01      15   0.69685E-08   0.12412E-07 0.12517E+00 
c  r12          0.93879E-03      18   0.51311E-08   0.29159E-09 0.59638E+00 
c  r13          0.46678E-02      18   0.70905E-08   0.14799E-08 0.19739E+00 
c  r23          0.39980E-02      19   0.56577E-08   0.12598E-08 0.19608E+00 
c  epsilon      0.10969E+02      11   0.32126E-08   0.99754E-02 0.16554E+00 
c  TempC        0.25716E+06      16   0.15142E-04   0.84084E-02 0.43276E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61393       0.0052573       0.0015073
v  Velocity[Y]            -0.57343         0.54295       0.0030792      0.00087258
v  Velocity[Z]              1.5657           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5795           5.441          4.3406          4.3632
v  Pressure                -36.441          360.05          87.662          169.88
v  r11                   0.0010623        0.081828        0.013076        0.018287
v  r22                   0.0011162        0.082603        0.013356        0.018647
v  r33                   0.0016447         0.17439        0.027256        0.037208
v  r12                   -0.010673        0.013577     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052782       9.336e-05       0.0010139
v  r23                   -0.046721        0.051186      3.0595e-05      0.00057465
v  epsilon                0.069627          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9941e-05       0.0099174      0.00092535       0.0017429
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017892          5.2789         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            11151:        0.71108E+02

===============================================================


 INSTANT    0.111520000E-01   TIME STEP NUMBER           11152
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.400675371E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.268777118E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.232929662E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.757363329E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.207707379E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21885E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81359E-03   0.45003E-02 0.19855E+01 
c  Velocity[X]                                      0.13668E-03 
c  Velocity[Y]                                      0.12700E-03 
c  Velocity[Z]                                      0.42366E-02 
c  Pressure     0.36204E-04     133   0.92121E-02   0.25535E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52512E-08   0.16331E-08 0.98388E-01 
c  r22          0.10853E-01      13   0.54015E-08   0.18490E-08 0.10093E+00 
c  r33          0.21861E-01      15   0.68807E-08   0.12611E-07 0.12613E+00 
c  r12          0.93879E-03      17   0.68849E-08   0.30625E-09 0.60733E+00 
c  r13          0.46678E-02      18   0.70046E-08   0.15452E-08 0.20084E+00 
c  r23          0.39980E-02      19   0.67861E-08   0.12959E-08 0.19844E+00 
c  epsilon      0.10969E+02      11   0.34424E-08   0.10095E-01 0.16642E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.83467E-02 0.43138E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343           0.614       0.0052573       0.0015073
v  Velocity[Y]            -0.57343         0.54271       0.0030791      0.00087254
v  Velocity[Z]              1.5657           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5795           5.441          4.3406          4.3632
v  Pressure                -36.444          360.04          87.664          169.88
v  r11                   0.0010623        0.081843        0.013076        0.018287
v  r22                   0.0011162        0.082604        0.013356        0.018647
v  r33                   0.0016448          0.1744        0.027256        0.037208
v  r12                   -0.010673        0.013574     -0.00023388     -0.00030934
v  r13                    -0.04551        0.052782       9.336e-05       0.0010139
v  r23                   -0.046721        0.051169      3.0595e-05      0.00057465
v  epsilon                0.069628          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099174      0.00092535       0.0017429
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017892          5.2787         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71353         0.85285


 TIME FOR THE TIME STEP            11152:        0.69789E+02

===============================================================


 INSTANT    0.111530000E-01   TIME STEP NUMBER           11153
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.726628668E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.143757127E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.297467443E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.529496211E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.869970356E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81227E-03   0.45356E-02 0.19926E+01 
c  Velocity[X]                                      0.13759E-03 
c  Velocity[Y]                                      0.12846E-03 
c  Velocity[Z]                                      0.42696E-02 
c  Pressure     0.36402E-04     132   0.92657E-02   0.25675E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55521E-08   0.16397E-08 0.98550E-01 
c  r22          0.10853E-01      13   0.55076E-08   0.18381E-08 0.10079E+00 
c  r33          0.21861E-01      16   0.58851E-08   0.12545E-07 0.12614E+00 
c  r12          0.93879E-03      17   0.68094E-08   0.30770E-09 0.61232E+00 
c  r13          0.46679E-02      19   0.57603E-08   0.15032E-08 0.19910E+00 
c  r23          0.39980E-02      19   0.73513E-08   0.12910E-08 0.19866E+00 
c  epsilon      0.10969E+02      11   0.36293E-08   0.10047E-01 0.16676E+00 
c  TempC        0.25716E+06      16   0.15138E-04   0.84006E-02 0.43233E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61395       0.0052573       0.0015073
v  Velocity[Y]            -0.57356         0.54289       0.0030792      0.00087258
v  Velocity[Z]              1.5659           5.441          4.3387          4.3625
v  ǁVelocityǁ               1.5797           5.441          4.3406          4.3632
v  Pressure                -36.409          359.99          87.634          169.83
v  r11                   0.0010623        0.081843        0.013076        0.018287
v  r22                   0.0011162        0.082604        0.013356        0.018647
v  r33                   0.0016448          0.1744        0.027256        0.037208
v  r12                   -0.010672        0.013575     -0.00023388     -0.00030934
v  r13                   -0.045509        0.052781      9.3361e-05       0.0010139
v  r23                   -0.046722        0.051147      3.0595e-05      0.00057465
v  epsilon                0.069629          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9945e-05       0.0099174      0.00092535       0.0017429
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017893          5.2791         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8791         0.71352         0.85284


 TIME FOR THE TIME STEP            11153:        0.70235E+02

===============================================================


 INSTANT    0.111540000E-01   TIME STEP NUMBER           11154
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181205598E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.159492794E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.197136684E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178272210E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.326043991E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81294E-03   0.45164E-02 0.19905E+01 
c  Velocity[X]                                      0.13715E-03 
c  Velocity[Y]                                      0.12802E-03 
c  Velocity[Z]                                      0.42512E-02 
c  Pressure     0.36355E-04     132   0.92554E-02   0.25643E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53715E-08   0.16496E-08 0.99031E-01 
c  r22          0.10853E-01      13   0.55155E-08   0.18202E-08 0.10038E+00 
c  r33          0.21861E-01      15   0.68973E-08   0.12568E-07 0.12626E+00 
c  r12          0.93879E-03      17   0.66378E-08   0.30029E-09 0.60431E+00 
c  r13          0.46679E-02      19   0.60161E-08   0.15017E-08 0.19924E+00 
c  r23          0.39980E-02      19   0.68440E-08   0.12974E-08 0.19903E+00 
c  epsilon      0.10969E+02      11   0.35105E-08   0.99824E-02 0.16604E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.84824E-02 0.43385E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63356         0.61392       0.0052573       0.0015074
v  Velocity[Y]            -0.57351         0.54326       0.0030791      0.00087258
v  Velocity[Z]              1.5658          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4411          4.3406          4.3632
v  Pressure                -36.486             360          87.651          169.84
v  r11                   0.0010623        0.081845        0.013076        0.018287
v  r22                   0.0011162        0.082603        0.013356        0.018647
v  r33                   0.0016448         0.17436        0.027256        0.037208
v  r12                   -0.010671        0.013575     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052781      9.3362e-05       0.0010139
v  r23                   -0.046722        0.051167      3.0595e-05      0.00057465
v  epsilon                 0.06963           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099174      0.00092535       0.0017429
v  CourantNb                0.4426             0.6         0.59908         0.59839
v  FourierNb             0.0017893          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            11154:        0.70032E+02

===============================================================


 INSTANT    0.111550000E-01   TIME STEP NUMBER           11155
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.246879305E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.181746658E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.364492750E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.551122829E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.291876983E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81344E-03   0.44577E-02 0.19778E+01 
c  Velocity[X]                                      0.13672E-03 
c  Velocity[Y]                                      0.12725E-03 
c  Velocity[Z]                                      0.41937E-02 
c  Pressure     0.36112E-04     132   0.91992E-02   0.25470E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.50296E-08   0.16136E-08 0.98263E-01 
c  r22          0.10853E-01      13   0.57878E-08   0.18050E-08 0.10002E+00 
c  r33          0.21861E-01      15   0.65522E-08   0.12363E-07 0.12558E+00 
c  r12          0.93879E-03      18   0.50139E-08   0.29483E-09 0.59961E+00 
c  r13          0.46679E-02      19   0.62840E-08   0.14903E-08 0.19845E+00 
c  r23          0.39980E-02      19   0.66138E-08   0.12735E-08 0.19707E+00 
c  epsilon      0.10969E+02      11   0.33124E-08   0.97343E-02 0.16361E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.83743E-02 0.43162E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61381       0.0052573       0.0015074
v  Velocity[Y]            -0.57361         0.54357       0.0030792      0.00087259
v  Velocity[Z]              1.5658          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4411          4.3406          4.3632
v  Pressure                -36.438          359.98          87.602          169.81
v  r11                   0.0010624        0.081839        0.013076        0.018287
v  r22                   0.0011162        0.082599        0.013356        0.018647
v  r33                   0.0016448         0.17435        0.027256        0.037208
v  r12                   -0.010671        0.013572     -0.00023388     -0.00030934
v  r13                    -0.04551        0.052782      9.3363e-05       0.0010139
v  r23                   -0.046723         0.05116      3.0595e-05      0.00057465
v  epsilon                0.069631          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.995e-05       0.0099174      0.00092535       0.0017429
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017893          5.2786         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71353         0.85284


 TIME FOR THE TIME STEP            11155:        0.70179E+02

===============================================================


 INSTANT    0.111560000E-01   TIME STEP NUMBER           11156
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.197719508E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.251048943E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.290061743E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.734879243E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.924780223E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81305E-03   0.45124E-02 0.19888E+01 
c  Velocity[X]                                      0.13706E-03 
c  Velocity[Y]                                      0.12812E-03 
c  Velocity[Z]                                      0.42472E-02 
c  Pressure     0.36450E-04     133   0.92747E-02   0.25709E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55550E-08   0.16446E-08 0.99104E-01 
c  r22          0.10853E-01      13   0.54264E-08   0.18205E-08 0.10019E+00 
c  r33          0.21861E-01      15   0.61443E-08   0.12550E-07 0.12637E+00 
c  r12          0.93879E-03      18   0.55505E-08   0.30118E-09 0.60598E+00 
c  r13          0.46679E-02      19   0.67441E-08   0.14878E-08 0.19823E+00 
c  r23          0.39980E-02      19   0.64660E-08   0.12993E-08 0.20017E+00 
c  epsilon      0.10969E+02      11   0.32390E-08   0.10336E-01 0.17310E+00 
c  TempC        0.25716E+06      16   0.15176E-04   0.83682E-02 0.43203E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61375       0.0052574       0.0015074
v  Velocity[Y]            -0.57345         0.54381       0.0030791      0.00087259
v  Velocity[Z]              1.5658          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4411          4.3406          4.3632
v  Pressure                -36.485          359.95          87.622           169.8
v  r11                   0.0010624        0.081836        0.013076        0.018287
v  r22                   0.0011162        0.082599        0.013356        0.018647
v  r33                   0.0016448         0.17432        0.027256        0.037208
v  r12                   -0.010679        0.013568     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052779      9.3363e-05       0.0010139
v  r23                   -0.046724        0.051146      3.0596e-05      0.00057465
v  epsilon                0.069633          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9952e-05       0.0099174      0.00092535       0.0017429
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017893          5.2787         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85284


 TIME FOR THE TIME STEP            11156:        0.69650E+02

===============================================================


 INSTANT    0.111570000E-01   TIME STEP NUMBER           11157
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.509689410E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.957609474E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106086799E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116930486E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.495970611E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81260E-03   0.45198E-02 0.19910E+01 
c  Velocity[X]                                      0.13778E-03 
c  Velocity[Y]                                      0.12784E-03 
c  Velocity[Z]                                      0.42542E-02 
c  Pressure     0.36290E-04     133   0.92349E-02   0.25597E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56612E-08   0.16406E-08 0.98575E-01 
c  r22          0.10853E-01      13   0.56990E-08   0.18370E-08 0.10005E+00 
c  r33          0.21861E-01      15   0.54387E-08   0.12584E-07 0.12572E+00 
c  r12          0.93879E-03      18   0.66820E-08   0.29990E-09 0.60538E+00 
c  r13          0.46679E-02      19   0.56728E-08   0.15182E-08 0.19856E+00 
c  r23          0.39980E-02      19   0.57885E-08   0.12789E-08 0.19721E+00 
c  epsilon      0.10969E+02      11   0.34939E-08   0.10244E-01 0.16765E+00 
c  TempC        0.25716E+06      16   0.15131E-04   0.83928E-02 0.43226E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61381       0.0052574       0.0015074
v  Velocity[Y]            -0.57347         0.54405       0.0030791      0.00087261
v  Velocity[Z]              1.5658          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4411          4.3406          4.3632
v  Pressure                -36.445          360.08          87.681           169.9
v  r11                   0.0010624        0.081833        0.013076        0.018287
v  r22                   0.0011162        0.082601        0.013356        0.018647
v  r33                   0.0016448         0.17433        0.027256        0.037208
v  r12                   -0.010681        0.013572     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052778      9.3364e-05       0.0010139
v  r23                   -0.046725        0.051133      3.0596e-05      0.00057465
v  epsilon                0.069634          271.18          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9955e-05       0.0099173      0.00092535       0.0017429
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017893          5.2783         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71353         0.85284


 TIME FOR THE TIME STEP            11157:        0.69510E+02

===============================================================


 INSTANT    0.111580000E-01   TIME STEP NUMBER           11158
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.192567467E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.103016897E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.361244238E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935012E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.319284210E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.148838003E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40355E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81302E-03   0.45012E-02 0.19863E+01 
c  Velocity[X]                                      0.13650E-03 
c  Velocity[Y]                                      0.12733E-03 
c  Velocity[Z]                                      0.42374E-02 
c  Pressure     0.36487E-04     131   0.92892E-02   0.25735E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54286E-08   0.16331E-08 0.98366E-01 
c  r22          0.10853E-01      13   0.55047E-08   0.17923E-08 0.99724E-01 
c  r33          0.21861E-01      15   0.56177E-08   0.12353E-07 0.12525E+00 
c  r12          0.93879E-03      18   0.58070E-08   0.29948E-09 0.60615E+00 
c  r13          0.46679E-02      18   0.72310E-08   0.14693E-08 0.19754E+00 
c  r23          0.39980E-02      19   0.72893E-08   0.12777E-08 0.19715E+00 
c  epsilon      0.10969E+02      11   0.36014E-08   0.97920E-02 0.16436E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.83710E-02 0.43147E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63359         0.61378       0.0052573       0.0015074
v  Velocity[Y]            -0.57337         0.54392       0.0030791      0.00087258
v  Velocity[Z]              1.5657          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4411          4.3406          4.3632
v  Pressure                -36.441          359.99          87.628          169.83
v  r11                   0.0010624        0.081832        0.013076        0.018287
v  r22                   0.0011162        0.082601        0.013356        0.018647
v  r33                   0.0016448         0.17436        0.027256        0.037208
v  r12                   -0.010683        0.013568     -0.00023388     -0.00030934
v  r13                    -0.04551        0.052778      9.3364e-05       0.0010139
v  r23                   -0.046725        0.051161      3.0596e-05      0.00057465
v  epsilon                0.069635           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099172      0.00092535       0.0017429
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017893           5.279         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71352         0.85284


 TIME FOR THE TIME STEP            11158:        0.69768E+02

===============================================================


 INSTANT    0.111590000E-01   TIME STEP NUMBER           11159
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267126661E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.974994500E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.387839646E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.164483749E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.104649645E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81208E-03   0.44965E-02 0.19896E+01 
c  Velocity[X]                                      0.13705E-03 
c  Velocity[Y]                                      0.12792E-03 
c  Velocity[Z]                                      0.42316E-02 
c  Pressure     0.36432E-04     132   0.92695E-02   0.25697E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.50221E-08   0.16416E-08 0.98864E-01 
c  r22          0.10853E-01      13   0.50430E-08   0.18191E-08 0.99864E-01 
c  r33          0.21861E-01      15   0.54049E-08   0.12548E-07 0.12595E+00 
c  r12          0.93879E-03      18   0.52122E-08   0.30011E-09 0.60404E+00 
c  r13          0.46679E-02      19   0.59924E-08   0.14877E-08 0.19834E+00 
c  r23          0.39980E-02      20   0.56868E-08   0.12968E-08 0.19885E+00 
c  epsilon      0.10969E+02      11   0.35090E-08   0.10176E-01 0.16770E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.84319E-02 0.43267E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63354         0.61371       0.0052573       0.0015074
v  Velocity[Y]            -0.57343         0.54407       0.0030791      0.00087261
v  Velocity[Z]              1.5655          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4411          4.3406          4.3632
v  Pressure                -36.412          360.02          87.635          169.85
v  r11                   0.0010624        0.081845        0.013076        0.018287
v  r22                   0.0011162        0.082601        0.013356        0.018647
v  r33                   0.0016448         0.17438        0.027256        0.037208
v  r12                   -0.010679        0.013572     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052778      9.3365e-05       0.0010139
v  r23                   -0.046725        0.051159      3.0596e-05      0.00057465
v  epsilon                0.069636           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9963e-05       0.0099173      0.00092535       0.0017429
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2795         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8795         0.71352         0.85284


 TIME FOR THE TIME STEP            11159:        0.71077E+02

===============================================================


 INSTANT    0.111600000E-01   TIME STEP NUMBER           11160
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.855491416E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.951525159E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.923199182E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.235332755E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294680251E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81310E-03   0.45028E-02 0.19861E+01 
c  Velocity[X]                                      0.13778E-03 
c  Velocity[Y]                                      0.12842E-03 
c  Velocity[Z]                                      0.42366E-02 
c  Pressure     0.36091E-04     133   0.91854E-02   0.25456E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51530E-08   0.16039E-08 0.98306E-01 
c  r22          0.10853E-01      13   0.52583E-08   0.18101E-08 0.99781E-01 
c  r33          0.21861E-01      15   0.57370E-08   0.12242E-07 0.12513E+00 
c  r12          0.93879E-03      18   0.58539E-08   0.30601E-09 0.60702E+00 
c  r13          0.46679E-02      19   0.59448E-08   0.14953E-08 0.19816E+00 
c  r23          0.39980E-02      20   0.57547E-08   0.12543E-08 0.19691E+00 
c  epsilon      0.10969E+02      11   0.32832E-08   0.95320E-02 0.16269E+00 
c  TempC        0.25716E+06      16   0.15166E-04   0.84154E-02 0.43325E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63359         0.61378       0.0052574       0.0015074
v  Velocity[Y]            -0.57332         0.54424       0.0030791      0.00087258
v  Velocity[Z]              1.5658          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4411          4.3406          4.3632
v  Pressure                 -36.46          360.05          87.676          169.88
v  r11                   0.0010624        0.081856        0.013076        0.018287
v  r22                   0.0011162        0.082601        0.013356        0.018647
v  r33                   0.0016448         0.17439        0.027256        0.037208
v  r12                   -0.010675        0.013569     -0.00023388     -0.00030934
v  r13                   -0.045507        0.052777      9.3366e-05       0.0010139
v  r23                   -0.046725        0.051147      3.0597e-05      0.00057465
v  epsilon                0.069637          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9965e-05       0.0099174      0.00092535       0.0017429
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017893          5.2792         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8792         0.71352         0.85284


 TIME FOR THE TIME STEP            11160:        0.70532E+02

===============================================================


 INSTANT    0.111610000E-01   TIME STEP NUMBER           11161
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.898338953E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.476736476E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168458751E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.232827763E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.222554927E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81303E-03   0.44903E-02 0.19812E+01 
c  Velocity[X]                                      0.13738E-03 
c  Velocity[Y]                                      0.12746E-03 
c  Velocity[Z]                                      0.42255E-02 
c  Pressure     0.36025E-04     132   0.91752E-02   0.25410E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52813E-08   0.16390E-08 0.98946E-01 
c  r22          0.10853E-01      13   0.52699E-08   0.18216E-08 0.10030E+00 
c  r33          0.21861E-01      15   0.61732E-08   0.12501E-07 0.12621E+00 
c  r12          0.93879E-03      18   0.54093E-08   0.30068E-09 0.60562E+00 
c  r13          0.46679E-02      19   0.63502E-08   0.15069E-08 0.19922E+00 
c  r23          0.39980E-02      20   0.60149E-08   0.12872E-08 0.19892E+00 
c  epsilon      0.10969E+02      11   0.32035E-08   0.97751E-02 0.16480E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.83432E-02 0.43116E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6336         0.61378       0.0052574       0.0015074
v  Velocity[Y]            -0.57349         0.54411       0.0030792      0.00087263
v  Velocity[Z]              1.5658          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4411          4.3406          4.3632
v  Pressure                -36.377          360.01          87.634          169.84
v  r11                   0.0010624        0.081862        0.013076        0.018287
v  r22                   0.0011162          0.0826        0.013356        0.018647
v  r33                   0.0016448          0.1744        0.027256        0.037208
v  r12                   -0.010675        0.013567     -0.00023388     -0.00030934
v  r13                    -0.04551        0.052776      9.3366e-05       0.0010139
v  r23                   -0.046724        0.051171      3.0596e-05      0.00057465
v  epsilon                0.069638          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9968e-05       0.0099176      0.00092535       0.0017429
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017894           5.279         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71353         0.85284


 TIME FOR THE TIME STEP            11161:        0.72531E+02

===============================================================


 INSTANT    0.111620000E-01   TIME STEP NUMBER           11162
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.173587354E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.635844165E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.223712361E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.192743113E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.315858312E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81229E-03   0.45240E-02 0.19922E+01 
c  Velocity[X]                                      0.13658E-03 
c  Velocity[Y]                                      0.12816E-03 
c  Velocity[Z]                                      0.42592E-02 
c  Pressure     0.36407E-04     133   0.92669E-02   0.25678E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56404E-08   0.16946E-08 0.10028E+00 
c  r22          0.10853E-01      13   0.56765E-08   0.18604E-08 0.10122E+00 
c  r33          0.21861E-01      15   0.61620E-08   0.12925E-07 0.12780E+00 
c  r12          0.93879E-03      18   0.61308E-08   0.30478E-09 0.60923E+00 
c  r13          0.46679E-02      19   0.64579E-08   0.15253E-08 0.20041E+00 
c  r23          0.39980E-02      20   0.65922E-08   0.13224E-08 0.20164E+00 
c  epsilon      0.10969E+02      11   0.34050E-08   0.10804E-01 0.17542E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.83629E-02 0.43144E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61372       0.0052573       0.0015074
v  Velocity[Y]            -0.57344         0.54405       0.0030792      0.00087263
v  Velocity[Z]              1.5658          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4411          4.3406          4.3632
v  Pressure                -36.427          360.02          87.659          169.85
v  r11                   0.0010624        0.081871        0.013076        0.018287
v  r22                   0.0011162        0.082597        0.013356        0.018647
v  r33                   0.0016448         0.17436        0.027256        0.037208
v  r12                   -0.010675        0.013574     -0.00023388     -0.00030934
v  r13                   -0.045507        0.052775      9.3367e-05       0.0010139
v  r23                   -0.046724        0.051152      3.0596e-05      0.00057465
v  epsilon                 0.06964          271.17          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.997e-05       0.0099176      0.00092536       0.0017429
v  CourantNb               0.44243             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2788         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71352         0.85284


 TIME FOR THE TIME STEP            11162:        0.71368E+02

===============================================================


 INSTANT    0.111630000E-01   TIME STEP NUMBER           11163
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.211196205E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140802438E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.207624071E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.712452981E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186490547E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81303E-03   0.45195E-02 0.19914E+01 
c  Velocity[X]                                      0.13830E-03 
c  Velocity[Y]                                      0.12775E-03 
c  Velocity[Z]                                      0.42535E-02 
c  Pressure     0.36203E-04     132   0.92153E-02   0.25536E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60188E-08   0.16319E-08 0.98982E-01 
c  r22          0.10853E-01      13   0.52447E-08   0.18093E-08 0.10087E+00 
c  r33          0.21861E-01      15   0.52190E-08   0.12320E-07 0.12620E+00 
c  r12          0.93879E-03      18   0.54897E-08   0.29923E-09 0.60706E+00 
c  r13          0.46679E-02      19   0.61049E-08   0.14683E-08 0.19804E+00 
c  r23          0.39980E-02      19   0.72338E-08   0.12660E-08 0.19788E+00 
c  epsilon      0.10969E+02      11   0.33721E-08   0.94887E-02 0.16213E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.84756E-02 0.43438E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61381       0.0052574       0.0015074
v  Velocity[Y]             -0.5735         0.54412       0.0030792      0.00087267
v  Velocity[Z]              1.5658          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4411          4.3406          4.3632
v  Pressure                -36.424          360.01          87.634          169.84
v  r11                   0.0010624        0.081875        0.013076        0.018287
v  r22                   0.0011162        0.082595        0.013356        0.018647
v  r33                   0.0016448         0.17432        0.027256        0.037208
v  r12                   -0.010671        0.013573     -0.00023388     -0.00030934
v  r13                   -0.045506        0.052774      9.3368e-05       0.0010139
v  r23                   -0.046725         0.05114      3.0597e-05      0.00057465
v  epsilon                0.069641          271.16          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9971e-05       0.0099177      0.00092536       0.0017429
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2788         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8788         0.71352         0.85284


 TIME FOR THE TIME STEP            11163:        0.68154E+02

===============================================================


 INSTANT    0.111640000E-01   TIME STEP NUMBER           11164
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.681254027E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.147064244E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934913E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.792143494E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209531347E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.147706411E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81397E-03   0.44678E-02 0.19797E+01 
c  Velocity[X]                                      0.13614E-03 
c  Velocity[Y]                                      0.12724E-03 
c  Velocity[Z]                                      0.42044E-02 
c  Pressure     0.36512E-04     132   0.92945E-02   0.25753E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.63902E-08   0.16573E-08 0.99407E-01 
c  r22          0.10853E-01      13   0.55919E-08   0.18408E-08 0.10085E+00 
c  r33          0.21862E-01      15   0.60083E-08   0.12613E-07 0.12649E+00 
c  r12          0.93879E-03      18   0.61947E-08   0.29971E-09 0.60717E+00 
c  r13          0.46679E-02      19   0.61264E-08   0.14994E-08 0.19905E+00 
c  r23          0.39980E-02      19   0.69605E-08   0.12864E-08 0.19874E+00 
c  epsilon      0.10969E+02      11   0.35026E-08   0.10361E-01 0.16848E+00 
c  TempC        0.25716E+06      16   0.15191E-04   0.83838E-02 0.43204E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63356          0.6138       0.0052572       0.0015074
v  Velocity[Y]            -0.57347         0.54421       0.0030792      0.00087262
v  Velocity[Z]              1.5656          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4411          4.3406          4.3632
v  Pressure                -36.437             360          87.646          169.84
v  r11                   0.0010624        0.081876        0.013076        0.018287
v  r22                   0.0011162        0.082595        0.013356        0.018647
v  r33                   0.0016448         0.17433        0.027256        0.037208
v  r12                   -0.010675        0.013575     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052776      9.3368e-05       0.0010139
v  r23                   -0.046725         0.05117      3.0597e-05      0.00057465
v  epsilon                0.069642          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9971e-05       0.0099177      0.00092536       0.0017429
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017894          5.2784         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85284


 TIME FOR THE TIME STEP            11164:        0.70794E+02

===============================================================


 INSTANT    0.111650000E-01   TIME STEP NUMBER           11165
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.659710804E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.418891227E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.269976953E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.988137067E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.702517592E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81203E-03   0.45177E-02 0.19896E+01 
c  Velocity[X]                                      0.13773E-03 
c  Velocity[Y]                                      0.12784E-03 
c  Velocity[Z]                                      0.42521E-02 
c  Pressure     0.36265E-04     131   0.92326E-02   0.25578E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56662E-08   0.16455E-08 0.99170E-01 
c  r22          0.10853E-01      13   0.52664E-08   0.18255E-08 0.10056E+00 
c  r33          0.21862E-01      14   0.68204E-08   0.12530E-07 0.12634E+00 
c  r12          0.93879E-03      18   0.62572E-08   0.30443E-09 0.60598E+00 
c  r13          0.46679E-02      19   0.57842E-08   0.15165E-08 0.19932E+00 
c  r23          0.39980E-02      20   0.55255E-08   0.12979E-08 0.19843E+00 
c  epsilon      0.10969E+02      11   0.34042E-08   0.10000E-01 0.16663E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.84038E-02 0.43265E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61375       0.0052572       0.0015073
v  Velocity[Y]            -0.57363         0.54401       0.0030791      0.00087258
v  Velocity[Z]              1.5657          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4411          4.3406          4.3632
v  Pressure                -36.378          360.05          87.672          169.88
v  r11                   0.0010624        0.081874        0.013076        0.018287
v  r22                   0.0011162        0.082594        0.013356        0.018647
v  r33                   0.0016448         0.17434        0.027256        0.037208
v  r12                   -0.010674        0.013583     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052775      9.3369e-05       0.0010139
v  r23                   -0.046725        0.051162      3.0598e-05      0.00057466
v  epsilon                0.069643           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.997e-05       0.0099176      0.00092536       0.0017429
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2784         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85283


 TIME FOR THE TIME STEP            11165:        0.70242E+02

===============================================================


 INSTANT    0.111660000E-01   TIME STEP NUMBER           11166
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.172509899E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.210877400E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.392979686E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.350739931E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.115548479E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81434E-03   0.45318E-02 0.19910E+01 
c  Velocity[X]                                      0.13705E-03 
c  Velocity[Y]                                      0.12794E-03 
c  Velocity[Z]                                      0.42668E-02 
c  Pressure     0.36338E-04     132   0.92455E-02   0.25630E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54221E-08   0.16380E-08 0.99849E-01 
c  r22          0.10853E-01      13   0.49481E-08   0.17841E-08 0.10015E+00 
c  r33          0.21862E-01      15   0.50639E-08   0.12294E-07 0.12621E+00 
c  r12          0.93879E-03      18   0.58954E-08   0.29968E-09 0.60805E+00 
c  r13          0.46679E-02      19   0.56473E-08   0.14782E-08 0.19883E+00 
c  r23          0.39980E-02      20   0.54768E-08   0.12854E-08 0.19875E+00 
c  epsilon      0.10969E+02      11   0.33453E-08   0.94450E-02 0.16364E+00 
c  TempC        0.25716E+06      16   0.15164E-04   0.84041E-02 0.43274E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61382       0.0052573       0.0015074
v  Velocity[Y]            -0.57349         0.54411       0.0030791      0.00087258
v  Velocity[Z]              1.5658          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4411          4.3406          4.3632
v  Pressure                 -36.45          360.07          87.681          169.89
v  r11                   0.0010624        0.081869        0.013076        0.018287
v  r22                   0.0011162        0.082594        0.013356        0.018647
v  r33                   0.0016449         0.17436        0.027256        0.037208
v  r12                    -0.01067        0.013583     -0.00023388     -0.00030934
v  r13                   -0.045506        0.052773       9.337e-05       0.0010139
v  r23                   -0.046726        0.051152      3.0599e-05      0.00057466
v  epsilon                0.069644          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9965e-05       0.0099176      0.00092536       0.0017429
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2776         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11166:        0.71837E+02

===============================================================


 INSTANT    0.111670000E-01   TIME STEP NUMBER           11167
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.874793500E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.517128299E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.371689000E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.241003540E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.193073057E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69759E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81147E-03   0.45145E-02 0.19899E+01 
c  Velocity[X]                                      0.13737E-03 
c  Velocity[Y]                                      0.12808E-03 
c  Velocity[Z]                                      0.42490E-02 
c  Pressure     0.36288E-04     133   0.92454E-02   0.25596E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56826E-08   0.16304E-08 0.99198E-01 
c  r22          0.10853E-01      13   0.54268E-08   0.18289E-08 0.10090E+00 
c  r33          0.21862E-01      15   0.60464E-08   0.12537E-07 0.12688E+00 
c  r12          0.93879E-03      18   0.59836E-08   0.30035E-09 0.61042E+00 
c  r13          0.46679E-02      19   0.60834E-08   0.15065E-08 0.20030E+00 
c  r23          0.39980E-02      20   0.61033E-08   0.12757E-08 0.19817E+00 
c  epsilon      0.10969E+02      11   0.31485E-08   0.97460E-02 0.16443E+00 
c  TempC        0.25716E+06      16   0.15121E-04   0.83862E-02 0.43171E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61382       0.0052573       0.0015074
v  Velocity[Y]            -0.57356         0.54426       0.0030791      0.00087259
v  Velocity[Z]              1.5657          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4411          4.3406          4.3632
v  Pressure                -36.402          360.03           87.63          169.85
v  r11                   0.0010624        0.081868        0.013076        0.018287
v  r22                   0.0011162        0.082593        0.013356        0.018647
v  r33                   0.0016449         0.17437        0.027256        0.037208
v  r12                    -0.01067        0.013581     -0.00023388     -0.00030934
v  r13                   -0.045509        0.052772       9.337e-05       0.0010139
v  r23                   -0.046726        0.051178      3.0599e-05      0.00057466
v  epsilon                0.069646           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9964e-05       0.0099175      0.00092536       0.0017429
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2771         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71352         0.85284


 TIME FOR THE TIME STEP            11167:        0.69053E+02

===============================================================


 INSTANT    0.111680000E-01   TIME STEP NUMBER           11168
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.253485360E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.227276638E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934907E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.168979344E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.220277173E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.253647573E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81384E-03   0.44938E-02 0.19855E+01 
c  Velocity[X]                                      0.13735E-03 
c  Velocity[Y]                                      0.12797E-03 
c  Velocity[Z]                                      0.42285E-02 
c  Pressure     0.36332E-04     133   0.92529E-02   0.25626E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54460E-08   0.16707E-08 0.99599E-01 
c  r22          0.10853E-01      13   0.55737E-08   0.18398E-08 0.10076E+00 
c  r33          0.21862E-01      15   0.50451E-08   0.12800E-07 0.12730E+00 
c  r12          0.93879E-03      18   0.58140E-08   0.31040E-09 0.61148E+00 
c  r13          0.46679E-02      18   0.70087E-08   0.15281E-08 0.20085E+00 
c  r23          0.39980E-02      19   0.67010E-08   0.13243E-08 0.20091E+00 
c  epsilon      0.10969E+02      11   0.32482E-08   0.10657E-01 0.17488E+00 
c  TempC        0.25716E+06      16   0.15172E-04   0.83516E-02 0.43109E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63359          0.6138       0.0052573       0.0015074
v  Velocity[Y]            -0.57349         0.54396       0.0030791      0.00087259
v  Velocity[Z]              1.5658          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4411          4.3406          4.3632
v  Pressure                -36.433          360.02          87.665          169.86
v  r11                   0.0010624        0.081868        0.013076        0.018287
v  r22                   0.0011162        0.082592        0.013356        0.018647
v  r33                   0.0016449         0.17439        0.027256        0.037208
v  r12                   -0.010675         0.01358     -0.00023388     -0.00030934
v  r13                   -0.045506        0.052773      9.3371e-05       0.0010139
v  r23                   -0.046727        0.051164      3.0599e-05      0.00057466
v  epsilon                0.069647          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.996e-05       0.0099174      0.00092536       0.0017429
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2771         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71353         0.85284


 TIME FOR THE TIME STEP            11168:        0.69750E+02

===============================================================


 INSTANT    0.111690000E-01   TIME STEP NUMBER           11169
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.196879075E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.285125545E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.321606307E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276346849E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172142287E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81248E-03   0.44985E-02 0.19854E+01 
c  Velocity[X]                                      0.13740E-03 
c  Velocity[Y]                                      0.12767E-03 
c  Velocity[Z]                                      0.42334E-02 
c  Pressure     0.35875E-04     133   0.91284E-02   0.25304E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54184E-08   0.16178E-08 0.98460E-01 
c  r22          0.10853E-01      13   0.56376E-08   0.18214E-08 0.10045E+00 
c  r33          0.21862E-01      15   0.57661E-08   0.12313E-07 0.12550E+00 
c  r12          0.93880E-03      18   0.63568E-08   0.29705E-09 0.60346E+00 
c  r13          0.46679E-02      18   0.70380E-08   0.14868E-08 0.19845E+00 
c  r23          0.39980E-02      19   0.61094E-08   0.12643E-08 0.19657E+00 
c  epsilon      0.10969E+02      11   0.34771E-08   0.96706E-02 0.16251E+00 
c  TempC        0.25716E+06      16   0.15167E-04   0.84220E-02 0.43295E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361         0.61383       0.0052573       0.0015074
v  Velocity[Y]            -0.57352         0.54398       0.0030791      0.00087256
v  Velocity[Z]              1.5661          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5799          5.4411          4.3406          4.3632
v  Pressure                -36.392          359.96          87.613          169.81
v  r11                   0.0010624        0.081864        0.013076        0.018287
v  r22                   0.0011162        0.082592        0.013357        0.018647
v  r33                   0.0016449          0.1744        0.027256        0.037208
v  r12                   -0.010677        0.013585     -0.00023388     -0.00030934
v  r13                   -0.045507        0.052773      9.3371e-05       0.0010139
v  r23                   -0.046726        0.051149      3.0599e-05      0.00057466
v  epsilon                0.069648          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9959e-05       0.0099174      0.00092536       0.0017429
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2774         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            11169:        0.70728E+02

===============================================================


 INSTANT    0.111700000E-01   TIME STEP NUMBER           11170
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.270702007E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221016225E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.277677356E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.855488183E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.258032807E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81343E-03   0.44719E-02 0.19807E+01 
c  Velocity[X]                                      0.13617E-03 
c  Velocity[Y]                                      0.12754E-03 
c  Velocity[Z]                                      0.42082E-02 
c  Pressure     0.36191E-04     132   0.92146E-02   0.25526E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54429E-08   0.16213E-08 0.98372E-01 
c  r22          0.10853E-01      13   0.53140E-08   0.17933E-08 0.10004E+00 
c  r33          0.21862E-01      14   0.67085E-08   0.12305E-07 0.12563E+00 
c  r12          0.93880E-03      18   0.57396E-08   0.30136E-09 0.60552E+00 
c  r13          0.46679E-02      18   0.65751E-08   0.14717E-08 0.19796E+00 
c  r23          0.39980E-02      19   0.53340E-08   0.12742E-08 0.19756E+00 
c  epsilon      0.10969E+02      11   0.33032E-08   0.95167E-02 0.16247E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.83965E-02 0.43234E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364         0.61386       0.0052573       0.0015073
v  Velocity[Y]            -0.57345         0.54412        0.003079      0.00087251
v  Velocity[Z]              1.5657          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4411          4.3406          4.3632
v  Pressure                -36.468          360.04          87.659          169.87
v  r11                   0.0010624        0.081864        0.013076        0.018287
v  r22                   0.0011163        0.082591        0.013357        0.018647
v  r33                   0.0016449         0.17436        0.027256        0.037208
v  r12                   -0.010674        0.013585     -0.00023388     -0.00030934
v  r13                   -0.045509        0.052774      9.3373e-05       0.0010139
v  r23                   -0.046726        0.051176        3.06e-05      0.00057466
v  epsilon                0.069649          271.26          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9956e-05       0.0099174      0.00092536       0.0017429
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2778         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71353         0.85284


 TIME FOR THE TIME STEP            11170:        0.69389E+02

===============================================================


 INSTANT    0.111710000E-01   TIME STEP NUMBER           11171
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.259093005E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.385172190E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.101273955E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.163716016E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.329800123E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81229E-03   0.45250E-02 0.19917E+01 
c  Velocity[X]                                      0.13778E-03 
c  Velocity[Y]                                      0.12815E-03 
c  Velocity[Z]                                      0.42591E-02 
c  Pressure     0.36828E-04     132   0.93789E-02   0.25976E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55879E-08   0.16254E-08 0.99027E-01 
c  r22          0.10853E-01      13   0.48227E-08   0.18223E-08 0.10086E+00 
c  r33          0.21862E-01      14   0.69398E-08   0.12419E-07 0.12642E+00 
c  r12          0.93880E-03      18   0.50079E-08   0.29917E-09 0.60435E+00 
c  r13          0.46679E-02      19   0.53918E-08   0.14934E-08 0.19919E+00 
c  r23          0.39980E-02      19   0.56924E-08   0.12657E-08 0.19769E+00 
c  epsilon      0.10969E+02      11   0.32795E-08   0.98199E-02 0.16552E+00 
c  TempC        0.25716E+06      16   0.15155E-04   0.83965E-02 0.43183E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61382       0.0052573       0.0015074
v  Velocity[Y]             -0.5736         0.54391       0.0030791      0.00087255
v  Velocity[Z]              1.5657          5.4411          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4411          4.3406          4.3632
v  Pressure                -36.435          360.04          87.656          169.86
v  r11                   0.0010624         0.08186        0.013076        0.018287
v  r22                   0.0011163        0.082587        0.013357        0.018647
v  r33                   0.0016449         0.17431        0.027256        0.037208
v  r12                   -0.010669        0.013587     -0.00023388     -0.00030934
v  r13                   -0.045506        0.052773      9.3373e-05       0.0010139
v  r23                   -0.046726        0.051173        3.06e-05      0.00057466
v  epsilon                 0.06965          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9954e-05       0.0099174      0.00092536       0.0017429
v  CourantNb               0.44257             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2777         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            11171:        0.72747E+02

===============================================================


 INSTANT    0.111720000E-01   TIME STEP NUMBER           11172
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.275740022E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.102259793E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.219162410E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.218813489E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.412191718E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81419E-03   0.45322E-02 0.19937E+01 
c  Velocity[X]                                      0.13772E-03 
c  Velocity[Y]                                      0.12813E-03 
c  Velocity[Z]                                      0.42664E-02 
c  Pressure     0.36553E-04     133   0.93057E-02   0.25782E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54512E-08   0.16490E-08 0.99865E-01 
c  r22          0.10853E-01      13   0.49415E-08   0.18421E-08 0.10137E+00 
c  r33          0.21862E-01      15   0.62995E-08   0.12650E-07 0.12739E+00 
c  r12          0.93880E-03      18   0.52856E-08   0.30324E-09 0.60988E+00 
c  r13          0.46679E-02      20   0.61327E-08   0.14977E-08 0.20012E+00 
c  r23          0.39980E-02      19   0.59818E-08   0.12867E-08 0.19938E+00 
c  epsilon      0.10969E+02      11   0.33622E-08   0.10162E-01 0.16719E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.84199E-02 0.43302E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61388       0.0052573       0.0015073
v  Velocity[Y]            -0.57349         0.54382        0.003079      0.00087254
v  Velocity[Z]              1.5655          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4412          4.3406          4.3632
v  Pressure                -36.485          360.05           87.68          169.88
v  r11                   0.0010624        0.081859        0.013076        0.018287
v  r22                   0.0011163        0.082588        0.013357        0.018647
v  r33                   0.0016449         0.17432        0.027256        0.037208
v  r12                   -0.010674        0.013587     -0.00023388     -0.00030934
v  r13                   -0.045505        0.052772      9.3374e-05       0.0010139
v  r23                   -0.046726         0.05116        3.06e-05      0.00057466
v  epsilon                0.069652          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9947e-05       0.0099174      0.00092536       0.0017429
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017895          5.2774         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71353         0.85284


 TIME FOR THE TIME STEP            11172:        0.68650E+02

===============================================================


 INSTANT    0.111730000E-01   TIME STEP NUMBER           11173
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.369834122E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.617802741E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.318936809E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.833722569E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110153059E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81243E-03   0.44874E-02 0.19819E+01 
c  Velocity[X]                                      0.13673E-03 
c  Velocity[Y]                                      0.12687E-03 
c  Velocity[Z]                                      0.42238E-02 
c  Pressure     0.35975E-04     132   0.91553E-02   0.25372E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52304E-08   0.16361E-08 0.99223E-01 
c  r22          0.10853E-01      13   0.50747E-08   0.18130E-08 0.10050E+00 
c  r33          0.21862E-01      15   0.64968E-08   0.12442E-07 0.12600E+00 
c  r12          0.93880E-03      18   0.60852E-08   0.30321E-09 0.60831E+00 
c  r13          0.46679E-02      20   0.62711E-08   0.15005E-08 0.19994E+00 
c  r23          0.39980E-02      19   0.56474E-08   0.12869E-08 0.19812E+00 
c  epsilon      0.10969E+02      11   0.33945E-08   0.99022E-02 0.16571E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.83439E-02 0.43140E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63355         0.61387       0.0052572       0.0015073
v  Velocity[Y]            -0.57358         0.54385        0.003079      0.00087248
v  Velocity[Z]              1.5656          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4412          4.3406          4.3632
v  Pressure                -36.419          359.99          87.622          169.82
v  r11                   0.0010624        0.081857        0.013076        0.018287
v  r22                   0.0011163         0.08259        0.013357        0.018647
v  r33                   0.0016449         0.17434        0.027256        0.037208
v  r12                   -0.010676        0.013585     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052772      9.3375e-05       0.0010139
v  r23                   -0.046725        0.051187      3.0601e-05      0.00057466
v  epsilon                0.069653          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9943e-05       0.0099173      0.00092536       0.0017429
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2764         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8764         0.71352         0.85284


 TIME FOR THE TIME STEP            11173:        0.70460E+02

===============================================================


 INSTANT    0.111740000E-01   TIME STEP NUMBER           11174
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151892754E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.287013032E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.255965509E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.250577321E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.166697789E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81328E-03   0.45145E-02 0.19913E+01 
c  Velocity[X]                                      0.13689E-03 
c  Velocity[Y]                                      0.12874E-03 
c  Velocity[Z]                                      0.42489E-02 
c  Pressure     0.36712E-04     133   0.93467E-02   0.25894E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51715E-08   0.16473E-08 0.99393E-01 
c  r22          0.10853E-01      13   0.50876E-08   0.18020E-08 0.10050E+00 
c  r33          0.21862E-01      15   0.60743E-08   0.12442E-07 0.12638E+00 
c  r12          0.93880E-03      18   0.59112E-08   0.29759E-09 0.60703E+00 
c  r13          0.46679E-02      19   0.74299E-08   0.14682E-08 0.19825E+00 
c  r23          0.39980E-02      19   0.54329E-08   0.12983E-08 0.19943E+00 
c  epsilon      0.10969E+02      11   0.33345E-08   0.10023E-01 0.16947E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.83487E-02 0.43039E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63366         0.61384       0.0052573       0.0015074
v  Velocity[Y]            -0.57348         0.54398        0.003079      0.00087249
v  Velocity[Z]              1.5659          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4412          4.3406          4.3632
v  Pressure                -36.459             360          87.652          169.84
v  r11                   0.0010624         0.08186        0.013076        0.018287
v  r22                   0.0011163        0.082591        0.013357        0.018647
v  r33                   0.0016449         0.17435        0.027256        0.037208
v  r12                   -0.010674        0.013591     -0.00023388     -0.00030934
v  r13                   -0.045505        0.052772      9.3376e-05       0.0010139
v  r23                   -0.046725         0.05118      3.0602e-05      0.00057466
v  epsilon                0.069654          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.994e-05       0.0099174      0.00092536       0.0017429
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2762         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8762         0.71352         0.85284


 TIME FOR THE TIME STEP            11174:        0.70227E+02

===============================================================


 INSTANT    0.111750000E-01   TIME STEP NUMBER           11175
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.304226867E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.567847514E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.326078221E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.215708816E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276726319E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81155E-03   0.44726E-02 0.19837E+01 
c  Velocity[X]                                      0.13751E-03 
c  Velocity[Y]                                      0.12797E-03 
c  Velocity[Z]                                      0.42071E-02 
c  Pressure     0.35982E-04     132   0.91516E-02   0.25380E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51133E-08   0.16569E-08 0.99337E-01 
c  r22          0.10853E-01      13   0.49078E-08   0.18431E-08 0.10085E+00 
c  r33          0.21862E-01      15   0.54421E-08   0.12635E-07 0.12662E+00 
c  r12          0.93880E-03      18   0.57533E-08   0.30695E-09 0.61072E+00 
c  r13          0.46679E-02      19   0.55255E-08   0.15012E-08 0.19959E+00 
c  r23          0.39980E-02      19   0.55485E-08   0.12867E-08 0.19802E+00 
c  epsilon      0.10969E+02      11   0.33353E-08   0.10043E-01 0.16533E+00 
c  TempC        0.25716E+06      16   0.15112E-04   0.84500E-02 0.43363E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61387       0.0052573       0.0015074
v  Velocity[Y]            -0.57356         0.54415       0.0030791      0.00087252
v  Velocity[Z]              1.5656          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4412          4.3406          4.3632
v  Pressure                -36.417          360.07          87.665          169.89
v  r11                   0.0010624        0.081858        0.013076        0.018287
v  r22                   0.0011163        0.082591        0.013357        0.018647
v  r33                   0.0016449         0.17437        0.027256        0.037208
v  r12                   -0.010669        0.013598     -0.00023388     -0.00030934
v  r13                   -0.045504        0.052769      9.3377e-05       0.0010139
v  r23                   -0.046726         0.05117      3.0602e-05      0.00057466
v  epsilon                0.069655           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099173      0.00092536       0.0017429
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2766         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8766         0.71352         0.85284


 TIME FOR THE TIME STEP            11175:        0.69367E+02

===============================================================


 INSTANT    0.111760000E-01   TIME STEP NUMBER           11176
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.532530176E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.691874031E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.281720893E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.231661529E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.662383847E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81339E-03   0.44923E-02 0.19841E+01 
c  Velocity[X]                                      0.13732E-03 
c  Velocity[Y]                                      0.12669E-03 
c  Velocity[Z]                                      0.42283E-02 
c  Pressure     0.36472E-04     132   0.92857E-02   0.25725E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54717E-08   0.15999E-08 0.97836E-01 
c  r22          0.10853E-01      13   0.48697E-08   0.18037E-08 0.99846E-01 
c  r33          0.21862E-01      15   0.57573E-08   0.12264E-07 0.12515E+00 
c  r12          0.93880E-03      18   0.61174E-08   0.29936E-09 0.60359E+00 
c  r13          0.46679E-02      19   0.63093E-08   0.14911E-08 0.19844E+00 
c  r23          0.39980E-02      19   0.53417E-08   0.12482E-08 0.19585E+00 
c  epsilon      0.10969E+02      11   0.34227E-08   0.95368E-02 0.16133E+00 
c  TempC        0.25716E+06      16   0.15185E-04   0.83343E-02 0.43144E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61385       0.0052573       0.0015074
v  Velocity[Y]             -0.5735         0.54393        0.003079      0.00087243
v  Velocity[Z]              1.5657          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4412          4.3406          4.3632
v  Pressure                 -36.46          360.03          87.649          169.86
v  r11                   0.0010624        0.081862        0.013076        0.018287
v  r22                   0.0011163         0.08259        0.013357        0.018647
v  r33                   0.0016449         0.17438        0.027256        0.037208
v  r12                   -0.010666        0.013601     -0.00023388     -0.00030934
v  r13                   -0.045507        0.052769      9.3377e-05       0.0010139
v  r23                   -0.046726        0.051192      3.0602e-05      0.00057466
v  epsilon                0.069656           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099173      0.00092536       0.0017429
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017896          5.2769         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71352         0.85284


 TIME FOR THE TIME STEP            11176:        0.70849E+02

===============================================================


 INSTANT    0.111770000E-01   TIME STEP NUMBER           11177
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.200544383E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195437074E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.814763672E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.820716375E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.351526589E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81259E-03   0.45385E-02 0.19932E+01 
c  Velocity[X]                                      0.13768E-03 
c  Velocity[Y]                                      0.12786E-03 
c  Velocity[Z]                                      0.42729E-02 
c  Pressure     0.36202E-04     133   0.92246E-02   0.25534E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51901E-08   0.16266E-08 0.98561E-01 
c  r22          0.10853E-01      13   0.50502E-08   0.18257E-08 0.10043E+00 
c  r33          0.21862E-01      15   0.67867E-08   0.12479E-07 0.12594E+00 
c  r12          0.93880E-03      18   0.60208E-08   0.30552E-09 0.61129E+00 
c  r13          0.46679E-02      19   0.63377E-08   0.15027E-08 0.19875E+00 
c  r23          0.39980E-02      19   0.56153E-08   0.12834E-08 0.19816E+00 
c  epsilon      0.10969E+02      11   0.33110E-08   0.98916E-02 0.16523E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.84046E-02 0.43249E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63355         0.61383       0.0052573       0.0015073
v  Velocity[Y]            -0.57352         0.54405       0.0030789      0.00087243
v  Velocity[Z]              1.5656          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4412          4.3406          4.3632
v  Pressure                -36.415          359.97          87.626          169.82
v  r11                   0.0010624        0.081862        0.013076        0.018287
v  r22                   0.0011163         0.08259        0.013357        0.018647
v  r33                   0.0016449          0.1744        0.027256        0.037208
v  r12                   -0.010667        0.013599     -0.00023388     -0.00030934
v  r13                   -0.045507        0.052769      9.3378e-05       0.0010139
v  r23                   -0.046727        0.051185      3.0602e-05      0.00057466
v  epsilon                0.069658          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099172      0.00092536       0.0017429
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2772         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71353         0.85284


 TIME FOR THE TIME STEP            11177:        0.70681E+02

===============================================================


 INSTANT    0.111780000E-01   TIME STEP NUMBER           11178
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.549789792E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.498458980E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.883892206E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.870274627E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209655038E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69756E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81305E-03   0.44911E-02 0.19848E+01 
c  Velocity[X]                                      0.13643E-03 
c  Velocity[Y]                                      0.12819E-03 
c  Velocity[Z]                                      0.42265E-02 
c  Pressure     0.35860E-04     133   0.91319E-02   0.25292E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53931E-08   0.16214E-08 0.98786E-01 
c  r22          0.10853E-01      13   0.47735E-08   0.18094E-08 0.10033E+00 
c  r33          0.21862E-01      15   0.61325E-08   0.12357E-07 0.12582E+00 
c  r12          0.93880E-03      18   0.56417E-08   0.30620E-09 0.61105E+00 
c  r13          0.46679E-02      19   0.59783E-08   0.14931E-08 0.19919E+00 
c  r23          0.39980E-02      19   0.52102E-08   0.12724E-08 0.19807E+00 
c  epsilon      0.10969E+02      11   0.32389E-08   0.96758E-02 0.16401E+00 
c  TempC        0.25716E+06      16   0.15142E-04   0.85011E-02 0.43482E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61385       0.0052573       0.0015074
v  Velocity[Y]            -0.57346         0.54424       0.0030789      0.00087237
v  Velocity[Z]              1.5656          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4412          4.3406          4.3632
v  Pressure                -36.471             360          87.647          169.84
v  r11                   0.0010624        0.081865        0.013076        0.018287
v  r22                   0.0011163        0.082589        0.013357        0.018647
v  r33                   0.0016449         0.17441        0.027256        0.037208
v  r12                   -0.010665        0.013603     -0.00023388     -0.00030934
v  r13                   -0.045505        0.052771      9.3378e-05       0.0010139
v  r23                   -0.046728        0.051174      3.0603e-05      0.00057466
v  epsilon                0.069659          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099173      0.00092536       0.0017429
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2777         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            11178:        0.72478E+02

===============================================================


 INSTANT    0.111790000E-01   TIME STEP NUMBER           11179
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178427993E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138463673E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.803136683E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.312129149E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.254058584E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69757E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81370E-03   0.45058E-02 0.19877E+01 
c  Velocity[X]                                      0.13695E-03 
c  Velocity[Y]                                      0.12742E-03 
c  Velocity[Z]                                      0.42415E-02 
c  Pressure     0.36589E-04     133   0.93169E-02   0.25808E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56427E-08   0.16106E-08 0.98331E-01 
c  r22          0.10853E-01      13   0.49646E-08   0.18044E-08 0.10002E+00 
c  r33          0.21862E-01      15   0.56960E-08   0.12379E-07 0.12586E+00 
c  r12          0.93880E-03      18   0.53292E-08   0.29207E-09 0.60147E+00 
c  r13          0.46679E-02      19   0.63220E-08   0.14800E-08 0.19779E+00 
c  r23          0.39980E-02      19   0.53168E-08   0.12698E-08 0.19805E+00 
c  epsilon      0.10969E+02      11   0.33520E-08   0.97458E-02 0.16349E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.83938E-02 0.43177E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61384       0.0052573       0.0015074
v  Velocity[Y]            -0.57346         0.54391       0.0030789      0.00087238
v  Velocity[Z]              1.5658          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4412          4.3406          4.3632
v  Pressure                -36.426          360.01          87.631          169.83
v  r11                   0.0010624        0.081863        0.013076        0.018287
v  r22                   0.0011163        0.082586        0.013357        0.018647
v  r33                   0.0016449         0.17437        0.027256        0.037208
v  r12                   -0.010671        0.013608     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052772      9.3379e-05       0.0010139
v  r23                   -0.046729        0.051177      3.0603e-05      0.00057466
v  epsilon                 0.06966          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099174      0.00092536       0.0017429
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2779         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            11179:        0.71165E+02

===============================================================


 INSTANT    0.111800000E-01   TIME STEP NUMBER           11180
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.118101283E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.235571497E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.187832048E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.318131619E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.522751897E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81270E-03   0.45059E-02 0.19865E+01 
c  Velocity[X]                                      0.13757E-03 
c  Velocity[Y]                                      0.12706E-03 
c  Velocity[Z]                                      0.42412E-02 
c  Pressure     0.36361E-04     132   0.92639E-02   0.25647E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56636E-08   0.16700E-08 0.99997E-01 
c  r22          0.10853E-01      13   0.49302E-08   0.18116E-08 0.10057E+00 
c  r33          0.21862E-01      15   0.71178E-08   0.12688E-07 0.12760E+00 
c  r12          0.93880E-03      18   0.57109E-08   0.29977E-09 0.60916E+00 
c  r13          0.46679E-02      20   0.60088E-08   0.14811E-08 0.19976E+00 
c  r23          0.39980E-02      18   0.68258E-08   0.13093E-08 0.20111E+00 
c  epsilon      0.10969E+02      11   0.35747E-08   0.10516E-01 0.17404E+00 
c  TempC        0.25716E+06      16   0.15172E-04   0.83690E-02 0.43186E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63362         0.61382       0.0052574       0.0015074
v  Velocity[Y]            -0.57342         0.54398       0.0030789      0.00087239
v  Velocity[Z]              1.5657          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4412          4.3406          4.3632
v  Pressure                -36.467          360.02          87.635          169.84
v  r11                   0.0010624        0.081872        0.013076        0.018287
v  r22                   0.0011163        0.082587        0.013357        0.018647
v  r33                   0.0016449         0.17433        0.027256        0.037209
v  r12                   -0.010671        0.013603     -0.00023388     -0.00030934
v  r13                   -0.045505        0.052771       9.338e-05       0.0010139
v  r23                    -0.04673        0.051207      3.0604e-05      0.00057466
v  epsilon                0.069661          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099177      0.00092536       0.0017429
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2782         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            11180:        0.69518E+02

===============================================================


 INSTANT    0.111810000E-01   TIME STEP NUMBER           11181
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.307306688E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.571354368E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.198009590E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.106879919E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.350278792E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69758E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81260E-03   0.44927E-02 0.19836E+01 
c  Velocity[X]                                      0.13725E-03 
c  Velocity[Y]                                      0.12824E-03 
c  Velocity[Z]                                      0.42272E-02 
c  Pressure     0.36231E-04     131   0.92086E-02   0.25555E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61271E-08   0.15941E-08 0.98639E-01 
c  r22          0.10853E-01      12   0.65679E-08   0.17802E-08 0.99963E-01 
c  r33          0.21862E-01      15   0.64200E-08   0.12130E-07 0.12540E+00 
c  r12          0.93880E-03      18   0.53096E-08   0.29253E-09 0.60309E+00 
c  r13          0.46679E-02      19   0.72711E-08   0.14649E-08 0.19816E+00 
c  r23          0.39980E-02      18   0.67403E-08   0.12485E-08 0.19680E+00 
c  epsilon      0.10969E+02      11   0.33615E-08   0.93556E-02 0.16122E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.83697E-02 0.43197E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63359         0.61381       0.0052574       0.0015074
v  Velocity[Y]            -0.57348         0.54414       0.0030789      0.00087237
v  Velocity[Z]              1.5658          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4412          4.3406          4.3632
v  Pressure                -36.416          360.04          87.647          169.85
v  r11                   0.0010624        0.081876        0.013076        0.018287
v  r22                   0.0011163         0.08259        0.013357        0.018647
v  r33                   0.0016449         0.17433        0.027256        0.037209
v  r12                    -0.01067        0.013606     -0.00023388     -0.00030934
v  r13                   -0.045506         0.05277      9.3381e-05       0.0010139
v  r23                   -0.046731        0.051197      3.0605e-05      0.00057466
v  epsilon                0.069662          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099178      0.00092536       0.0017429
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017897          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            11181:        0.69720E+02

===============================================================


 INSTANT    0.111820000E-01   TIME STEP NUMBER           11182
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.501777953E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116307024E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934908E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.116216600E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.406127086E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.559255204E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81331E-03   0.44816E-02 0.19842E+01 
c  Velocity[X]                                      0.13645E-03 
c  Velocity[Y]                                      0.12723E-03 
c  Velocity[Z]                                      0.42180E-02 
c  Pressure     0.36557E-04     132   0.93023E-02   0.25785E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.64285E-08   0.16075E-08 0.98560E-01 
c  r22          0.10853E-01      13   0.45337E-08   0.18015E-08 0.10079E+00 
c  r33          0.21862E-01      15   0.53518E-08   0.12333E-07 0.12639E+00 
c  r12          0.93880E-03      18   0.55032E-08   0.29298E-09 0.60335E+00 
c  r13          0.46679E-02      20   0.61031E-08   0.14613E-08 0.19866E+00 
c  r23          0.39980E-02      18   0.66960E-08   0.12553E-08 0.19706E+00 
c  epsilon      0.10969E+02      11   0.32189E-08   0.95757E-02 0.16137E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.83237E-02 0.43029E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369         0.61383       0.0052573       0.0015074
v  Velocity[Y]            -0.57337         0.54397       0.0030788      0.00087235
v  Velocity[Z]              1.5659          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4412          4.3406          4.3632
v  Pressure                -36.472          360.08          87.697           169.9
v  r11                   0.0010624        0.081877        0.013076        0.018287
v  r22                   0.0011163        0.082591        0.013357        0.018647
v  r33                    0.001645         0.17434        0.027256        0.037209
v  r12                   -0.010671          0.0136     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052771      9.3382e-05       0.0010139
v  r23                   -0.046732        0.051179      3.0605e-05      0.00057467
v  epsilon                0.069663          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099179      0.00092536       0.0017429
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2784         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85284


 TIME FOR THE TIME STEP            11182:        0.69595E+02

===============================================================


 INSTANT    0.111830000E-01   TIME STEP NUMBER           11183
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.272210873E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.329040150E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.250473931E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.699858220E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.309611664E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81231E-03   0.45099E-02 0.19894E+01 
c  Velocity[X]                                      0.13701E-03 
c  Velocity[Y]                                      0.12765E-03 
c  Velocity[Z]                                      0.42452E-02 
c  Pressure     0.35937E-04     133   0.91434E-02   0.25348E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.66620E-08   0.16038E-08 0.98517E-01 
c  r22          0.10853E-01      13   0.46572E-08   0.18207E-08 0.10070E+00 
c  r33          0.21862E-01      15   0.57635E-08   0.12294E-07 0.12600E+00 
c  r12          0.93880E-03      18   0.58575E-08   0.30202E-09 0.60932E+00 
c  r13          0.46679E-02      20   0.66211E-08   0.15139E-08 0.20047E+00 
c  r23          0.39980E-02      19   0.66169E-08   0.12703E-08 0.19760E+00 
c  epsilon      0.10969E+02      11   0.32159E-08   0.96377E-02 0.16324E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.84415E-02 0.43381E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61378       0.0052573       0.0015074
v  Velocity[Y]            -0.57348         0.54408       0.0030788      0.00087233
v  Velocity[Z]              1.5658          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4412          4.3406          4.3632
v  Pressure                -36.402          359.99          87.635          169.83
v  r11                   0.0010624        0.081878        0.013076        0.018287
v  r22                   0.0011163        0.082592        0.013357        0.018647
v  r33                    0.001645         0.17436        0.027256        0.037209
v  r12                    -0.01067        0.013602     -0.00023388     -0.00030934
v  r13                   -0.045505        0.052772      9.3382e-05       0.0010139
v  r23                   -0.046732        0.051168      3.0606e-05      0.00057467
v  epsilon                0.069665          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.994e-05       0.0099178      0.00092536       0.0017429
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            11183:        0.70795E+02

===============================================================


 INSTANT    0.111840000E-01   TIME STEP NUMBER           11184
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.805482836E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33841E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.300578558E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33841E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.314139131E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33841E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179858093E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33841E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.385956902E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33841E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81328E-03   0.45124E-02 0.19887E+01 
c  Velocity[X]                                      0.13703E-03 
c  Velocity[Y]                                      0.12803E-03 
c  Velocity[Z]                                      0.42473E-02 
c  Pressure     0.36266E-04     133   0.92346E-02   0.25580E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58905E-08   0.15944E-08 0.98422E-01 
c  r22          0.10853E-01      13   0.55117E-08   0.18045E-08 0.10027E+00 
c  r33          0.21862E-01      14   0.70850E-08   0.12254E-07 0.12552E+00 
c  r12          0.93880E-03      18   0.70464E-08   0.29910E-09 0.60604E+00 
c  r13          0.46679E-02      20   0.66747E-08   0.15046E-08 0.19927E+00 
c  r23          0.39980E-02      19   0.64884E-08   0.12616E-08 0.19657E+00 
c  epsilon      0.10969E+02      11   0.31340E-08   0.97303E-02 0.16472E+00 
c  TempC        0.25716E+06      16   0.15190E-04   0.84242E-02 0.43280E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361         0.61382       0.0052573       0.0015074
v  Velocity[Y]            -0.57353         0.54411       0.0030788      0.00087233
v  Velocity[Z]              1.5657          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4412          4.3406          4.3632
v  Pressure                 -36.46          359.98          87.619          169.82
v  r11                   0.0010624        0.081884        0.013077        0.018287
v  r22                   0.0011163        0.082593        0.013357        0.018647
v  r33                    0.001645         0.17439        0.027256        0.037209
v  r12                   -0.010669        0.013605     -0.00023388     -0.00030934
v  r13                   -0.045504        0.052775      9.3384e-05       0.0010139
v  r23                   -0.046733        0.051196      3.0606e-05      0.00057467
v  epsilon                0.069666          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9939e-05       0.0099178      0.00092537       0.0017429
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017898           5.279         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71353         0.85284


 TIME FOR THE TIME STEP            11184:        0.68843E+02

===============================================================


 INSTANT    0.111850000E-01   TIME STEP NUMBER           11185
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.135796471E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.397012316E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117893040E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.255693750E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.132200783E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81317E-03   0.45062E-02 0.19861E+01 
c  Velocity[X]                                      0.13719E-03 
c  Velocity[Y]                                      0.12720E-03 
c  Velocity[Z]                                      0.42418E-02 
c  Pressure     0.36221E-04     132   0.92249E-02   0.25548E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54818E-08   0.16138E-08 0.98353E-01 
c  r22          0.10853E-01      13   0.52546E-08   0.17889E-08 0.99971E-01 
c  r33          0.21862E-01      14   0.68592E-08   0.12326E-07 0.12572E+00 
c  r12          0.93880E-03      19   0.56770E-08   0.29187E-09 0.60105E+00 
c  r13          0.46679E-02      19   0.73739E-08   0.14773E-08 0.19824E+00 
c  r23          0.39980E-02      19   0.64924E-08   0.12675E-08 0.19716E+00 
c  epsilon      0.10969E+02      11   0.32443E-08   0.97598E-02 0.16289E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.83591E-02 0.43111E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364         0.61377       0.0052573       0.0015074
v  Velocity[Y]            -0.57355         0.54416       0.0030787       0.0008723
v  Velocity[Z]              1.5656          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4412          4.3406          4.3632
v  Pressure                -36.411          360.03          87.635          169.85
v  r11                   0.0010624        0.081883        0.013077        0.018287
v  r22                   0.0011163        0.082595        0.013357        0.018647
v  r33                    0.001645          0.1744        0.027256        0.037209
v  r12                   -0.010668        0.013609     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052776      9.3384e-05       0.0010139
v  r23                   -0.046733        0.051195      3.0605e-05      0.00057467
v  epsilon                0.069667          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9942e-05       0.0099177      0.00092537       0.0017429
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2787         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85284


 TIME FOR THE TIME STEP            11185:        0.71097E+02

===============================================================


 INSTANT    0.111860000E-01   TIME STEP NUMBER           11186
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.213093879E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.272079294E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934909E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.354469702E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.425978797E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.134689330E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81309E-03   0.45171E-02 0.19906E+01 
c  Velocity[X]                                      0.13760E-03 
c  Velocity[Y]                                      0.12856E-03 
c  Velocity[Z]                                      0.42510E-02 
c  Pressure     0.36321E-04     133   0.92449E-02   0.25618E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60213E-08   0.16190E-08 0.98690E-01 
c  r22          0.10853E-01      13   0.57749E-08   0.18007E-08 0.10031E+00 
c  r33          0.21862E-01      15   0.58530E-08   0.12339E-07 0.12605E+00 
c  r12          0.93880E-03      19   0.58659E-08   0.29066E-09 0.60058E+00 
c  r13          0.46679E-02      19   0.74431E-08   0.14718E-08 0.19860E+00 
c  r23          0.39980E-02      19   0.60519E-08   0.12602E-08 0.19715E+00 
c  epsilon      0.10969E+02      11   0.33610E-08   0.10238E-01 0.17153E+00 
c  TempC        0.25716E+06      16   0.15194E-04   0.84410E-02 0.43305E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61379       0.0052573       0.0015074
v  Velocity[Y]             -0.5735         0.54422       0.0030787       0.0008723
v  Velocity[Z]              1.5656          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4412          4.3406          4.3632
v  Pressure                -36.442          360.03          87.663          169.86
v  r11                   0.0010624        0.081887        0.013077        0.018287
v  r22                   0.0011163        0.082596        0.013357        0.018647
v  r33                    0.001645         0.17441        0.027256        0.037209
v  r12                   -0.010667        0.013604     -0.00023388     -0.00030934
v  r13                   -0.045506        0.052775      9.3385e-05        0.001014
v  r23                   -0.046733        0.051187      3.0606e-05      0.00057467
v  epsilon                0.069668          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9944e-05       0.0099176      0.00092537       0.0017429
v  CourantNb               0.44254             0.6         0.59908         0.59839
v  FourierNb             0.0017898          5.2786         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            11186:        0.70603E+02

===============================================================


 INSTANT    0.111870000E-01   TIME STEP NUMBER           11187
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.459694734E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.446723606E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141133710E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.937722298E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.375953864E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81307E-03   0.45150E-02 0.19897E+01 
c  Velocity[X]                                      0.13743E-03 
c  Velocity[Y]                                      0.12857E-03 
c  Velocity[Z]                                      0.42490E-02 
c  Pressure     0.36136E-04     134   0.92035E-02   0.25488E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.63289E-08   0.16125E-08 0.98602E-01 
c  r22          0.10853E-01      13   0.57495E-08   0.18133E-08 0.10085E+00 
c  r33          0.21862E-01      15   0.58316E-08   0.12383E-07 0.12599E+00 
c  r12          0.93880E-03      19   0.55351E-08   0.30036E-09 0.60783E+00 
c  r13          0.46679E-02      20   0.68538E-08   0.14938E-08 0.19939E+00 
c  r23          0.39980E-02      19   0.54353E-08   0.12607E-08 0.19636E+00 
c  epsilon      0.10969E+02      11   0.34306E-08   0.98588E-02 0.16459E+00 
c  TempC        0.25716E+06      16   0.15135E-04   0.84312E-02 0.43335E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61376       0.0052573       0.0015074
v  Velocity[Y]            -0.57355         0.54429       0.0030787      0.00087232
v  Velocity[Z]              1.5657          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4412          4.3406          4.3632
v  Pressure                -36.445           360.1          87.718          169.93
v  r11                   0.0010624        0.081885        0.013077        0.018287
v  r22                   0.0011163        0.082597        0.013357        0.018647
v  r33                    0.001645         0.17437        0.027256        0.037209
v  r12                   -0.010667        0.013605     -0.00023388     -0.00030934
v  r13                   -0.045505        0.052775      9.3385e-05        0.001014
v  r23                   -0.046733        0.051175      3.0606e-05      0.00057467
v  epsilon                0.069669          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099176      0.00092537       0.0017429
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017898           5.278         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            11187:        0.70135E+02

===============================================================


 INSTANT    0.111880000E-01   TIME STEP NUMBER           11188
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105863087E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.726036070E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199085416E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935018E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267618974E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.197288896E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81327E-03   0.44659E-02 0.19777E+01 
c  Velocity[X]                                      0.13609E-03 
c  Velocity[Y]                                      0.12690E-03 
c  Velocity[Z]                                      0.42029E-02 
c  Pressure     0.36246E-04     133   0.92320E-02   0.25565E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60237E-08   0.16077E-08 0.98530E-01 
c  r22          0.10853E-01      13   0.59786E-08   0.18068E-08 0.10075E+00 
c  r33          0.21862E-01      15   0.59555E-08   0.12385E-07 0.12628E+00 
c  r12          0.93880E-03      19   0.54534E-08   0.29758E-09 0.60538E+00 
c  r13          0.46679E-02      20   0.66275E-08   0.14985E-08 0.19953E+00 
c  r23          0.39980E-02      19   0.59351E-08   0.12748E-08 0.19802E+00 
c  epsilon      0.10969E+02      11   0.35449E-08   0.97502E-02 0.16431E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.83209E-02 0.43098E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61374       0.0052572       0.0015074
v  Velocity[Y]            -0.57343         0.54409       0.0030787      0.00087227
v  Velocity[Z]              1.5655          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4412          4.3406          4.3632
v  Pressure                -36.427          360.04          87.669          169.87
v  r11                   0.0010624        0.081885        0.013077        0.018287
v  r22                   0.0011163        0.082596        0.013357        0.018647
v  r33                    0.001645         0.17433        0.027256        0.037209
v  r12                   -0.010668        0.013608     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052777      9.3385e-05       0.0010139
v  r23                   -0.046734        0.051201      3.0606e-05      0.00057467
v  epsilon                0.069671          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9945e-05       0.0099177      0.00092537       0.0017429
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            11188:        0.70551E+02

===============================================================


 INSTANT    0.111890000E-01   TIME STEP NUMBER           11189
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.724714251E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.445174905E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.366567034E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.105745112E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.285060959E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81160E-03   0.45057E-02 0.19878E+01 
c  Velocity[X]                                      0.13705E-03 
c  Velocity[Y]                                      0.12780E-03 
c  Velocity[Z]                                      0.42409E-02 
c  Pressure     0.36262E-04     131   0.92300E-02   0.25576E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58637E-08   0.16188E-08 0.98871E-01 
c  r22          0.10853E-01      13   0.56163E-08   0.18108E-08 0.10049E+00 
c  r33          0.21862E-01      14   0.70536E-08   0.12304E-07 0.12586E+00 
c  r12          0.93880E-03      18   0.68286E-08   0.29963E-09 0.60807E+00 
c  r13          0.46679E-02      19   0.69978E-08   0.14836E-08 0.19870E+00 
c  r23          0.39980E-02      19   0.57080E-08   0.12697E-08 0.19778E+00 
c  epsilon      0.10969E+02      11   0.32523E-08   0.98332E-02 0.16542E+00 
c  TempC        0.25716E+06      16   0.15169E-04   0.84186E-02 0.43239E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63365         0.61378       0.0052572       0.0015074
v  Velocity[Y]             -0.5736          0.5442       0.0030787      0.00087229
v  Velocity[Z]              1.5657          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4412          4.3406          4.3632
v  Pressure                -36.362          360.02          87.631          169.84
v  r11                   0.0010624        0.081886        0.013077        0.018287
v  r22                   0.0011163        0.082596        0.013357        0.018647
v  r33                    0.001645         0.17434        0.027256        0.037209
v  r12                   -0.010665        0.013604     -0.00023388     -0.00030934
v  r13                   -0.045507        0.052779      9.3386e-05        0.001014
v  r23                   -0.046734        0.051192      3.0605e-05      0.00057467
v  epsilon                0.069672          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099177      0.00092537       0.0017429
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2772         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85284


 TIME FOR THE TIME STEP            11189:        0.71694E+02

===============================================================


 INSTANT    0.111900000E-01   TIME STEP NUMBER           11190
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221041876E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221562088E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934906E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.183373640E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242829591E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226007064E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81274E-03   0.45502E-02 0.19962E+01 
c  Velocity[X]                                      0.13711E-03 
c  Velocity[Y]                                      0.12862E-03 
c  Velocity[Z]                                      0.42845E-02 
c  Pressure     0.36355E-04     133   0.92486E-02   0.25643E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59738E-08   0.16421E-08 0.99569E-01 
c  r22          0.10853E-01      13   0.49691E-08   0.18200E-08 0.10109E+00 
c  r33          0.21862E-01      15   0.52366E-08   0.12461E-07 0.12711E+00 
c  r12          0.93880E-03      18   0.61160E-08   0.29813E-09 0.60502E+00 
c  r13          0.46679E-02      20   0.57686E-08   0.14890E-08 0.20005E+00 
c  r23          0.39980E-02      19   0.63336E-08   0.12812E-08 0.19901E+00 
c  epsilon      0.10969E+02      11   0.32250E-08   0.99267E-02 0.16541E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.84156E-02 0.43258E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63371         0.61373       0.0052572       0.0015073
v  Velocity[Y]             -0.5736          0.5439       0.0030787      0.00087228
v  Velocity[Z]              1.5657          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4412          4.3406          4.3632
v  Pressure                -36.459             360           87.65          169.84
v  r11                   0.0010624        0.081882        0.013077        0.018287
v  r22                   0.0011163        0.082597        0.013357        0.018647
v  r33                    0.001645         0.17435        0.027256        0.037209
v  r12                   -0.010664        0.013606     -0.00023388     -0.00030934
v  r13                   -0.045505        0.052782      9.3386e-05        0.001014
v  r23                   -0.046733        0.051181      3.0606e-05      0.00057467
v  epsilon                0.069673          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9946e-05       0.0099177      0.00092537       0.0017429
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71352         0.85284


 TIME FOR THE TIME STEP            11190:        0.71247E+02

===============================================================


 INSTANT    0.111910000E-01   TIME STEP NUMBER           11191
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.920790378E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.756658509E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.549123607E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.216983631E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.345524024E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81332E-03   0.44705E-02 0.19776E+01 
c  Velocity[X]                                      0.13675E-03 
c  Velocity[Y]                                      0.12695E-03 
c  Velocity[Z]                                      0.42068E-02 
c  Pressure     0.36176E-04     132   0.92187E-02   0.25516E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61685E-08   0.17039E-08 0.10029E+00 
c  r22          0.10853E-01      13   0.57016E-08   0.18853E-08 0.10153E+00 
c  r33          0.21862E-01      15   0.54836E-08   0.13083E-07 0.12858E+00 
c  r12          0.93880E-03      18   0.66116E-08   0.31263E-09 0.61679E+00 
c  r13          0.46679E-02      19   0.57194E-08   0.15309E-08 0.20080E+00 
c  r23          0.39980E-02      19   0.61695E-08   0.13435E-08 0.20355E+00 
c  epsilon      0.10969E+02      11   0.33464E-08   0.10863E-01 0.17417E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.83602E-02 0.43140E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61371       0.0052573       0.0015074
v  Velocity[Y]            -0.57362         0.54395       0.0030787       0.0008723
v  Velocity[Z]              1.5655          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4412          4.3406          4.3632
v  Pressure                -36.384          360.05          87.656          169.87
v  r11                   0.0010624        0.081878        0.013077        0.018287
v  r22                   0.0011163        0.082599        0.013357        0.018647
v  r33                    0.001645         0.17437        0.027256        0.037209
v  r12                   -0.010669         0.01361     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052783      9.3387e-05        0.001014
v  r23                   -0.046732        0.051177      3.0605e-05      0.00057467
v  epsilon                0.069674          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9945e-05       0.0099177      0.00092537       0.0017429
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2776         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11191:        0.70948E+02

===============================================================


 INSTANT    0.111920000E-01   TIME STEP NUMBER           11192
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205615185E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.916314456E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934878E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105286192E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.849340387E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.454091750E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81343E-03   0.45013E-02 0.19856E+01 
c  Velocity[X]                                      0.13745E-03 
c  Velocity[Y]                                      0.12753E-03 
c  Velocity[Z]                                      0.42363E-02 
c  Pressure     0.36057E-04     131   0.91765E-02   0.25430E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58405E-08   0.16185E-08 0.98486E-01 
c  r22          0.10853E-01      13   0.55978E-08   0.18086E-08 0.10031E+00 
c  r33          0.21862E-01      15   0.52759E-08   0.12421E-07 0.12627E+00 
c  r12          0.93880E-03      18   0.64582E-08   0.29580E-09 0.60331E+00 
c  r13          0.46679E-02      18   0.69676E-08   0.14942E-08 0.19860E+00 
c  r23          0.39980E-02      19   0.58966E-08   0.12812E-08 0.19878E+00 
c  epsilon      0.10969E+02      11   0.33574E-08   0.98526E-02 0.16613E+00 
c  TempC        0.25716E+06      16   0.15176E-04   0.83835E-02 0.43174E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361         0.61372       0.0052572       0.0015074
v  Velocity[Y]            -0.57347         0.54413       0.0030786      0.00087224
v  Velocity[Z]              1.5657          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4412          4.3406          4.3632
v  Pressure                 -36.45          360.05          87.688          169.89
v  r11                   0.0010624        0.081876        0.013077        0.018287
v  r22                   0.0011163          0.0826        0.013357        0.018647
v  r33                    0.001645         0.17438        0.027256        0.037209
v  r12                   -0.010669        0.013603     -0.00023388     -0.00030934
v  r13                   -0.045506        0.052783      9.3387e-05        0.001014
v  r23                   -0.046731        0.051203      3.0605e-05      0.00057467
v  epsilon                0.069675          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.994e-05       0.0099176      0.00092537       0.0017429
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017899          5.2778         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85284


 TIME FOR THE TIME STEP            11192:        0.69570E+02

===============================================================


 INSTANT    0.111930000E-01   TIME STEP NUMBER           11193
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.699776005E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.134208270E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.142718782E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935019E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.226212859E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.287377140E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81207E-03   0.45287E-02 0.19927E+01 
c  Velocity[X]                                      0.13795E-03 
c  Velocity[Y]                                      0.12815E-03 
c  Velocity[Z]                                      0.42626E-02 
c  Pressure     0.36401E-04     131   0.92668E-02   0.25675E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56820E-08   0.16160E-08 0.98775E-01 
c  r22          0.10853E-01      13   0.55689E-08   0.18054E-08 0.10023E+00 
c  r33          0.21862E-01      15   0.54344E-08   0.12308E-07 0.12593E+00 
c  r12          0.93880E-03      18   0.63731E-08   0.29895E-09 0.60541E+00 
c  r13          0.46679E-02      19   0.56675E-08   0.14801E-08 0.19835E+00 
c  r23          0.39980E-02      19   0.54569E-08   0.12593E-08 0.19660E+00 
c  epsilon      0.10969E+02      11   0.34736E-08   0.96316E-02 0.16260E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.84476E-02 0.43389E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63366          0.6137       0.0052573       0.0015074
v  Velocity[Y]            -0.57355         0.54428       0.0030786      0.00087227
v  Velocity[Z]              1.5658          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4412          4.3406          4.3632
v  Pressure                -36.406          360.05          87.657          169.87
v  r11                   0.0010624        0.081874        0.013077        0.018287
v  r22                   0.0011163        0.082596        0.013357        0.018647
v  r33                    0.001645         0.17439        0.027256        0.037209
v  r12                   -0.010667        0.013606     -0.00023388     -0.00030934
v  r13                   -0.045507         0.05278      9.3388e-05        0.001014
v  r23                   -0.046729        0.051197      3.0606e-05      0.00057467
v  epsilon                0.069677          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099174      0.00092537       0.0017429
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2783         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71352         0.85284


 TIME FOR THE TIME STEP            11193:        0.69304E+02

===============================================================


 INSTANT    0.111940000E-01   TIME STEP NUMBER           11194
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.620562187E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.132236613E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205567437E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.499723005E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.270704576E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81300E-03   0.45069E-02 0.19870E+01 
c  Velocity[X]                                      0.13655E-03 
c  Velocity[Y]                                      0.12698E-03 
c  Velocity[Z]                                      0.42433E-02 
c  Pressure     0.36126E-04     131   0.91901E-02   0.25481E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61656E-08   0.16144E-08 0.98308E-01 
c  r22          0.10853E-01      13   0.49568E-08   0.18015E-08 0.10020E+00 
c  r33          0.21862E-01      15   0.62705E-08   0.12397E-07 0.12625E+00 
c  r12          0.93880E-03      18   0.58213E-08   0.28882E-09 0.60220E+00 
c  r13          0.46679E-02      19   0.60237E-08   0.14693E-08 0.19863E+00 
c  r23          0.39980E-02      19   0.53989E-08   0.12703E-08 0.19752E+00 
c  epsilon      0.10969E+02      11   0.35274E-08   0.97914E-02 0.16508E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.83668E-02 0.43157E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63358         0.61369       0.0052572       0.0015074
v  Velocity[Y]            -0.57353         0.54409       0.0030786      0.00087224
v  Velocity[Z]               1.566          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5798          5.4412          4.3406          4.3632
v  Pressure                -36.439          360.02           87.66          169.85
v  r11                   0.0010624        0.081878        0.013077        0.018287
v  r22                   0.0011163        0.082597        0.013357        0.018647
v  r33                    0.001645         0.17435        0.027256        0.037209
v  r12                   -0.010666        0.013609     -0.00023388     -0.00030934
v  r13                   -0.045509        0.052778      9.3389e-05        0.001014
v  r23                   -0.046727        0.051173      3.0606e-05      0.00057467
v  epsilon                0.069678          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099174      0.00092537       0.0017429
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2786         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71352         0.85284


 TIME FOR THE TIME STEP            11194:        0.65829E+02

===============================================================


 INSTANT    0.111950000E-01   TIME STEP NUMBER           11195
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.179879423E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.566539631E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.414792686E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.240075007E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.243728729E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81321E-03   0.45065E-02 0.19873E+01 
c  Velocity[X]                                      0.13713E-03 
c  Velocity[Y]                                      0.12789E-03 
c  Velocity[Z]                                      0.42415E-02 
c  Pressure     0.36302E-04     131   0.92394E-02   0.25604E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57542E-08   0.16480E-08 0.99052E-01 
c  r22          0.10853E-01      13   0.48621E-08   0.18389E-08 0.10062E+00 
c  r33          0.21862E-01      15   0.58191E-08   0.12668E-07 0.12686E+00 
c  r12          0.93880E-03      18   0.58973E-08   0.30079E-09 0.60637E+00 
c  r13          0.46679E-02      20   0.59387E-08   0.15285E-08 0.20052E+00 
c  r23          0.39980E-02      19   0.56766E-08   0.12944E-08 0.19819E+00 
c  epsilon      0.10969E+02      11   0.34814E-08   0.10466E-01 0.17034E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.83895E-02 0.43145E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63363          0.6137       0.0052572       0.0015074
v  Velocity[Y]            -0.57356         0.54405       0.0030786      0.00087223
v  Velocity[Z]              1.5658          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4412          4.3406          4.3632
v  Pressure                -36.388          360.07          87.683          169.89
v  r11                   0.0010624        0.081874        0.013077        0.018287
v  r22                   0.0011163        0.082598        0.013357        0.018647
v  r33                    0.001645         0.17433        0.027256        0.037209
v  r12                   -0.010663        0.013604     -0.00023388     -0.00030934
v  r13                   -0.045506        0.052778      9.3389e-05        0.001014
v  r23                   -0.046725        0.051198      3.0606e-05      0.00057467
v  epsilon                0.069679          271.26          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099175      0.00092537       0.0017429
v  CourantNb               0.44256             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2796         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8796         0.71353         0.85285


 TIME FOR THE TIME STEP            11195:        0.68097E+02

===============================================================


 INSTANT    0.111960000E-01   TIME STEP NUMBER           11196
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.108588875E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.462340988E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.139037783E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.760555245E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.875113215E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81339E-03   0.44982E-02 0.19849E+01 
c  Velocity[X]                                      0.13674E-03 
c  Velocity[Y]                                      0.12710E-03 
c  Velocity[Z]                                      0.42344E-02 
c  Pressure     0.36906E-04     132   0.93930E-02   0.26031E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58478E-08   0.16411E-08 0.99187E-01 
c  r22          0.10853E-01      13   0.49800E-08   0.18360E-08 0.10095E+00 
c  r33          0.21862E-01      15   0.56426E-08   0.12490E-07 0.12674E+00 
c  r12          0.93880E-03      18   0.62579E-08   0.29739E-09 0.60347E+00 
c  r13          0.46679E-02      19   0.66753E-08   0.15054E-08 0.19984E+00 
c  r23          0.39980E-02      19   0.54360E-08   0.12822E-08 0.19788E+00 
c  epsilon      0.10969E+02      11   0.33515E-08   0.10059E-01 0.16682E+00 
c  TempC        0.25716E+06      16   0.15172E-04   0.84239E-02 0.43333E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63366          0.6137       0.0052573       0.0015074
v  Velocity[Y]            -0.57344         0.54412       0.0030785      0.00087222
v  Velocity[Z]              1.5658          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4412          4.3406          4.3632
v  Pressure                 -36.45          360.07          87.684          169.89
v  r11                   0.0010624        0.081872        0.013077        0.018287
v  r22                   0.0011164        0.082599        0.013357        0.018647
v  r33                    0.001645         0.17432        0.027256        0.037209
v  r12                   -0.010661        0.013606     -0.00023388     -0.00030934
v  r13                   -0.045505        0.052778       9.339e-05        0.001014
v  r23                   -0.046724        0.051191      3.0607e-05      0.00057467
v  epsilon                 0.06968          271.27          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099175      0.00092537       0.0017429
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2794         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8794         0.71353         0.85284


 TIME FOR THE TIME STEP            11196:        0.67322E+02

===============================================================


 INSTANT    0.111970000E-01   TIME STEP NUMBER           11197
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.194494469E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.330910289E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.570397489E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.484008422E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.132278125E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31857E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81237E-03   0.44973E-02 0.19848E+01 
c  Velocity[X]                                      0.13710E-03 
c  Velocity[Y]                                      0.12705E-03 
c  Velocity[Z]                                      0.42331E-02 
c  Pressure     0.36199E-04     131   0.92134E-02   0.25531E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56205E-08   0.16676E-08 0.99727E-01 
c  r22          0.10853E-01      13   0.50947E-08   0.18436E-08 0.10105E+00 
c  r33          0.21862E-01      15   0.59931E-08   0.12763E-07 0.12766E+00 
c  r12          0.93880E-03      18   0.57873E-08   0.30279E-09 0.60994E+00 
c  r13          0.46679E-02      19   0.58327E-08   0.14904E-08 0.19943E+00 
c  r23          0.39980E-02      19   0.50652E-08   0.13031E-08 0.19984E+00 
c  epsilon      0.10969E+02      11   0.35006E-08   0.10495E-01 0.17428E+00 
c  TempC        0.25716E+06      16   0.15123E-04   0.83750E-02 0.43182E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63371         0.61368       0.0052572       0.0015074
v  Velocity[Y]            -0.57352          0.5442       0.0030785      0.00087218
v  Velocity[Z]              1.5657          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4412          4.3406          4.3632
v  Pressure                 -36.38          360.04          87.641          169.85
v  r11                   0.0010624        0.081865        0.013077        0.018287
v  r22                   0.0011164          0.0826        0.013357        0.018647
v  r33                    0.001645         0.17433        0.027256        0.037209
v  r12                   -0.010662         0.01361     -0.00023388     -0.00030934
v  r13                   -0.045509        0.052778       9.339e-05        0.001014
v  r23                   -0.046723        0.051175      3.0607e-05      0.00057467
v  epsilon                0.069682          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9933e-05       0.0099174      0.00092537       0.0017429
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2794         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8794         0.71352         0.85284


 TIME FOR THE TIME STEP            11197:        0.67123E+02

===============================================================


 INSTANT    0.111980000E-01   TIME STEP NUMBER           11198
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209911674E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195969941E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267111499E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.202219901E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.759429262E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81333E-03   0.45033E-02 0.19876E+01 
c  Velocity[X]                                      0.13665E-03 
c  Velocity[Y]                                      0.12761E-03 
c  Velocity[Z]                                      0.42390E-02 
c  Pressure     0.36133E-04     133   0.91973E-02   0.25485E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.62915E-08   0.16603E-08 0.99084E-01 
c  r22          0.10853E-01      13   0.51527E-08   0.18260E-08 0.10038E+00 
c  r33          0.21862E-01      15   0.57382E-08   0.12545E-07 0.12613E+00 
c  r12          0.93880E-03      18   0.65010E-08   0.30331E-09 0.60741E+00 
c  r13          0.46679E-02      19   0.58375E-08   0.14863E-08 0.19838E+00 
c  r23          0.39980E-02      18   0.69306E-08   0.13017E-08 0.19839E+00 
c  epsilon      0.10969E+02      11   0.36126E-08   0.10114E-01 0.16723E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.83646E-02 0.43113E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63376         0.61368       0.0052572       0.0015074
v  Velocity[Y]            -0.57352         0.54396       0.0030785      0.00087217
v  Velocity[Z]              1.5658          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4412          4.3406          4.3632
v  Pressure                -36.444          360.03           87.68          169.86
v  r11                   0.0010624        0.081859        0.013077        0.018287
v  r22                   0.0011164        0.082599        0.013357        0.018647
v  r33                    0.001645         0.17435        0.027256        0.037209
v  r12                   -0.010665        0.013601     -0.00023388     -0.00030934
v  r13                   -0.045506        0.052777       9.339e-05        0.001014
v  r23                   -0.046722        0.051165      3.0607e-05      0.00057467
v  epsilon                0.069683          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099174      0.00092537       0.0017429
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb               0.00179          5.2796         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8796         0.71352         0.85284


 TIME FOR THE TIME STEP            11198:        0.66604E+02

===============================================================


 INSTANT    0.111990000E-01   TIME STEP NUMBER           11199
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.330880395E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.456531785E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.205575812E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935027E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.155608017E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153219156E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81283E-03   0.45140E-02 0.19907E+01 
c  Velocity[X]                                      0.13776E-03 
c  Velocity[Y]                                      0.12825E-03 
c  Velocity[Z]                                      0.42480E-02 
c  Pressure     0.35914E-04     134   0.91469E-02   0.25331E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.65399E-08   0.16278E-08 0.98796E-01 
c  r22          0.10853E-01      13   0.52985E-08   0.18464E-08 0.10107E+00 
c  r33          0.21862E-01      15   0.64232E-08   0.12537E-07 0.12670E+00 
c  r12          0.93880E-03      18   0.69559E-08   0.30104E-09 0.60595E+00 
c  r13          0.46679E-02      19   0.62824E-08   0.14995E-08 0.19913E+00 
c  r23          0.39980E-02      19   0.53273E-08   0.12913E-08 0.19813E+00 
c  epsilon      0.10969E+02      11   0.36623E-08   0.99218E-02 0.16523E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.84625E-02 0.43425E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63365         0.61364       0.0052572       0.0015074
v  Velocity[Y]            -0.57349         0.54407       0.0030784      0.00087218
v  Velocity[Z]              1.5657          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4412          4.3406          4.3632
v  Pressure                -36.416          360.03          87.639          169.85
v  r11                   0.0010624        0.081859        0.013077        0.018287
v  r22                   0.0011164        0.082599        0.013357        0.018647
v  r33                    0.001645         0.17437        0.027256        0.037209
v  r12                   -0.010666          0.0136     -0.00023388     -0.00030934
v  r13                   -0.045506        0.052778       9.339e-05        0.001014
v  r23                   -0.046721         0.05119      3.0608e-05      0.00057467
v  epsilon                0.069684          271.26          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099176      0.00092537       0.0017429
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2796         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8796         0.71352         0.85284


 TIME FOR THE TIME STEP            11199:        0.66847E+02

===============================================================


 INSTANT    0.112000000E-01   TIME STEP NUMBER           11200
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.123789070E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.222151678E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.247668264E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200389510E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.406419585E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81326E-03   0.44699E-02 0.19779E+01 
c  Velocity[X]                                      0.13707E-03 
c  Velocity[Y]                                      0.12619E-03 
c  Velocity[Z]                                      0.42066E-02 
c  Pressure     0.36219E-04     132   0.92203E-02   0.25546E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60560E-08   0.16259E-08 0.98869E-01 
c  r22          0.10853E-01      13   0.53101E-08   0.18206E-08 0.10053E+00 
c  r33          0.21862E-01      15   0.56116E-08   0.12406E-07 0.12624E+00 
c  r12          0.93880E-03      18   0.63102E-08   0.29956E-09 0.60451E+00 
c  r13          0.46679E-02      19   0.56301E-08   0.14815E-08 0.19899E+00 
c  r23          0.39980E-02      19   0.54665E-08   0.12493E-08 0.19641E+00 
c  epsilon      0.10969E+02      11   0.33828E-08   0.98419E-02 0.16627E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.83819E-02 0.43195E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369         0.61367       0.0052572       0.0015073
v  Velocity[Y]             -0.5734         0.54422       0.0030784      0.00087212
v  Velocity[Z]              1.5657          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4412          4.3406          4.3632
v  Pressure                 -36.44          360.01          87.646          169.84
v  r11                   0.0010624        0.081863        0.013077        0.018287
v  r22                   0.0011164        0.082598        0.013357        0.018647
v  r33                    0.001645         0.17439        0.027256        0.037209
v  r12                   -0.010665        0.013601     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052778      9.3391e-05        0.001014
v  r23                    -0.04672        0.051186      3.0608e-05      0.00057467
v  epsilon                0.069685          271.27          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9929e-05       0.0099178      0.00092537       0.0017429
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2793         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8793         0.71352         0.85284


 TIME FOR THE TIME STEP            11200:        0.65757E+02

===============================================================


 INSTANT    0.112010000E-01   TIME STEP NUMBER           11201
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.351440953E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237210398E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166720987E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.960410604E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.534903754E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81211E-03   0.45143E-02 0.19897E+01 
c  Velocity[X]                                      0.13677E-03 
c  Velocity[Y]                                      0.12818E-03 
c  Velocity[Z]                                      0.42493E-02 
c  Pressure     0.36367E-04     133   0.92533E-02   0.25650E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60445E-08   0.16369E-08 0.99068E-01 
c  r22          0.10853E-01      13   0.51768E-08   0.18256E-08 0.10055E+00 
c  r33          0.21862E-01      15   0.61257E-08   0.12510E-07 0.12663E+00 
c  r12          0.93880E-03      18   0.68303E-08   0.29708E-09 0.60163E+00 
c  r13          0.46679E-02      19   0.74616E-08   0.14938E-08 0.19910E+00 
c  r23          0.39980E-02      18   0.67312E-08   0.12902E-08 0.19820E+00 
c  epsilon      0.10969E+02      11   0.34122E-08   0.10023E-01 0.16721E+00 
c  TempC        0.25716E+06      16   0.15173E-04   0.83606E-02 0.43180E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361          0.6137       0.0052572       0.0015074
v  Velocity[Y]            -0.57342         0.54387       0.0030784      0.00087213
v  Velocity[Z]               1.566          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5798          5.4412          4.3406          4.3632
v  Pressure                -36.417          360.03          87.644          169.85
v  r11                   0.0010624        0.081863        0.013077        0.018287
v  r22                   0.0011164        0.082597        0.013357        0.018647
v  r33                    0.001645         0.17441        0.027256        0.037209
v  r12                   -0.010663        0.013601     -0.00023388     -0.00030934
v  r13                   -0.045507         0.05278      9.3392e-05        0.001014
v  r23                    -0.04672         0.05118      3.0608e-05      0.00057467
v  epsilon                0.069686          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099179      0.00092537       0.0017429
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2783         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71352         0.85284


 TIME FOR THE TIME STEP            11201:        0.66172E+02

===============================================================


 INSTANT    0.112020000E-01   TIME STEP NUMBER           11202
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.356726476E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.372497242E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.816015635E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.885617052E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.468329525E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81310E-03   0.45187E-02 0.19910E+01 
c  Velocity[X]                                      0.13690E-03 
c  Velocity[Y]                                      0.12813E-03 
c  Velocity[Z]                                      0.42537E-02 
c  Pressure     0.36373E-04     132   0.92671E-02   0.25655E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59512E-08   0.16166E-08 0.98599E-01 
c  r22          0.10853E-01      13   0.54148E-08   0.18380E-08 0.10106E+00 
c  r33          0.21862E-01      15   0.68508E-08   0.12454E-07 0.12634E+00 
c  r12          0.93880E-03      18   0.61393E-08   0.30186E-09 0.60683E+00 
c  r13          0.46679E-02      20   0.60925E-08   0.15175E-08 0.20023E+00 
c  r23          0.39980E-02      18   0.67026E-08   0.12659E-08 0.19637E+00 
c  epsilon      0.10969E+02      11   0.34945E-08   0.99251E-02 0.16627E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.84099E-02 0.43241E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61373       0.0052572       0.0015074
v  Velocity[Y]            -0.57326         0.54393       0.0030784      0.00087217
v  Velocity[Z]              1.5658          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4412          4.3406          4.3632
v  Pressure                -36.457          360.06          87.683          169.89
v  r11                   0.0010624        0.081868        0.013077        0.018287
v  r22                   0.0011164        0.082596        0.013357        0.018647
v  r33                    0.001645         0.17442        0.027256        0.037209
v  r12                   -0.010662        0.013597     -0.00023388     -0.00030934
v  r13                   -0.045506        0.052779      9.3393e-05        0.001014
v  r23                   -0.046719        0.051207      3.0608e-05      0.00057467
v  epsilon                0.069688          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099177      0.00092537       0.0017429
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017901           5.278         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            11202:        0.66738E+02

===============================================================


 INSTANT    0.112030000E-01   TIME STEP NUMBER           11203
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.208996451E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.393144923E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.590628997E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935014E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.256767757E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.146042295E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81320E-03   0.44869E-02 0.19811E+01 
c  Velocity[X]                                      0.13740E-03 
c  Velocity[Y]                                      0.12709E-03 
c  Velocity[Z]                                      0.42224E-02 
c  Pressure     0.36189E-04     132   0.92086E-02   0.25524E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53945E-08   0.16561E-08 0.99327E-01 
c  r22          0.10853E-01      13   0.53155E-08   0.18177E-08 0.10035E+00 
c  r33          0.21862E-01      15   0.68669E-08   0.12555E-07 0.12666E+00 
c  r12          0.93880E-03      18   0.61497E-08   0.30235E-09 0.60834E+00 
c  r13          0.46679E-02      19   0.59197E-08   0.14917E-08 0.19901E+00 
c  r23          0.39980E-02      19   0.55200E-08   0.12770E-08 0.19798E+00 
c  epsilon      0.10969E+02      11   0.34407E-08   0.10277E-01 0.17239E+00 
c  TempC        0.25716E+06      16   0.15119E-04   0.83630E-02 0.43150E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61372       0.0052572       0.0015074
v  Velocity[Y]             -0.5733         0.54401       0.0030784      0.00087215
v  Velocity[Z]              1.5658          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4412          4.3406          4.3632
v  Pressure                -36.412          360.04          87.637          169.86
v  r11                   0.0010624        0.081871        0.013077        0.018287
v  r22                   0.0011164        0.082593        0.013357        0.018647
v  r33                    0.001645         0.17438        0.027256        0.037209
v  r12                   -0.010661        0.013595     -0.00023388     -0.00030934
v  r13                   -0.045508         0.05278      9.3393e-05        0.001014
v  r23                    -0.04672          0.0512      3.0607e-05      0.00057467
v  epsilon                0.069689          271.26          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099176      0.00092537       0.0017429
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017901          5.2774         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8774         0.71352         0.85284


 TIME FOR THE TIME STEP            11203:        0.68269E+02

===============================================================


 INSTANT    0.112040000E-01   TIME STEP NUMBER           11204
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.513304345E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.156854611E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934907E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.496646702E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.277497542E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934921E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.896595531E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81315E-03   0.44766E-02 0.19801E+01 
c  Velocity[X]                                      0.13600E-03 
c  Velocity[Y]                                      0.12708E-03 
c  Velocity[Z]                                      0.42135E-02 
c  Pressure     0.36229E-04     133   0.92201E-02   0.25554E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56640E-08   0.15939E-08 0.97940E-01 
c  r22          0.10853E-01      13   0.56875E-08   0.17984E-08 0.99931E-01 
c  r33          0.21862E-01      15   0.67953E-08   0.12304E-07 0.12565E+00 
c  r12          0.93880E-03      18   0.67846E-08   0.29742E-09 0.60726E+00 
c  r13          0.46679E-02      19   0.57645E-08   0.14984E-08 0.19880E+00 
c  r23          0.39980E-02      19   0.53490E-08   0.12535E-08 0.19569E+00 
c  epsilon      0.10969E+02      11   0.34789E-08   0.97431E-02 0.16500E+00 
c  TempC        0.25716E+06      16   0.15203E-04   0.83944E-02 0.43250E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364          0.6137       0.0052572       0.0015074
v  Velocity[Y]            -0.57335         0.54417       0.0030784      0.00087213
v  Velocity[Z]              1.5656          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4412          4.3406          4.3632
v  Pressure                -36.435          360.04          87.669          169.87
v  r11                   0.0010624        0.081879        0.013077        0.018287
v  r22                   0.0011164        0.082594        0.013357        0.018647
v  r33                    0.001645         0.17433        0.027256        0.037209
v  r12                   -0.010662        0.013596     -0.00023388     -0.00030934
v  r13                   -0.045506         0.05278      9.3393e-05        0.001014
v  r23                   -0.046719        0.051181      3.0608e-05      0.00057467
v  epsilon                 0.06969          271.27          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099175      0.00092537       0.0017429
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2772         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85284


 TIME FOR THE TIME STEP            11204:        0.66633E+02

===============================================================


 INSTANT    0.112050000E-01   TIME STEP NUMBER           11205
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.258717780E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.168297197E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.267562679E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935011E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.600205607E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.260135743E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81139E-03   0.45326E-02 0.19927E+01 
c  Velocity[X]                                      0.13825E-03 
c  Velocity[Y]                                      0.12795E-03 
c  Velocity[Z]                                      0.42664E-02 
c  Pressure     0.36118E-04     133   0.91963E-02   0.25474E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.63767E-08   0.15874E-08 0.98120E-01 
c  r22          0.10853E-01      13   0.58466E-08   0.17788E-08 0.99859E-01 
c  r33          0.21862E-01      15   0.56801E-08   0.12132E-07 0.12554E+00 
c  r12          0.93880E-03      18   0.68561E-08   0.29073E-09 0.60074E+00 
c  r13          0.46679E-02      19   0.62155E-08   0.14513E-08 0.19750E+00 
c  r23          0.39980E-02      18   0.64837E-08   0.12419E-08 0.19609E+00 
c  epsilon      0.10969E+02      11   0.33317E-08   0.93703E-02 0.16073E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.84299E-02 0.43318E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61369       0.0052571       0.0015073
v  Velocity[Y]             -0.5733         0.54401       0.0030784      0.00087213
v  Velocity[Z]              1.5657          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4412          4.3406          4.3632
v  Pressure                -36.433          360.04           87.66          169.86
v  r11                   0.0010624        0.081881        0.013077        0.018287
v  r22                   0.0011164        0.082596        0.013357        0.018647
v  r33                    0.001645         0.17432        0.027256        0.037209
v  r12                   -0.010662        0.013588     -0.00023388     -0.00030934
v  r13                   -0.045506        0.052777      9.3394e-05        0.001014
v  r23                    -0.04672        0.051205      3.0608e-05      0.00057467
v  epsilon                0.069691          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05       0.0099175      0.00092537       0.0017429
v  CourantNb               0.44219             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2769         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71353         0.85284


 TIME FOR THE TIME STEP            11205:        0.65645E+02

===============================================================


 INSTANT    0.112060000E-01   TIME STEP NUMBER           11206
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.463666111E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.154209804E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.219983777E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150233668E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201174307E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      45   0.81402E-03   0.44981E-02 0.19859E+01 
c  Velocity[X]                                      0.13702E-03 
c  Velocity[Y]                                      0.12710E-03 
c  Velocity[Z]                                      0.42339E-02 
c  Pressure     0.36363E-04     133   0.92522E-02   0.25648E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.68491E-08   0.16140E-08 0.98141E-01 
c  r22          0.10853E-01      13   0.55869E-08   0.18071E-08 0.10013E+00 
c  r33          0.21862E-01      15   0.55865E-08   0.12483E-07 0.12619E+00 
c  r12          0.93880E-03      18   0.55737E-08   0.29576E-09 0.60416E+00 
c  r13          0.46679E-02      19   0.72023E-08   0.14992E-08 0.19915E+00 
c  r23          0.39980E-02      18   0.68305E-08   0.12765E-08 0.19689E+00 
c  epsilon      0.10969E+02      11   0.34668E-08   0.10102E-01 0.16639E+00 
c  TempC        0.25716E+06      16   0.15166E-04   0.83062E-02 0.42992E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63363         0.61372       0.0052572       0.0015074
v  Velocity[Y]            -0.57324         0.54397       0.0030784      0.00087216
v  Velocity[Z]              1.5659          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4412          4.3406          4.3632
v  Pressure                -36.454          359.99          87.635          169.83
v  r11                   0.0010624        0.081883        0.013077        0.018287
v  r22                   0.0011164        0.082598        0.013357        0.018647
v  r33                    0.001645         0.17433        0.027256        0.037209
v  r12                    -0.01066        0.013587     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052777      9.3394e-05        0.001014
v  r23                   -0.046719        0.051192      3.0609e-05      0.00057467
v  epsilon                0.069692          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9932e-05       0.0099175      0.00092538       0.0017429
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2767         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767         0.71352         0.85284


 TIME FOR THE TIME STEP            11206:        0.66790E+02

===============================================================


 INSTANT    0.112070000E-01   TIME STEP NUMBER           11207
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.946542307E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.198966391E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.382774806E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171184820E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.257522249E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81232E-03   0.44995E-02 0.19865E+01 
c  Velocity[X]                                      0.13726E-03 
c  Velocity[Y]                                      0.12779E-03 
c  Velocity[Z]                                      0.42344E-02 
c  Pressure     0.36300E-04     132   0.92419E-02   0.25602E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.62753E-08   0.16245E-08 0.98392E-01 
c  r22          0.10853E-01      13   0.52742E-08   0.18185E-08 0.10058E+00 
c  r33          0.21862E-01      15   0.55107E-08   0.12468E-07 0.12626E+00 
c  r12          0.93880E-03      18   0.55046E-08   0.29977E-09 0.60671E+00 
c  r13          0.46679E-02      20   0.58686E-08   0.14911E-08 0.19922E+00 
c  r23          0.39980E-02      19   0.57564E-08   0.12647E-08 0.19628E+00 
c  epsilon      0.10969E+02      11   0.34216E-08   0.10082E-01 0.16716E+00 
c  TempC        0.25716E+06      16   0.15139E-04   0.84232E-02 0.43268E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361         0.61373       0.0052572       0.0015074
v  Velocity[Y]            -0.57337         0.54405       0.0030784      0.00087218
v  Velocity[Z]              1.5658          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4412          4.3406          4.3632
v  Pressure                -36.413          360.04          87.657          169.87
v  r11                   0.0010624        0.081877        0.013077        0.018287
v  r22                   0.0011164        0.082597        0.013357        0.018647
v  r33                    0.001645         0.17435        0.027256        0.037209
v  r12                   -0.010662         0.01359     -0.00023388     -0.00030934
v  r13                   -0.045507        0.052775      9.3395e-05        0.001014
v  r23                   -0.046718        0.051181      3.0609e-05      0.00057467
v  epsilon                0.069694          271.27          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9935e-05       0.0099175      0.00092538       0.0017429
v  CourantNb               0.44218             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2769         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71352         0.85284


 TIME FOR THE TIME STEP            11207:        0.66093E+02

===============================================================


 INSTANT    0.112080000E-01   TIME STEP NUMBER           11208
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.211115534E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.950009955E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934922E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.861847849E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.269639370E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.302542453E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69760E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81350E-03   0.44901E-02 0.19826E+01 
c  Velocity[X]                                      0.13689E-03 
c  Velocity[Y]                                      0.12834E-03 
c  Velocity[Z]                                      0.42249E-02 
c  Pressure     0.36319E-04     133   0.92426E-02   0.25617E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61469E-08   0.16359E-08 0.98955E-01 
c  r22          0.10853E-01      13   0.50857E-08   0.18036E-08 0.10053E+00 
c  r33          0.21862E-01      15   0.56975E-08   0.12376E-07 0.12629E+00 
c  r12          0.93880E-03      18   0.55274E-08   0.31718E-09 0.61624E+00 
c  r13          0.46679E-02      19   0.65968E-08   0.14912E-08 0.19933E+00 
c  r23          0.39980E-02      19   0.56423E-08   0.12927E-08 0.19848E+00 
c  epsilon      0.10969E+02      11   0.33805E-08   0.96828E-02 0.16373E+00 
c  TempC        0.25716E+06      16   0.15188E-04   0.84618E-02 0.43423E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6336         0.61371       0.0052572       0.0015074
v  Velocity[Y]            -0.57313         0.54415       0.0030783      0.00087215
v  Velocity[Z]              1.5658          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4412          4.3406          4.3632
v  Pressure                 -36.47          360.05           87.67          169.87
v  r11                   0.0010624        0.081874        0.013077        0.018287
v  r22                   0.0011164        0.082599        0.013357        0.018647
v  r33                    0.001645         0.17437        0.027256        0.037209
v  r12                   -0.010662        0.013585     -0.00023388     -0.00030934
v  r13                   -0.045505        0.052777      9.3394e-05       0.0010139
v  r23                   -0.046717        0.051173      3.0609e-05      0.00057467
v  epsilon                0.069695          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9936e-05       0.0099176      0.00092538       0.0017429
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017902          5.2768         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71352         0.85284


 TIME FOR THE TIME STEP            11208:        0.66330E+02

===============================================================


 INSTANT    0.112090000E-01   TIME STEP NUMBER           11209
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.746989880E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.113936020E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.775332770E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.426736691E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.907632846E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81262E-03   0.44982E-02 0.19844E+01 
c  Velocity[X]                                      0.13619E-03 
c  Velocity[Y]                                      0.12715E-03 
c  Velocity[Z]                                      0.42349E-02 
c  Pressure     0.36297E-04     132   0.92379E-02   0.25601E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56672E-08   0.16461E-08 0.99731E-01 
c  r22          0.10853E-01      13   0.49562E-08   0.18308E-08 0.10122E+00 
c  r33          0.21862E-01      15   0.51972E-08   0.12540E-07 0.12746E+00 
c  r12          0.93880E-03      18   0.59296E-08   0.29916E-09 0.60983E+00 
c  r13          0.46679E-02      19   0.54560E-08   0.14905E-08 0.20046E+00 
c  r23          0.39980E-02      18   0.70236E-08   0.12955E-08 0.20039E+00 
c  epsilon      0.10969E+02      11   0.33438E-08   0.10082E-01 0.17054E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.83960E-02 0.43209E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63365          0.6137       0.0052572       0.0015074
v  Velocity[Y]            -0.57322         0.54393       0.0030783      0.00087214
v  Velocity[Z]              1.5657          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4412          4.3406          4.3632
v  Pressure                -36.405          359.96          87.593          169.79
v  r11                   0.0010624        0.081875        0.013077        0.018287
v  r22                   0.0011164        0.082595        0.013357        0.018647
v  r33                    0.001645         0.17439        0.027256        0.037209
v  r12                   -0.010668        0.013588     -0.00023388     -0.00030934
v  r13                   -0.045509        0.052775      9.3394e-05       0.0010139
v  r23                   -0.046717        0.051204      3.0609e-05      0.00057467
v  epsilon                0.069696          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9938e-05       0.0099176      0.00092538       0.0017429
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2772         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85284


 TIME FOR THE TIME STEP            11209:        0.67204E+02

===============================================================


 INSTANT    0.112100000E-01   TIME STEP NUMBER           11210
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237001957E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.290101973E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934920E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.240684333E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.391641603E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.195354629E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81339E-03   0.45022E-02 0.19885E+01 
c  Velocity[X]                                      0.13733E-03 
c  Velocity[Y]                                      0.12734E-03 
c  Velocity[Z]                                      0.42375E-02 
c  Pressure     0.36427E-04     133   0.92734E-02   0.25692E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53321E-08   0.16109E-08 0.98537E-01 
c  r22          0.10853E-01      13   0.50300E-08   0.17784E-08 0.10009E+00 
c  r33          0.21862E-01      14   0.70934E-08   0.12199E-07 0.12560E+00 
c  r12          0.93880E-03      18   0.57126E-08   0.28930E-09 0.60122E+00 
c  r13          0.46679E-02      18   0.67962E-08   0.14520E-08 0.19791E+00 
c  r23          0.39980E-02      19   0.53081E-08   0.12625E-08 0.19681E+00 
c  epsilon      0.10969E+02      11   0.33375E-08   0.93653E-02 0.16113E+00 
c  TempC        0.25716E+06      16   0.15140E-04   0.83845E-02 0.43190E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61373       0.0052572       0.0015074
v  Velocity[Y]            -0.57315         0.54406       0.0030783      0.00087214
v  Velocity[Z]              1.5657          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4412          4.3406          4.3632
v  Pressure                -36.421          360.02          87.662          169.85
v  r11                   0.0010624         0.08188        0.013077        0.018287
v  r22                   0.0011164        0.082596        0.013357        0.018647
v  r33                    0.001645          0.1744        0.027256        0.037209
v  r12                   -0.010668        0.013593     -0.00023388     -0.00030934
v  r13                   -0.045506        0.052773      9.3394e-05       0.0010139
v  r23                   -0.046716        0.051195      3.0609e-05      0.00057467
v  epsilon                0.069697          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9939e-05       0.0099176      0.00092538       0.0017429
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2769         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71352         0.85284


 TIME FOR THE TIME STEP            11210:        0.67817E+02

===============================================================


 INSTANT    0.112110000E-01   TIME STEP NUMBER           11211
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.346283045E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.189905409E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.465873488E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.934442812E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.223807796E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81291E-03   0.45157E-02 0.19907E+01 
c  Velocity[X]                                      0.13754E-03 
c  Velocity[Y]                                      0.12776E-03 
c  Velocity[Z]                                      0.42504E-02 
c  Pressure     0.36457E-04     133   0.92776E-02   0.25714E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51769E-08   0.16083E-08 0.98148E-01 
c  r22          0.10853E-01      13   0.50018E-08   0.18002E-08 0.10042E+00 
c  r33          0.21862E-01      15   0.52252E-08   0.12347E-07 0.12588E+00 
c  r12          0.93880E-03      18   0.52262E-08   0.29535E-09 0.60298E+00 
c  r13          0.46679E-02      18   0.70297E-08   0.14767E-08 0.19854E+00 
c  r23          0.39980E-02      19   0.58971E-08   0.12715E-08 0.19660E+00 
c  epsilon      0.10969E+02      11   0.34044E-08   0.96303E-02 0.16234E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.83917E-02 0.43299E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63371         0.61369       0.0052572       0.0015074
v  Velocity[Y]            -0.57317         0.54403       0.0030783      0.00087215
v  Velocity[Z]              1.5656          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4412          4.3406          4.3632
v  Pressure                -36.418          360.08           87.68           169.9
v  r11                   0.0010624         0.08188        0.013077        0.018287
v  r22                   0.0011164        0.082596        0.013357        0.018647
v  r33                    0.001645         0.17436        0.027256        0.037209
v  r12                   -0.010667        0.013586     -0.00023388     -0.00030934
v  r13                   -0.045505         0.05277      9.3394e-05       0.0010139
v  r23                   -0.046715        0.051191      3.0609e-05      0.00057467
v  epsilon                0.069699          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9941e-05       0.0099177      0.00092538       0.0017429
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71353         0.85284


 TIME FOR THE TIME STEP            11211:        0.67276E+02

===============================================================


 INSTANT    0.112120000E-01   TIME STEP NUMBER           11212
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.476298274E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.250419333E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.268444766E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.189056172E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.154239694E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81337E-03   0.44926E-02 0.19845E+01 
c  Velocity[X]                                      0.13660E-03 
c  Velocity[Y]                                      0.12681E-03 
c  Velocity[Z]                                      0.42292E-02 
c  Pressure     0.36510E-04     133   0.92906E-02   0.25752E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51132E-08   0.16279E-08 0.98530E-01 
c  r22          0.10853E-01      13   0.48025E-08   0.18334E-08 0.10108E+00 
c  r33          0.21862E-01      15   0.53807E-08   0.12544E-07 0.12653E+00 
c  r12          0.93880E-03      18   0.53820E-08   0.29480E-09 0.60511E+00 
c  r13          0.46679E-02      19   0.62114E-08   0.14897E-08 0.19901E+00 
c  r23          0.39980E-02      18   0.69611E-08   0.12643E-08 0.19640E+00 
c  epsilon      0.10969E+02      11   0.34354E-08   0.99017E-02 0.16581E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.83482E-02 0.43092E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63372         0.61371       0.0052572       0.0015074
v  Velocity[Y]            -0.57315         0.54406       0.0030783      0.00087214
v  Velocity[Z]              1.5657          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4412          4.3406          4.3632
v  Pressure                -36.445          360.01          87.642          169.85
v  r11                   0.0010624        0.081881        0.013077        0.018287
v  r22                   0.0011164        0.082595        0.013357        0.018647
v  r33                   0.0016451         0.17432        0.027256        0.037209
v  r12                   -0.010665        0.013584     -0.00023388     -0.00030934
v  r13                   -0.045507        0.052769      9.3395e-05       0.0010139
v  r23                   -0.046715        0.051177       3.061e-05      0.00057467
v  epsilon                  0.0697          271.26          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9941e-05       0.0099178      0.00092538       0.0017429
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017903          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71353         0.85284


 TIME FOR THE TIME STEP            11212:        0.66482E+02

===============================================================


 INSTANT    0.112130000E-01   TIME STEP NUMBER           11213
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.238640979E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.279634376E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.104877350E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.261069516E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.316220524E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81285E-03   0.45252E-02 0.19889E+01 
c  Velocity[X]                                      0.13668E-03 
c  Velocity[Y]                                      0.12729E-03 
c  Velocity[Z]                                      0.42612E-02 
c  Pressure     0.36086E-04     133   0.91842E-02   0.25452E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.49492E-08   0.16412E-08 0.98875E-01 
c  r22          0.10853E-01      13   0.51661E-08   0.18447E-08 0.10103E+00 
c  r33          0.21862E-01      14   0.62914E-08   0.12687E-07 0.12677E+00 
c  r12          0.93880E-03      18   0.56828E-08   0.30583E-09 0.60780E+00 
c  r13          0.46679E-02      19   0.59724E-08   0.15172E-08 0.20015E+00 
c  r23          0.39980E-02      18   0.69666E-08   0.12830E-08 0.19733E+00 
c  epsilon      0.10969E+02      11   0.33665E-08   0.10227E-01 0.16790E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.83977E-02 0.43196E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61367       0.0052572       0.0015074
v  Velocity[Y]             -0.5733         0.54385       0.0030783      0.00087213
v  Velocity[Z]              1.5658          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4412          4.3406          4.3632
v  Pressure                -36.428          360.02           87.65          169.86
v  r11                   0.0010624        0.081879        0.013077        0.018287
v  r22                   0.0011164        0.082594        0.013357        0.018647
v  r33                   0.0016451         0.17431        0.027256        0.037209
v  r12                   -0.010663        0.013587     -0.00023388     -0.00030934
v  r13                   -0.045507         0.05277      9.3395e-05       0.0010139
v  r23                   -0.046715          0.0512       3.061e-05      0.00057467
v  epsilon                0.069701          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9944e-05       0.0099179      0.00092538       0.0017429
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017904          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71353         0.85284


 TIME FOR THE TIME STEP            11213:        0.65983E+02

===============================================================


 INSTANT    0.112140000E-01   TIME STEP NUMBER           11214
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.222069555E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.179872609E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934919E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.421981836E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.365892286E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.357337199E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81293E-03   0.45355E-02 0.19923E+01 
c  Velocity[X]                                      0.13791E-03 
c  Velocity[Y]                                      0.12805E-03 
c  Velocity[Z]                                      0.42695E-02 
c  Pressure     0.36402E-04     134   0.92682E-02   0.25676E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.48990E-08   0.16376E-08 0.98549E-01 
c  r22          0.10853E-01      13   0.49117E-08   0.18082E-08 0.10039E+00 
c  r33          0.21862E-01      15   0.56089E-08   0.12399E-07 0.12592E+00 
c  r12          0.93880E-03      18   0.57239E-08   0.29665E-09 0.60424E+00 
c  r13          0.46679E-02      19   0.62965E-08   0.14711E-08 0.19814E+00 
c  r23          0.39980E-02      19   0.59454E-08   0.12641E-08 0.19645E+00 
c  epsilon      0.10969E+02      11   0.33671E-08   0.95631E-02 0.16216E+00 
c  TempC        0.25716E+06      16   0.15177E-04   0.84511E-02 0.43314E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63354         0.61372       0.0052572       0.0015075
v  Velocity[Y]            -0.57329          0.5439       0.0030783      0.00087216
v  Velocity[Z]              1.5658          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4412          4.3406          4.3632
v  Pressure                -36.478             360          87.653          169.84
v  r11                   0.0010624        0.081884        0.013077        0.018287
v  r22                   0.0011164        0.082593        0.013357        0.018647
v  r33                   0.0016451         0.17433        0.027256        0.037209
v  r12                   -0.010662        0.013584     -0.00023388     -0.00030934
v  r13                   -0.045505        0.052772      9.3395e-05       0.0010139
v  r23                   -0.046715        0.051188       3.061e-05      0.00057467
v  epsilon                0.069702          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9943e-05       0.0099179      0.00092538       0.0017429
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017904          5.2778         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71353         0.85284


 TIME FOR THE TIME STEP            11214:        0.64357E+02

===============================================================


 INSTANT    0.112150000E-01   TIME STEP NUMBER           11215
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.362498269E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.144343397E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.417462578E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935015E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.155027503E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232851046E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81257E-03   0.45134E-02 0.19887E+01 
c  Velocity[X]                                      0.13758E-03 
c  Velocity[Y]                                      0.12780E-03 
c  Velocity[Z]                                      0.42480E-02 
c  Pressure     0.36373E-04     132   0.92610E-02   0.25654E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54295E-08   0.16533E-08 0.99199E-01 
c  r22          0.10853E-01      13   0.50142E-08   0.18295E-08 0.10059E+00 
c  r33          0.21862E-01      15   0.54559E-08   0.12683E-07 0.12727E+00 
c  r12          0.93880E-03      18   0.57403E-08   0.29764E-09 0.60606E+00 
c  r13          0.46679E-02      19   0.54793E-08   0.14988E-08 0.19903E+00 
c  r23          0.39980E-02      18   0.70426E-08   0.12894E-08 0.19910E+00 
c  epsilon      0.10969E+02      11   0.32500E-08   0.10317E-01 0.17223E+00 
c  TempC        0.25716E+06      16   0.15114E-04   0.84015E-02 0.43226E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61371       0.0052573       0.0015075
v  Velocity[Y]            -0.57342         0.54405       0.0030783      0.00087211
v  Velocity[Z]              1.5658          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4412          4.3406          4.3632
v  Pressure                -36.403          359.99          87.628          169.83
v  r11                   0.0010624        0.081882        0.013077        0.018287
v  r22                   0.0011164        0.082591        0.013357        0.018647
v  r33                   0.0016451         0.17435        0.027256        0.037209
v  r12                   -0.010661        0.013587     -0.00023388     -0.00030934
v  r13                   -0.045507        0.052774      9.3395e-05       0.0010139
v  r23                   -0.046715        0.051176       3.061e-05      0.00057467
v  epsilon                0.069704          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9944e-05        0.009918      0.00092538       0.0017429
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017904          5.2781         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71353         0.85284


 TIME FOR THE TIME STEP            11215:        0.66960E+02

===============================================================


 INSTANT    0.112160000E-01   TIME STEP NUMBER           11216
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.185730454E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.316181625E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.278392166E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.164820805E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.338265741E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81298E-03   0.44777E-02 0.19821E+01 
c  Velocity[X]                                      0.13700E-03 
c  Velocity[Y]                                      0.12733E-03 
c  Velocity[Z]                                      0.42134E-02 
c  Pressure     0.36225E-04     132   0.92195E-02   0.25551E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.50595E-08   0.16626E-08 0.98995E-01 
c  r22          0.10853E-01      13   0.51278E-08   0.18366E-08 0.10129E+00 
c  r33          0.21862E-01      15   0.58586E-08   0.12637E-07 0.12702E+00 
c  r12          0.93881E-03      18   0.59553E-08   0.30953E-09 0.61274E+00 
c  r13          0.46679E-02      19   0.58608E-08   0.14857E-08 0.19902E+00 
c  r23          0.39980E-02      19   0.56957E-08   0.12926E-08 0.19821E+00 
c  epsilon      0.10969E+02      11   0.34200E-08   0.10027E-01 0.16796E+00 
c  TempC        0.25716E+06      16   0.15180E-04   0.83542E-02 0.43166E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162017


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6336          0.6137       0.0052573       0.0015075
v  Velocity[Y]            -0.57336         0.54385       0.0030782       0.0008721
v  Velocity[Z]              1.5656          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4412          4.3406          4.3632
v  Pressure                -36.466          360.08          87.688           169.9
v  r11                   0.0010624        0.081878        0.013077        0.018287
v  r22                   0.0011164        0.082595        0.013357        0.018647
v  r33                   0.0016451         0.17437        0.027256        0.037209
v  r12                    -0.01066        0.013594     -0.00023388     -0.00030934
v  r13                   -0.045505        0.052773      9.3395e-05       0.0010139
v  r23                   -0.046715         0.05117      3.0609e-05      0.00057467
v  epsilon                0.069705          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9941e-05        0.009918      0.00092538       0.0017429
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017904          5.2784         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85284


 TIME FOR THE TIME STEP            11216:        0.66897E+02

===============================================================


 INSTANT    0.112170000E-01   TIME STEP NUMBER           11217
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.661949510E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.579310678E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.507789946E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935021E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161100985E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.868080640E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81200E-03   0.45085E-02 0.19875E+01 
c  Velocity[X]                                      0.13710E-03 
c  Velocity[Y]                                      0.12694E-03 
c  Velocity[Z]                                      0.42445E-02 
c  Pressure     0.36095E-04     132   0.91955E-02   0.25459E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53720E-08   0.16201E-08 0.98598E-01 
c  r22          0.10853E-01      13   0.51545E-08   0.18359E-08 0.10125E+00 
c  r33          0.21862E-01      15   0.51912E-08   0.12416E-07 0.12647E+00 
c  r12          0.93881E-03      18   0.60349E-08   0.29307E-09 0.60249E+00 
c  r13          0.46679E-02      19   0.57193E-08   0.14814E-08 0.19893E+00 
c  r23          0.39980E-02      19   0.52134E-08   0.12559E-08 0.19627E+00 
c  epsilon      0.10969E+02      11   0.34093E-08   0.95869E-02 0.16261E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.83992E-02 0.43277E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61366       0.0052573       0.0015075
v  Velocity[Y]            -0.57335         0.54397       0.0030783      0.00087215
v  Velocity[Z]              1.5659          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4412          4.3406          4.3632
v  Pressure                -36.438          359.97          87.612          169.81
v  r11                   0.0010624        0.081875        0.013077        0.018287
v  r22                   0.0011164        0.082597        0.013357        0.018647
v  r33                   0.0016451         0.17439        0.027256        0.037209
v  r12                   -0.010656        0.013591     -0.00023388     -0.00030934
v  r13                   -0.045505         0.05277      9.3395e-05       0.0010139
v  r23                   -0.046715        0.051204       3.061e-05      0.00057467
v  epsilon                0.069706          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9941e-05        0.009918      0.00092538       0.0017429
v  CourantNb               0.44235             0.6         0.59908         0.59839
v  FourierNb             0.0017905           5.278         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            11217:        0.68534E+02

===============================================================


 INSTANT    0.112180000E-01   TIME STEP NUMBER           11218
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.712302444E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.115069358E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.194274976E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.334914139E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294920792E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81416E-03   0.45085E-02 0.19884E+01 
c  Velocity[X]                                      0.13702E-03 
c  Velocity[Y]                                      0.12686E-03 
c  Velocity[Z]                                      0.42446E-02 
c  Pressure     0.36218E-04     132   0.92166E-02   0.25545E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.50734E-08   0.16328E-08 0.98889E-01 
c  r22          0.10853E-01      13   0.50058E-08   0.18056E-08 0.10084E+00 
c  r33          0.21862E-01      14   0.71464E-08   0.12517E-07 0.12703E+00 
c  r12          0.93881E-03      18   0.56953E-08   0.29648E-09 0.60201E+00 
c  r13          0.46679E-02      18   0.62615E-08   0.14773E-08 0.19941E+00 
c  r23          0.39980E-02      18   0.67902E-08   0.12766E-08 0.19772E+00 
c  epsilon      0.10969E+02      11   0.34577E-08   0.98552E-02 0.16564E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.83372E-02 0.43111E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6336         0.61362       0.0052572       0.0015074
v  Velocity[Y]            -0.57334         0.54396       0.0030782      0.00087209
v  Velocity[Z]               1.566          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5798          5.4412          4.3406          4.3632
v  Pressure                -36.458             360          87.638          169.84
v  r11                   0.0010624        0.081875        0.013077        0.018287
v  r22                   0.0011164        0.082597        0.013357        0.018647
v  r33                   0.0016451         0.17441        0.027256        0.037209
v  r12                   -0.010659        0.013586     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052771      9.3395e-05       0.0010139
v  r23                   -0.046715         0.05119       3.061e-05      0.00057467
v  epsilon                0.069708          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9939e-05        0.009918      0.00092538       0.0017429
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017905          5.2778         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71353         0.85284


 TIME FOR THE TIME STEP            11218:        0.69110E+02

===============================================================


 INSTANT    0.112190000E-01   TIME STEP NUMBER           11219
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.135458624E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.336221121E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.722299515E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.189698253E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.211011725E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81169E-03   0.45226E-02 0.19909E+01 
c  Velocity[X]                                      0.13764E-03 
c  Velocity[Y]                                      0.12846E-03 
c  Velocity[Z]                                      0.42565E-02 
c  Pressure     0.36579E-04     132   0.93099E-02   0.25799E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52489E-08   0.16527E-08 0.99281E-01 
c  r22          0.10853E-01      13   0.49307E-08   0.18334E-08 0.10130E+00 
c  r33          0.21862E-01      14   0.70630E-08   0.12653E-07 0.12742E+00 
c  r12          0.93881E-03      18   0.61286E-08   0.30034E-09 0.60475E+00 
c  r13          0.46679E-02      18   0.62782E-08   0.14773E-08 0.19914E+00 
c  r23          0.39980E-02      18   0.70648E-08   0.12782E-08 0.19841E+00 
c  epsilon      0.10969E+02      11   0.33259E-08   0.10168E-01 0.16798E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.84501E-02 0.43290E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63368         0.61357       0.0052572       0.0015075
v  Velocity[Y]            -0.57341           0.544       0.0030783      0.00087212
v  Velocity[Z]               1.566          5.4412          4.3387          4.3625
v  ǁVelocityǁ               1.5798          5.4412          4.3406          4.3632
v  Pressure                -36.441          360.05          87.665          169.88
v  r11                   0.0010625        0.081874        0.013077        0.018287
v  r22                   0.0011164        0.082596        0.013357        0.018647
v  r33                   0.0016451         0.17442        0.027256        0.037209
v  r12                    -0.01066        0.013587     -0.00023388     -0.00030934
v  r13                   -0.045506         0.05277      9.3395e-05       0.0010139
v  r23                   -0.046715        0.051185       3.061e-05      0.00057467
v  epsilon                0.069709          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9937e-05       0.0099179      0.00092538       0.0017429
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017905           5.278         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            11219:        0.69432E+02

===============================================================


 INSTANT    0.112200000E-01   TIME STEP NUMBER           11220
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.476238987E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.254446306E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190448454E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.133507651E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.367135568E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      45   0.81323E-03   0.45109E-02 0.19881E+01 
c  Velocity[X]                                      0.13720E-03 
c  Velocity[Y]                                      0.12836E-03 
c  Velocity[Z]                                      0.42453E-02 
c  Pressure     0.36503E-04     133   0.92974E-02   0.25747E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52089E-08   0.16483E-08 0.99401E-01 
c  r22          0.10853E-01      13   0.49175E-08   0.18893E-08 0.10217E+00 
c  r33          0.21862E-01      14   0.69445E-08   0.12796E-07 0.12771E+00 
c  r12          0.93881E-03      18   0.58140E-08   0.30681E-09 0.60953E+00 
c  r13          0.46679E-02      18   0.63544E-08   0.15458E-08 0.20101E+00 
c  r23          0.39980E-02      19   0.55219E-08   0.12798E-08 0.19832E+00 
c  epsilon      0.10969E+02      11   0.33658E-08   0.10296E-01 0.16872E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.83955E-02 0.43229E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61362       0.0052573       0.0015075
v  Velocity[Y]            -0.57334         0.54409       0.0030782      0.00087211
v  Velocity[Z]               1.566          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5798          5.4413          4.3406          4.3632
v  Pressure                 -36.45          360.08          87.689           169.9
v  r11                   0.0010625        0.081878        0.013077        0.018287
v  r22                   0.0011164        0.082596        0.013357        0.018647
v  r33                   0.0016451         0.17438        0.027256        0.037209
v  r12                   -0.010663        0.013589     -0.00023388     -0.00030934
v  r13                   -0.045504        0.052772      9.3396e-05       0.0010139
v  r23                   -0.046715        0.051215      3.0611e-05      0.00057467
v  epsilon                 0.06971          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9933e-05        0.009918      0.00092538       0.0017429
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017905           5.278         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            11220:        0.68321E+02

===============================================================


 INSTANT    0.112210000E-01   TIME STEP NUMBER           11221
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.201897505E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.768857049E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.123411449E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.132875025E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.263373464E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81262E-03   0.44752E-02 0.19810E+01 
c  Velocity[X]                                      0.13757E-03 
c  Velocity[Y]                                      0.12711E-03 
c  Velocity[Z]                                      0.42105E-02 
c  Pressure     0.36243E-04     132   0.92288E-02   0.25563E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.46684E-08   0.16361E-08 0.99201E-01 
c  r22          0.10853E-01      13   0.47927E-08   0.17839E-08 0.10077E+00 
c  r33          0.21862E-01      15   0.60443E-08   0.12284E-07 0.12656E+00 
c  r12          0.93881E-03      18   0.57919E-08   0.29746E-09 0.60357E+00 
c  r13          0.46679E-02      18   0.67463E-08   0.14730E-08 0.19890E+00 
c  r23          0.39980E-02      19   0.60517E-08   0.12771E-08 0.19905E+00 
c  epsilon      0.10969E+02      11   0.34108E-08   0.96724E-02 0.16699E+00 
c  TempC        0.25716E+06      16   0.15174E-04   0.83425E-02 0.43165E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61361       0.0052573       0.0015075
v  Velocity[Y]            -0.57324          0.5439       0.0030782      0.00087209
v  Velocity[Z]              1.5659          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4413          4.3406          4.3632
v  Pressure                -36.424          360.01          87.621          169.83
v  r11                   0.0010625        0.081875        0.013077        0.018287
v  r22                   0.0011164        0.082591        0.013357        0.018647
v  r33                   0.0016451         0.17434        0.027256        0.037209
v  r12                   -0.010661        0.013585     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052776      9.3395e-05       0.0010139
v  r23                   -0.046716        0.051207      3.0611e-05      0.00057467
v  epsilon                0.069711          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9934e-05       0.0099179      0.00092538       0.0017429
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017905          5.2784         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71353         0.85285


 TIME FOR THE TIME STEP            11221:        0.69326E+02

===============================================================


 INSTANT    0.112220000E-01   TIME STEP NUMBER           11222
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.944711785E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.102840888E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934923E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.326423067E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149833499E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123964490E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81317E-03   0.45245E-02 0.19914E+01 
c  Velocity[X]                                      0.13718E-03 
c  Velocity[Y]                                      0.12744E-03 
c  Velocity[Z]                                      0.42598E-02 
c  Pressure     0.36268E-04     133   0.92366E-02   0.25580E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.49022E-08   0.16277E-08 0.98879E-01 
c  r22          0.10853E-01      13   0.51768E-08   0.17691E-08 0.10033E+00 
c  r33          0.21862E-01      15   0.62022E-08   0.12229E-07 0.12616E+00 
c  r12          0.93881E-03      18   0.64483E-08   0.29208E-09 0.59920E+00 
c  r13          0.46679E-02      18   0.67047E-08   0.14466E-08 0.19835E+00 
c  r23          0.39980E-02      19   0.60290E-08   0.12646E-08 0.19776E+00 
c  epsilon      0.10969E+02      11   0.33102E-08   0.96555E-02 0.16520E+00 
c  TempC        0.25716E+06      16   0.15161E-04   0.84119E-02 0.43296E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337          0.6136       0.0052574       0.0015075
v  Velocity[Y]            -0.57323         0.54404       0.0030781      0.00087207
v  Velocity[Z]              1.5659          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4413          4.3406          4.3632
v  Pressure                 -36.49          360.02          87.658          169.85
v  r11                   0.0010625        0.081876        0.013077        0.018287
v  r22                   0.0011164        0.082595        0.013357        0.018647
v  r33                   0.0016451         0.17434        0.027256        0.037209
v  r12                   -0.010662        0.013585     -0.00023388     -0.00030934
v  r13                   -0.045505        0.052773      9.3396e-05       0.0010139
v  r23                   -0.046717        0.051187      3.0611e-05      0.00057467
v  epsilon                0.069713          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9933e-05       0.0099178      0.00092538       0.0017429
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017906          5.2784         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85284


 TIME FOR THE TIME STEP            11222:        0.68510E+02

===============================================================


 INSTANT    0.112230000E-01   TIME STEP NUMBER           11223
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.139303732E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.427890370E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.231376149E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.199076108E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.102270892E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81276E-03   0.45233E-02 0.19906E+01 
c  Velocity[X]                                      0.13776E-03 
c  Velocity[Y]                                      0.12769E-03 
c  Velocity[Z]                                      0.42579E-02 
c  Pressure     0.36230E-04     132   0.92251E-02   0.25553E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51533E-08   0.16167E-08 0.98535E-01 
c  r22          0.10853E-01      13   0.50816E-08   0.18128E-08 0.10073E+00 
c  r33          0.21862E-01      15   0.54355E-08   0.12410E-07 0.12631E+00 
c  r12          0.93881E-03      18   0.58562E-08   0.30007E-09 0.60372E+00 
c  r13          0.46679E-02      18   0.64725E-08   0.14934E-08 0.19979E+00 
c  r23          0.39980E-02      19   0.62289E-08   0.12729E-08 0.19763E+00 
c  epsilon      0.10969E+02      11   0.34258E-08   0.98505E-02 0.16564E+00 
c  TempC        0.25716E+06      16   0.15109E-04   0.84566E-02 0.43372E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61359       0.0052573       0.0015074
v  Velocity[Y]             -0.5734         0.54374       0.0030782      0.00087211
v  Velocity[Z]              1.5658          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4413          4.3406          4.3632
v  Pressure                -36.404          360.05          87.661          169.86
v  r11                   0.0010625        0.081876        0.013077        0.018287
v  r22                   0.0011164        0.082598        0.013357        0.018647
v  r33                   0.0016451         0.17435        0.027256        0.037209
v  r12                   -0.010669        0.013587     -0.00023388     -0.00030934
v  r13                   -0.045504        0.052768      9.3396e-05       0.0010139
v  r23                   -0.046718        0.051215      3.0612e-05      0.00057467
v  epsilon                0.069714           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9933e-05       0.0099178      0.00092538       0.0017429
v  CourantNb               0.44214             0.6         0.59908         0.59839
v  FourierNb             0.0017906          5.2786         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71353         0.85284


 TIME FOR THE TIME STEP            11223:        0.68902E+02

===============================================================


 INSTANT    0.112240000E-01   TIME STEP NUMBER           11224
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.192741523E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127385783E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.178741247E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123929017E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127745816E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81377E-03   0.44844E-02 0.19833E+01 
c  Velocity[X]                                      0.13591E-03 
c  Velocity[Y]                                      0.12683E-03 
c  Velocity[Z]                                      0.42217E-02 
c  Pressure     0.36431E-04     132   0.92732E-02   0.25695E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52607E-08   0.16326E-08 0.98598E-01 
c  r22          0.10853E-01      13   0.53347E-08   0.18251E-08 0.10117E+00 
c  r33          0.21862E-01      15   0.64681E-08   0.12580E-07 0.12692E+00 
c  r12          0.93881E-03      18   0.63533E-08   0.29540E-09 0.60218E+00 
c  r13          0.46679E-02      19   0.54192E-08   0.15018E-08 0.20009E+00 
c  r23          0.39980E-02      19   0.59318E-08   0.12817E-08 0.19814E+00 
c  epsilon      0.10969E+02      11   0.36260E-08   0.10072E-01 0.16617E+00 
c  TempC        0.25716E+06      16   0.15193E-04   0.83930E-02 0.43178E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61361       0.0052573       0.0015075
v  Velocity[Y]            -0.57339         0.54379       0.0030781      0.00087207
v  Velocity[Z]              1.5659          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5798          5.4413          4.3406          4.3632
v  Pressure                -36.456          360.05          87.673          169.88
v  r11                   0.0010625         0.08188        0.013077        0.018287
v  r22                   0.0011164        0.082598        0.013357        0.018647
v  r33                   0.0016451         0.17437        0.027256        0.037209
v  r12                   -0.010667        0.013592     -0.00023388     -0.00030934
v  r13                   -0.045507        0.052768      9.3395e-05       0.0010139
v  r23                   -0.046719        0.051203      3.0611e-05      0.00057467
v  epsilon                0.069715          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099178      0.00092538       0.0017429
v  CourantNb               0.44221             0.6         0.59908         0.59839
v  FourierNb             0.0017906          5.2781         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            11224:        0.68247E+02

===============================================================


 INSTANT    0.112250000E-01   TIME STEP NUMBER           11225
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.163438009E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136877569E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.172282522E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935023E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.721681339E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.141873912E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40354E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81178E-03   0.45189E-02 0.19903E+01 
c  Velocity[X]                                      0.13752E-03 
c  Velocity[Y]                                      0.12762E-03 
c  Velocity[Z]                                      0.42538E-02 
c  Pressure     0.36479E-04     131   0.92872E-02   0.25730E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51534E-08   0.16099E-08 0.98077E-01 
c  r22          0.10853E-01      13   0.54166E-08   0.18147E-08 0.10059E+00 
c  r33          0.21862E-01      15   0.56545E-08   0.12449E-07 0.12599E+00 
c  r12          0.93881E-03      18   0.56097E-08   0.29312E-09 0.60168E+00 
c  r13          0.46679E-02      18   0.70115E-08   0.15144E-08 0.19985E+00 
c  r23          0.39980E-02      19   0.56765E-08   0.12766E-08 0.19650E+00 
c  epsilon      0.10969E+02      11   0.34478E-08   0.99992E-02 0.16618E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.83831E-02 0.43185E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61361       0.0052573       0.0015075
v  Velocity[Y]            -0.57345           0.544       0.0030782      0.00087211
v  Velocity[Z]               1.566          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5798          5.4413          4.3406          4.3632
v  Pressure                -36.412          359.97           87.61          169.81
v  r11                   0.0010625        0.081882        0.013077        0.018287
v  r22                   0.0011164        0.082599        0.013357        0.018647
v  r33                   0.0016451         0.17438        0.027256        0.037209
v  r12                   -0.010664        0.013587     -0.00023388     -0.00030934
v  r13                   -0.045506        0.052769      9.3396e-05       0.0010139
v  r23                    -0.04672        0.051196       3.061e-05      0.00057467
v  epsilon                0.069717          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.993e-05       0.0099178      0.00092538       0.0017429
v  CourantNb               0.44215             0.6         0.59908         0.59839
v  FourierNb             0.0017906          5.2775         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71353         0.85285


 TIME FOR THE TIME STEP            11225:        0.69585E+02

===============================================================


 INSTANT    0.112260000E-01   TIME STEP NUMBER           11226
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.115024739E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.792143261E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.195331179E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172398124E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117681160E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81365E-03   0.45500E-02 0.19966E+01 
c  Velocity[X]                                      0.13751E-03 
c  Velocity[Y]                                      0.12770E-03 
c  Velocity[Z]                                      0.42848E-02 
c  Pressure     0.36514E-04     132   0.92941E-02   0.25754E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53918E-08   0.16180E-08 0.98480E-01 
c  r22          0.10853E-01      13   0.57436E-08   0.18147E-08 0.10086E+00 
c  r33          0.21862E-01      15   0.53879E-08   0.12367E-07 0.12622E+00 
c  r12          0.93881E-03      18   0.65070E-08   0.29784E-09 0.60366E+00 
c  r13          0.46679E-02      19   0.60052E-08   0.14903E-08 0.19942E+00 
c  r23          0.39980E-02      19   0.63206E-08   0.12768E-08 0.19732E+00 
c  epsilon      0.10969E+02      11   0.33587E-08   0.97091E-02 0.16397E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.84363E-02 0.43345E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63379         0.61361       0.0052573       0.0015075
v  Velocity[Y]            -0.57326         0.54403       0.0030782       0.0008721
v  Velocity[Z]              1.5659          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4413          4.3406          4.3632
v  Pressure                -36.461          359.99          87.636          169.83
v  r11                   0.0010625        0.081883        0.013077        0.018287
v  r22                   0.0011164          0.0826        0.013357        0.018647
v  r33                   0.0016451          0.1744        0.027256        0.037209
v  r12                   -0.010665        0.013588     -0.00023388     -0.00030934
v  r13                   -0.045504        0.052772      9.3397e-05       0.0010139
v  r23                   -0.046722         0.05121      3.0611e-05      0.00057467
v  epsilon                0.069718          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099177      0.00092538       0.0017429
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017906          5.2783         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71352         0.85284


 TIME FOR THE TIME STEP            11226:        0.67183E+02

===============================================================


 INSTANT    0.112270000E-01   TIME STEP NUMBER           11227
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151844020E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282157325E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.510498515E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188496979E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.421785418E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81248E-03   0.44993E-02 0.19853E+01 
c  Velocity[X]                                      0.13647E-03 
c  Velocity[Y]                                      0.12770E-03 
c  Velocity[Z]                                      0.42351E-02 
c  Pressure     0.36177E-04     133   0.92102E-02   0.25516E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51929E-08   0.16445E-08 0.99099E-01 
c  r22          0.10853E-01      13   0.57283E-08   0.18180E-08 0.10088E+00 
c  r33          0.21862E-01      15   0.55584E-08   0.12594E-07 0.12746E+00 
c  r12          0.93881E-03      18   0.64258E-08   0.29388E-09 0.60305E+00 
c  r13          0.46679E-02      19   0.55095E-08   0.14949E-08 0.19999E+00 
c  r23          0.39980E-02      19   0.59092E-08   0.12860E-08 0.19928E+00 
c  epsilon      0.10969E+02      11   0.34320E-08   0.10292E-01 0.17129E+00 
c  TempC        0.25716E+06      16   0.15115E-04   0.83520E-02 0.43094E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6337         0.61365       0.0052573       0.0015074
v  Velocity[Y]            -0.57332         0.54412       0.0030782       0.0008721
v  Velocity[Z]              1.5657          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4413          4.3406          4.3632
v  Pressure                -36.421          360.03           87.65          169.86
v  r11                   0.0010625        0.081886        0.013077        0.018287
v  r22                   0.0011164        0.082601        0.013357        0.018647
v  r33                   0.0016451         0.17441        0.027256        0.037209
v  r12                   -0.010667        0.013588     -0.00023388     -0.00030934
v  r13                   -0.045507        0.052773      9.3396e-05       0.0010139
v  r23                   -0.046722        0.051193      3.0611e-05      0.00057467
v  epsilon                0.069719          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099176      0.00092538       0.0017429
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017907          5.2786         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71353         0.85284


 TIME FOR THE TIME STEP            11227:        0.69909E+02

===============================================================


 INSTANT    0.112280000E-01   TIME STEP NUMBER           11228
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.177004714E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.208236354E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934912E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.397103231E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.531066530E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.344170006E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81292E-03   0.44878E-02 0.19839E+01 
c  Velocity[X]                                      0.13729E-03 
c  Velocity[Y]                                      0.12774E-03 
c  Velocity[Z]                                      0.42228E-02 
c  Pressure     0.36339E-04     133   0.92488E-02   0.25630E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56674E-08   0.16060E-08 0.98065E-01 
c  r22          0.10853E-01      13   0.51383E-08   0.18030E-08 0.10109E+00 
c  r33          0.21862E-01      15   0.55520E-08   0.12283E-07 0.12612E+00 
c  r12          0.93881E-03      18   0.57935E-08   0.29283E-09 0.60253E+00 
c  r13          0.46679E-02      19   0.54768E-08   0.14815E-08 0.19920E+00 
c  r23          0.39980E-02      19   0.60936E-08   0.12742E-08 0.19682E+00 
c  epsilon      0.10969E+02      11   0.33125E-08   0.96623E-02 0.16423E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.83851E-02 0.43240E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161993


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61362       0.0052573       0.0015074
v  Velocity[Y]            -0.57326         0.54423       0.0030781      0.00087205
v  Velocity[Z]              1.5658          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4413          4.3406          4.3632
v  Pressure                -36.477          360.05          87.675          169.88
v  r11                   0.0010625        0.081885        0.013077        0.018287
v  r22                   0.0011164        0.082601        0.013357        0.018647
v  r33                   0.0016451         0.17437        0.027256        0.037209
v  r12                    -0.01067        0.013591     -0.00023388     -0.00030934
v  r13                   -0.045504        0.052772      9.3396e-05       0.0010139
v  r23                   -0.046723        0.051183      3.0611e-05      0.00057466
v  epsilon                0.069721          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099176      0.00092538       0.0017429
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb             0.0017907          5.2785         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            11228:        0.70072E+02

===============================================================


 INSTANT    0.112290000E-01   TIME STEP NUMBER           11229
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.525886296E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.179634876E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.102191443E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.142777687E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.269301864E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81248E-03   0.45260E-02 0.19916E+01 
c  Velocity[X]                                      0.13739E-03 
c  Velocity[Y]                                      0.12774E-03 
c  Velocity[Z]                                      0.42609E-02 
c  Pressure     0.36203E-04     132   0.92129E-02   0.25536E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53174E-08   0.16078E-08 0.98123E-01 
c  r22          0.10853E-01      13   0.48836E-08   0.18113E-08 0.10055E+00 
c  r33          0.21862E-01      15   0.58132E-08   0.12340E-07 0.12586E+00 
c  r12          0.93881E-03      18   0.51016E-08   0.30106E-09 0.60340E+00 
c  r13          0.46679E-02      19   0.58458E-08   0.14713E-08 0.19848E+00 
c  r23          0.39980E-02      19   0.55121E-08   0.12653E-08 0.19665E+00 
c  epsilon      0.10969E+02      11   0.35239E-08   0.98044E-02 0.16370E+00 
c  TempC        0.25716E+06      16   0.15172E-04   0.84234E-02 0.43332E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369          0.6136       0.0052573       0.0015075
v  Velocity[Y]             -0.5733         0.54403       0.0030781      0.00087205
v  Velocity[Z]              1.5659          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4413          4.3406          4.3632
v  Pressure                -36.415          360.04          87.657          169.86
v  r11                   0.0010625        0.081883        0.013077        0.018287
v  r22                   0.0011164        0.082599        0.013357        0.018647
v  r33                   0.0016451         0.17434        0.027256        0.037209
v  r12                   -0.010671         0.01359     -0.00023388     -0.00030934
v  r13                   -0.045505        0.052772      9.3397e-05       0.0010139
v  r23                   -0.046724        0.051209      3.0611e-05      0.00057466
v  epsilon                0.069722          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099177      0.00092539       0.0017429
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017907          5.2786         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71353         0.85284


 TIME FOR THE TIME STEP            11229:        0.69514E+02

===============================================================


 INSTANT    0.112300000E-01   TIME STEP NUMBER           11230
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.105117836E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.380726559E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.327878765E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.192065789E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.119976100E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21884E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81356E-03   0.44913E-02 0.19834E+01 
c  Velocity[X]                                      0.13622E-03 
c  Velocity[Y]                                      0.12692E-03 
c  Velocity[Z]                                      0.42282E-02 
c  Pressure     0.36169E-04     132   0.92098E-02   0.25510E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51694E-08   0.16021E-08 0.97873E-01 
c  r22          0.10853E-01      13   0.48728E-08   0.17641E-08 0.99819E-01 
c  r33          0.21862E-01      15   0.52791E-08   0.12102E-07 0.12508E+00 
c  r12          0.93881E-03      18   0.55455E-08   0.29440E-09 0.60212E+00 
c  r13          0.46679E-02      19   0.69443E-08   0.14444E-08 0.19792E+00 
c  r23          0.39980E-02      19   0.70703E-08   0.12493E-08 0.19551E+00 
c  epsilon      0.10969E+02      11   0.33609E-08   0.94165E-02 0.16194E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.83029E-02 0.42963E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161996


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63373         0.61365       0.0052573       0.0015074
v  Velocity[Y]            -0.57317         0.54398       0.0030781      0.00087203
v  Velocity[Z]              1.5657          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4413          4.3406          4.3632
v  Pressure                -36.448          359.97          87.624          169.81
v  r11                   0.0010625        0.081885        0.013077        0.018287
v  r22                   0.0011164        0.082598        0.013357        0.018647
v  r33                   0.0016451         0.17433        0.027256        0.037209
v  r12                   -0.010674         0.01359     -0.00023388     -0.00030934
v  r13                   -0.045507        0.052775      9.3397e-05       0.0010139
v  r23                   -0.046725        0.051195      3.0611e-05      0.00057466
v  epsilon                0.069723          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099177      0.00092539       0.0017429
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017908          5.2783         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71353         0.85285


 TIME FOR THE TIME STEP            11230:        0.69137E+02

===============================================================


 INSTANT    0.112310000E-01   TIME STEP NUMBER           11231
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.221742029E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.155188498E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.740625323E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.245008334E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.150209275E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69762E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81284E-03   0.45011E-02 0.19862E+01 
c  Velocity[X]                                      0.13683E-03 
c  Velocity[Y]                                      0.12787E-03 
c  Velocity[Z]                                      0.42364E-02 
c  Pressure     0.36281E-04     133   0.92308E-02   0.25589E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53322E-08   0.16249E-08 0.98340E-01 
c  r22          0.10853E-01      13   0.52173E-08   0.18000E-08 0.10025E+00 
c  r33          0.21862E-01      15   0.56714E-08   0.12437E-07 0.12605E+00 
c  r12          0.93881E-03      18   0.52719E-08   0.29054E-09 0.59961E+00 
c  r13          0.46679E-02      19   0.68801E-08   0.14718E-08 0.19854E+00 
c  r23          0.39980E-02      19   0.67167E-08   0.12835E-08 0.19781E+00 
c  epsilon      0.10969E+02      11   0.32410E-08   0.10003E-01 0.16620E+00 
c  TempC        0.25716E+06      16   0.15142E-04   0.83751E-02 0.43204E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63365         0.61364       0.0052573       0.0015074
v  Velocity[Y]            -0.57327         0.54406       0.0030781      0.00087205
v  Velocity[Z]              1.5656          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4413          4.3406          4.3632
v  Pressure                -36.398          360.02          87.651          169.86
v  r11                   0.0010625         0.08188        0.013077        0.018287
v  r22                   0.0011164        0.082598        0.013357        0.018647
v  r33                   0.0016451         0.17435        0.027256        0.037209
v  r12                   -0.010674        0.013586     -0.00023388     -0.00030934
v  r13                   -0.045505        0.052777      9.3397e-05       0.0010139
v  r23                   -0.046725        0.051185      3.0611e-05      0.00057466
v  epsilon                0.069724          271.18          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099177      0.00092539       0.0017429
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017908          5.2784         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85284


 TIME FOR THE TIME STEP            11231:        0.69505E+02

===============================================================


 INSTANT    0.112320000E-01   TIME STEP NUMBER           11232
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.184748467E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.415690560E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.209945768E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.113352605E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.300832304E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69761E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81323E-03   0.45080E-02 0.19883E+01 
c  Velocity[X]                                      0.13705E-03 
c  Velocity[Y]                                      0.12821E-03 
c  Velocity[Z]                                      0.42428E-02 
c  Pressure     0.36192E-04     131   0.92147E-02   0.25526E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60831E-08   0.16386E-08 0.98603E-01 
c  r22          0.10853E-01      13   0.50922E-08   0.18338E-08 0.10128E+00 
c  r33          0.21862E-01      15   0.55269E-08   0.12609E-07 0.12722E+00 
c  r12          0.93881E-03      18   0.51964E-08   0.29481E-09 0.60301E+00 
c  r13          0.46679E-02      19   0.65117E-08   0.15015E-08 0.20003E+00 
c  r23          0.39980E-02      19   0.56082E-08   0.13052E-08 0.19945E+00 
c  epsilon      0.10969E+02      11   0.31926E-08   0.10311E-01 0.17010E+00 
c  TempC        0.25716E+06      16   0.15188E-04   0.84539E-02 0.43402E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61365       0.0052573       0.0015074
v  Velocity[Y]            -0.57328         0.54419       0.0030781      0.00087206
v  Velocity[Z]              1.5656          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4413          4.3406          4.3632
v  Pressure                -36.464          360.01          87.653          169.85
v  r11                   0.0010625        0.081881        0.013077        0.018287
v  r22                   0.0011164        0.082596        0.013357        0.018647
v  r33                   0.0016451         0.17437        0.027256        0.037209
v  r12                   -0.010673        0.013579     -0.00023388     -0.00030934
v  r13                   -0.045504        0.052779      9.3397e-05       0.0010139
v  r23                   -0.046725        0.051199       3.061e-05      0.00057466
v  epsilon                0.069726          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099177      0.00092539       0.0017429
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017908          5.2781         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            11232:        0.66927E+02

===============================================================


 INSTANT    0.112330000E-01   TIME STEP NUMBER           11233
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.340270246E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.460689785E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.346175384E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.466491753E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.352474077E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934998E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81213E-03   0.44955E-02 0.19832E+01 
c  Velocity[X]                                      0.13774E-03 
c  Velocity[Y]                                      0.12694E-03 
c  Velocity[Z]                                      0.42308E-02 
c  Pressure     0.36375E-04     131   0.92580E-02   0.25656E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61236E-08   0.16279E-08 0.98817E-01 
c  r22          0.10853E-01      13   0.55666E-08   0.18219E-08 0.10152E+00 
c  r33          0.21862E-01      14   0.68448E-08   0.12402E-07 0.12723E+00 
c  r12          0.93881E-03      18   0.59230E-08   0.29517E-09 0.60246E+00 
c  r13          0.46679E-02      19   0.59628E-08   0.14919E-08 0.20123E+00 
c  r23          0.39980E-02      19   0.57449E-08   0.12726E-08 0.19859E+00 
c  epsilon      0.10969E+02      11   0.32010E-08   0.96903E-02 0.16238E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.83698E-02 0.43182E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161994


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6336         0.61369       0.0052572       0.0015074
v  Velocity[Y]            -0.57329         0.54399       0.0030781      0.00087203
v  Velocity[Z]              1.5656          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4413          4.3406          4.3632
v  Pressure                -36.406          360.03          87.637          169.85
v  r11                   0.0010625        0.081878        0.013077        0.018287
v  r22                   0.0011164        0.082594        0.013357        0.018647
v  r33                   0.0016451         0.17438        0.027256        0.037209
v  r12                    -0.01067        0.013572     -0.00023388     -0.00030934
v  r13                   -0.045508        0.052779      9.3397e-05       0.0010139
v  r23                   -0.046725        0.051192      3.0611e-05      0.00057466
v  epsilon                0.069727          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099178      0.00092539       0.0017429
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017908          5.2783         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71352         0.85284


 TIME FOR THE TIME STEP            11233:        0.69883E+02

===============================================================


 INSTANT    0.112340000E-01   TIME STEP NUMBER           11234
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.599292402E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237625144E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.114487574E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.269768712E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.190649829E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81279E-03   0.45136E-02 0.19907E+01 
c  Velocity[X]                                      0.13738E-03 
c  Velocity[Y]                                      0.12756E-03 
c  Velocity[Z]                                      0.42487E-02 
c  Pressure     0.36164E-04     131   0.92050E-02   0.25508E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.66115E-08   0.16019E-08 0.98460E-01 
c  r22          0.10853E-01      13   0.53257E-08   0.17707E-08 0.10048E+00 
c  r33          0.21862E-01      15   0.56036E-08   0.12136E-07 0.12630E+00 
c  r12          0.93881E-03      18   0.56121E-08   0.28572E-09 0.59879E+00 
c  r13          0.46679E-02      19   0.68589E-08   0.14474E-08 0.19876E+00 
c  r23          0.39980E-02      19   0.57405E-08   0.12600E-08 0.19760E+00 
c  epsilon      0.10969E+02      11   0.33225E-08   0.93424E-02 0.16162E+00 
c  TempC        0.25716E+06      16   0.15179E-04   0.84346E-02 0.43232E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161990


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364         0.61368       0.0052572       0.0015074
v  Velocity[Y]            -0.57305          0.5441        0.003078      0.00087201
v  Velocity[Z]              1.5659          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4413          4.3406          4.3632
v  Pressure                -36.442          359.99          87.628          169.82
v  r11                   0.0010625        0.081877        0.013077        0.018287
v  r22                   0.0011164        0.082598        0.013357        0.018647
v  r33                   0.0016451          0.1744        0.027256        0.037209
v  r12                   -0.010672        0.013579     -0.00023388     -0.00030934
v  r13                   -0.045505        0.052779      9.3397e-05       0.0010139
v  r23                   -0.046724        0.051186      3.0611e-05      0.00057466
v  epsilon                0.069728          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099176      0.00092539       0.0017429
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017908          5.2782         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71353         0.85284


 TIME FOR THE TIME STEP            11234:        0.70159E+02

===============================================================


 INSTANT    0.112350000E-01   TIME STEP NUMBER           11235
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.274525676E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.232639241E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182959121E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.102413150E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.277036623E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81267E-03   0.44982E-02 0.19849E+01 
c  Velocity[X]                                      0.13768E-03 
c  Velocity[Y]                                      0.12787E-03 
c  Velocity[Z]                                      0.42327E-02 
c  Pressure     0.36114E-04     132   0.91876E-02   0.25472E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61733E-08   0.16159E-08 0.99105E-01 
c  r22          0.10853E-01      13   0.57934E-08   0.17991E-08 0.10098E+00 
c  r33          0.21862E-01      15   0.56449E-08   0.12245E-07 0.12687E+00 
c  r12          0.93881E-03      18   0.61073E-08   0.29263E-09 0.60143E+00 
c  r13          0.46679E-02      19   0.70739E-08   0.14642E-08 0.19929E+00 
c  r23          0.39980E-02      19   0.57773E-08   0.12511E-08 0.19698E+00 
c  epsilon      0.10969E+02      11   0.32751E-08   0.95019E-02 0.16302E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.84043E-02 0.43248E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369         0.61368       0.0052573       0.0015074
v  Velocity[Y]            -0.57302         0.54412       0.0030781      0.00087208
v  Velocity[Z]              1.5657          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4413          4.3406          4.3632
v  Pressure                -36.415          360.05          87.656          169.87
v  r11                   0.0010625        0.081875        0.013077        0.018287
v  r22                   0.0011164          0.0826        0.013357        0.018647
v  r33                   0.0016452         0.17442        0.027256        0.037209
v  r12                    -0.01067        0.013578     -0.00023388     -0.00030934
v  r13                   -0.045504        0.052776      9.3397e-05       0.0010139
v  r23                   -0.046723        0.051211      3.0611e-05      0.00057466
v  epsilon                 0.06973          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9925e-05       0.0099176      0.00092539       0.0017429
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017909           5.278         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7403e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71353         0.85285


 TIME FOR THE TIME STEP            11235:        0.70011E+02

===============================================================


 INSTANT    0.112360000E-01   TIME STEP NUMBER           11236
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.328759096E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.399399665E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.150381975E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.233566544E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.161346304E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81382E-03   0.44894E-02 0.19813E+01 
c  Velocity[X]                                      0.13606E-03 
c  Velocity[Y]                                      0.12633E-03 
c  Velocity[Z]                                      0.42270E-02 
c  Pressure     0.36193E-04     132   0.92132E-02   0.25527E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59307E-08   0.16121E-08 0.98755E-01 
c  r22          0.10853E-01      13   0.59455E-08   0.18164E-08 0.10128E+00 
c  r33          0.21862E-01      15   0.58316E-08   0.12427E-07 0.12721E+00 
c  r12          0.93881E-03      18   0.63927E-08   0.29345E-09 0.59920E+00 
c  r13          0.46679E-02      19   0.72916E-08   0.14938E-08 0.20029E+00 
c  r23          0.39980E-02      19   0.60289E-08   0.12888E-08 0.19896E+00 
c  epsilon      0.10969E+02      11   0.33298E-08   0.97345E-02 0.16455E+00 
c  TempC        0.25716E+06      16   0.15186E-04   0.83660E-02 0.43209E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61373       0.0052572       0.0015074
v  Velocity[Y]            -0.57305         0.54413        0.003078      0.00087208
v  Velocity[Z]              1.5657          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4413          4.3406          4.3632
v  Pressure                -36.424          360.04          87.665          169.87
v  r11                   0.0010625        0.081877        0.013077        0.018287
v  r22                   0.0011164          0.0826        0.013357        0.018647
v  r33                   0.0016452         0.17443        0.027256        0.037209
v  r12                    -0.01067        0.013575     -0.00023388     -0.00030934
v  r13                   -0.045506        0.052776      9.3396e-05       0.0010139
v  r23                   -0.046721        0.051196       3.061e-05      0.00057466
v  epsilon                0.069731          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9927e-05       0.0099177      0.00092539       0.0017429
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017909          5.2778         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85284


 TIME FOR THE TIME STEP            11236:        0.68427E+02

===============================================================


 INSTANT    0.112370000E-01   TIME STEP NUMBER           11237
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.116198561E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.417232405E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.168841197E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119202730E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.291758309E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81163E-03   0.45247E-02 0.19911E+01 
c  Velocity[X]                                      0.13757E-03 
c  Velocity[Y]                                      0.12795E-03 
c  Velocity[Z]                                      0.42592E-02 
c  Pressure     0.36213E-04     131   0.92227E-02   0.25541E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58043E-08   0.16079E-08 0.98580E-01 
c  r22          0.10853E-01      13   0.60437E-08   0.17879E-08 0.10027E+00 
c  r33          0.21862E-01      15   0.60031E-08   0.12249E-07 0.12620E+00 
c  r12          0.93881E-03      18   0.67251E-08   0.29615E-09 0.60198E+00 
c  r13          0.46679E-02      19   0.68855E-08   0.14620E-08 0.19820E+00 
c  r23          0.39980E-02      19   0.54394E-08   0.12622E-08 0.19706E+00 
c  epsilon      0.10969E+02      11   0.32746E-08   0.95392E-02 0.16269E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.83914E-02 0.43220E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63366         0.61375       0.0052571       0.0015074
v  Velocity[Y]            -0.57321         0.54419        0.003078      0.00087207
v  Velocity[Z]              1.5658          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4413          4.3406          4.3632
v  Pressure                -36.394             360          87.636          169.83
v  r11                   0.0010625        0.081875        0.013077        0.018287
v  r22                   0.0011164        0.082601        0.013357        0.018647
v  r33                   0.0016452         0.17439        0.027256        0.037209
v  r12                   -0.010671        0.013577     -0.00023388     -0.00030934
v  r13                   -0.045506        0.052776      9.3396e-05       0.0010139
v  r23                    -0.04672        0.051179       3.061e-05      0.00057466
v  epsilon                0.069732          271.16          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9928e-05       0.0099177      0.00092539       0.0017429
v  CourantNb                0.4423             0.6         0.59908         0.59839
v  FourierNb             0.0017909          5.2772         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71353         0.85284


 TIME FOR THE TIME STEP            11237:        0.68474E+02

===============================================================


 INSTANT    0.112380000E-01   TIME STEP NUMBER           11238
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.400266187E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.160561989E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.504733053E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166254382E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.178786898E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81311E-03   0.44988E-02 0.19846E+01 
c  Velocity[X]                                      0.13757E-03 
c  Velocity[Y]                                      0.12774E-03 
c  Velocity[Z]                                      0.42335E-02 
c  Pressure     0.36548E-04     134   0.93001E-02   0.25778E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59035E-08   0.16917E-08 0.10096E+00 
c  r22          0.10853E-01      13   0.56038E-08   0.18822E-08 0.10279E+00 
c  r33          0.21862E-01      15   0.58090E-08   0.13019E-07 0.13007E+00 
c  r12          0.93881E-03      18   0.72078E-08   0.32262E-09 0.62564E+00 
c  r13          0.46679E-02      19   0.71067E-08   0.15375E-08 0.20254E+00 
c  r23          0.39980E-02      19   0.56562E-08   0.13502E-08 0.20523E+00 
c  epsilon      0.10969E+02      11   0.33497E-08   0.10341E-01 0.17226E+00 
c  TempC        0.25716E+06      16   0.15130E-04   0.83988E-02 0.43226E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63359         0.61374       0.0052572       0.0015074
v  Velocity[Y]            -0.57323         0.54396        0.003078      0.00087205
v  Velocity[Z]              1.5657          5.4413          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4413          4.3406          4.3632
v  Pressure                -36.432          359.99           87.64          169.83
v  r11                   0.0010625        0.081875        0.013077        0.018287
v  r22                   0.0011164        0.082602        0.013357        0.018647
v  r33                   0.0016452         0.17433        0.027256        0.037209
v  r12                   -0.010671        0.013572     -0.00023389     -0.00030934
v  r13                   -0.045503        0.052775      9.3396e-05       0.0010139
v  r23                   -0.046719        0.051168      3.0609e-05      0.00057466
v  epsilon                0.069734          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9929e-05       0.0099177      0.00092539       0.0017429
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017909           5.278         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            11238:        0.13204E+03

===============================================================


 INSTANT    0.112390000E-01   TIME STEP NUMBER           11239
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.381477701E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294862135E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934966E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138688546E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.253926873E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.294361248E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81286E-03   0.44900E-02 0.19830E+01 
c  Velocity[X]                                      0.13639E-03 
c  Velocity[Y]                                      0.12720E-03 
c  Velocity[Z]                                      0.42264E-02 
c  Pressure     0.36075E-04     131   0.91917E-02   0.25445E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58014E-08   0.16508E-08 0.99411E-01 
c  r22          0.10853E-01      13   0.53449E-08   0.18269E-08 0.10157E+00 
c  r33          0.21862E-01      15   0.55596E-08   0.12543E-07 0.12770E+00 
c  r12          0.93881E-03      18   0.69170E-08   0.30466E-09 0.61187E+00 
c  r13          0.46679E-02      19   0.70294E-08   0.14927E-08 0.20038E+00 
c  r23          0.39980E-02      19   0.60674E-08   0.13066E-08 0.19991E+00 
c  epsilon      0.10969E+02      11   0.32894E-08   0.95849E-02 0.16273E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84039E-02 0.43229E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63358         0.61382       0.0052571       0.0015074
v  Velocity[Y]            -0.57325         0.54403        0.003078      0.00087208
v  Velocity[Z]              1.5659          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4414          4.3406          4.3632
v  Pressure                -36.402          359.98          87.603          169.81
v  r11                   0.0010625         0.08187        0.013077        0.018287
v  r22                   0.0011164        0.082598        0.013357        0.018647
v  r33                   0.0016452         0.17433        0.027256        0.037209
v  r12                   -0.010669        0.013574     -0.00023389     -0.00030934
v  r13                   -0.045506        0.052776      9.3396e-05       0.0010139
v  r23                   -0.046719        0.051193      3.0609e-05      0.00057466
v  epsilon                0.069735          271.14          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9931e-05       0.0099178      0.00092539       0.0017429
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb              0.001791          5.2779         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            11239:        0.87242E+02

===============================================================


 INSTANT    0.112400000E-01   TIME STEP NUMBER           11240
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.158646071E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.298616873E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934901E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.404699932E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.751095949E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.744114960E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81328E-03   0.44998E-02 0.19866E+01 
c  Velocity[X]                                      0.13767E-03 
c  Velocity[Y]                                      0.12749E-03 
c  Velocity[Z]                                      0.42346E-02 
c  Pressure     0.36455E-04     133   0.92757E-02   0.25712E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60865E-08   0.16169E-08 0.98916E-01 
c  r22          0.10853E-01      13   0.53708E-08   0.18189E-08 0.10118E+00 
c  r33          0.21862E-01      15   0.54199E-08   0.12442E-07 0.12728E+00 
c  r12          0.93881E-03      18   0.66587E-08   0.29761E-09 0.60606E+00 
c  r13          0.46679E-02      19   0.65470E-08   0.14902E-08 0.20021E+00 
c  r23          0.39980E-02      19   0.63775E-08   0.12847E-08 0.19923E+00 
c  epsilon      0.10969E+02      11   0.34436E-08   0.96369E-02 0.16319E+00 
c  TempC        0.25716E+06      16   0.15164E-04   0.83795E-02 0.43152E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364          0.6138       0.0052571       0.0015073
v  Velocity[Y]            -0.57317         0.54371        0.003078      0.00087206
v  Velocity[Z]              1.5657          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4414          4.3406          4.3632
v  Pressure                -36.439          360.07          87.689          169.89
v  r11                   0.0010625         0.08187        0.013077        0.018287
v  r22                   0.0011164        0.082599        0.013357        0.018647
v  r33                   0.0016452         0.17434        0.027256        0.037209
v  r12                   -0.010672        0.013574     -0.00023389     -0.00030934
v  r13                   -0.045503        0.052778      9.3396e-05       0.0010139
v  r23                   -0.046718        0.051194      3.0609e-05      0.00057466
v  epsilon                0.069736          271.17          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9929e-05       0.0099179      0.00092539       0.0017429
v  CourantNb               0.44222             0.6         0.59908         0.59839
v  FourierNb              0.001791          5.2782         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71353         0.85284


 TIME FOR THE TIME STEP            11240:        0.65768E+02

===============================================================


 INSTANT    0.112410000E-01   TIME STEP NUMBER           11241
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.130243914E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.370190175E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.229355718E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.308615558E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.838960188E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81272E-03   0.45228E-02 0.19923E+01 
c  Velocity[X]                                      0.13827E-03 
c  Velocity[Y]                                      0.12889E-03 
c  Velocity[Z]                                      0.42556E-02 
c  Pressure     0.36074E-04     131   0.91790E-02   0.25444E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56754E-08   0.16027E-08 0.98617E-01 
c  r22          0.10853E-01      13   0.56026E-08   0.18177E-08 0.10080E+00 
c  r33          0.21862E-01      14   0.68392E-08   0.12315E-07 0.12652E+00 
c  r12          0.93881E-03      18   0.65733E-08   0.29257E-09 0.60422E+00 
c  r13          0.46679E-02      19   0.59492E-08   0.15023E-08 0.20044E+00 
c  r23          0.39980E-02      19   0.66808E-08   0.12492E-08 0.19674E+00 
c  epsilon      0.10969E+02      11   0.33373E-08   0.96495E-02 0.16280E+00 
c  TempC        0.25716E+06      16   0.15155E-04   0.83950E-02 0.43315E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61378       0.0052572       0.0015074
v  Velocity[Y]            -0.57317         0.54348        0.003078      0.00087209
v  Velocity[Z]              1.5658          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4414          4.3406          4.3632
v  Pressure                -36.382          360.05          87.654          169.86
v  r11                   0.0010625        0.081868        0.013077        0.018287
v  r22                   0.0011164        0.082598        0.013357        0.018647
v  r33                   0.0016452         0.17436        0.027256        0.037209
v  r12                   -0.010674        0.013571     -0.00023389     -0.00030934
v  r13                   -0.045504        0.052779      9.3397e-05       0.0010139
v  r23                   -0.046717         0.05119      3.0609e-05      0.00057466
v  epsilon                0.069737          271.18          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099179      0.00092539       0.0017429
v  CourantNb                0.4422             0.6         0.59908         0.59839
v  FourierNb              0.001791          5.2782         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            11241:        0.65920E+02

===============================================================


 INSTANT    0.112420000E-01   TIME STEP NUMBER           11242
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.433910892E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.341621225E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.156540577E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.862311698E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.138985538E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31857E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81316E-03   0.44891E-02 0.19829E+01 
c  Velocity[X]                                      0.13686E-03 
c  Velocity[Y]                                      0.12684E-03 
c  Velocity[Z]                                      0.42254E-02 
c  Pressure     0.36123E-04     134   0.91980E-02   0.25478E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55128E-08   0.16514E-08 0.99585E-01 
c  r22          0.10853E-01      13   0.55118E-08   0.17858E-08 0.10077E+00 
c  r33          0.21862E-01      15   0.58886E-08   0.12408E-07 0.12701E+00 
c  r12          0.93881E-03      18   0.62184E-08   0.29512E-09 0.60474E+00 
c  r13          0.46679E-02      19   0.55284E-08   0.14770E-08 0.19988E+00 
c  r23          0.39980E-02      19   0.69206E-08   0.13070E-08 0.19968E+00 
c  epsilon      0.10969E+02      11   0.32971E-08   0.98204E-02 0.16453E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.83824E-02 0.43154E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61385       0.0052571       0.0015074
v  Velocity[Y]            -0.57312         0.54354        0.003078      0.00087205
v  Velocity[Z]              1.5658          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4414          4.3406          4.3632
v  Pressure                -36.412          360.04          87.662          169.87
v  r11                   0.0010625         0.08187        0.013077        0.018287
v  r22                   0.0011164        0.082602        0.013357        0.018647
v  r33                   0.0016452         0.17438        0.027256        0.037209
v  r12                   -0.010672        0.013574     -0.00023389     -0.00030934
v  r13                   -0.045506        0.052778      9.3396e-05       0.0010139
v  r23                   -0.046716        0.051212      3.0609e-05      0.00057466
v  epsilon                0.069739           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05        0.009918      0.00092539       0.0017429
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb              0.001791          5.2781         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71352         0.85284


 TIME FOR THE TIME STEP            11242:        0.64598E+02

===============================================================


 INSTANT    0.112430000E-01   TIME STEP NUMBER           11243
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169619665E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294876655E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.363972906E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.629381715E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.583906345E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12301E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81225E-03   0.44996E-02 0.19861E+01 
c  Velocity[X]                                      0.13761E-03 
c  Velocity[Y]                                      0.12844E-03 
c  Velocity[Z]                                      0.42335E-02 
c  Pressure     0.36429E-04     133   0.92704E-02   0.25694E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.50627E-08   0.16170E-08 0.98928E-01 
c  r22          0.10853E-01      13   0.54498E-08   0.18123E-08 0.10090E+00 
c  r33          0.21862E-01      14   0.70896E-08   0.12406E-07 0.12701E+00 
c  r12          0.93881E-03      18   0.60442E-08   0.29643E-09 0.60479E+00 
c  r13          0.46679E-02      18   0.67415E-08   0.14938E-08 0.20027E+00 
c  r23          0.39980E-02      19   0.56110E-08   0.12852E-08 0.19923E+00 
c  epsilon      0.10969E+02      11   0.33526E-08   0.97936E-02 0.16409E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.83845E-02 0.43170E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63357         0.61383       0.0052571       0.0015073
v  Velocity[Y]            -0.57327         0.54373        0.003078      0.00087209
v  Velocity[Z]              1.5659          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4414          4.3406          4.3632
v  Pressure                -36.405          359.96          87.601           169.8
v  r11                   0.0010625        0.081874        0.013077        0.018287
v  r22                   0.0011164        0.082603        0.013357        0.018647
v  r33                   0.0016452         0.17439        0.027256        0.037209
v  r12                    -0.01067        0.013572     -0.00023389     -0.00030934
v  r13                   -0.045504        0.052773      9.3396e-05       0.0010139
v  r23                   -0.046716        0.051207      3.0609e-05      0.00057466
v  epsilon                 0.06974           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099181      0.00092539       0.0017429
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017911          5.2779         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            11243:        0.64418E+02

===============================================================


 INSTANT    0.112440000E-01   TIME STEP NUMBER           11244
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.377783864E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.240397411E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934902E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.120687445E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.239351815E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.190978856E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81389E-03   0.45000E-02 0.19856E+01 
c  Velocity[X]                                      0.13691E-03 
c  Velocity[Y]                                      0.12803E-03 
c  Velocity[Z]                                      0.42350E-02 
c  Pressure     0.36574E-04     133   0.93064E-02   0.25797E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55245E-08   0.16459E-08 0.10024E+00 
c  r22          0.10853E-01      13   0.55803E-08   0.18304E-08 0.10218E+00 
c  r33          0.21862E-01      15   0.53778E-08   0.12550E-07 0.12876E+00 
c  r12          0.93881E-03      18   0.64601E-08   0.30098E-09 0.60972E+00 
c  r13          0.46679E-02      18   0.70885E-08   0.15105E-08 0.20196E+00 
c  r23          0.39980E-02      19   0.61628E-08   0.12992E-08 0.20198E+00 
c  epsilon      0.10969E+02      11   0.32710E-08   0.10022E-01 0.17036E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.84255E-02 0.43327E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63358         0.61381       0.0052572       0.0015074
v  Velocity[Y]             -0.5733         0.54394        0.003078      0.00087211
v  Velocity[Z]              1.5661          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5799          5.4414          4.3406          4.3632
v  Pressure                -36.417          359.99          87.641          169.83
v  r11                   0.0010625        0.081873        0.013077        0.018287
v  r22                   0.0011164        0.082601        0.013357        0.018647
v  r33                   0.0016452         0.17436        0.027256        0.037209
v  r12                   -0.010668        0.013578     -0.00023389     -0.00030934
v  r13                   -0.045503        0.052769      9.3397e-05       0.0010139
v  r23                   -0.046715         0.05119       3.061e-05      0.00057466
v  epsilon                0.069741          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099182      0.00092539       0.0017429
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017911          5.2783         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71352         0.85284


 TIME FOR THE TIME STEP            11244:        0.65684E+02

===============================================================


 INSTANT    0.112450000E-01   TIME STEP NUMBER           11245
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122507891E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.330749590E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.282007988E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.296687753E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.645443468E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934963E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81244E-03   0.44979E-02 0.19840E+01 
c  Velocity[X]                                      0.13773E-03 
c  Velocity[Y]                                      0.12673E-03 
c  Velocity[Z]                                      0.42334E-02 
c  Pressure     0.36204E-04     132   0.92256E-02   0.25536E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.50956E-08   0.16092E-08 0.98995E-01 
c  r22          0.10853E-01      13   0.53766E-08   0.17857E-08 0.10074E+00 
c  r33          0.21862E-01      14   0.68718E-08   0.12264E-07 0.12656E+00 
c  r12          0.93881E-03      18   0.63153E-08   0.29183E-09 0.60323E+00 
c  r13          0.46679E-02      19   0.53611E-08   0.14743E-08 0.19927E+00 
c  r23          0.39980E-02      19   0.62302E-08   0.12496E-08 0.19726E+00 
c  epsilon      0.10969E+02      11   0.32886E-08   0.97112E-02 0.16382E+00 
c  TempC        0.25716E+06      16   0.15111E-04   0.83685E-02 0.43147E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162016


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63358         0.61385       0.0052571       0.0015074
v  Velocity[Y]            -0.57341         0.54411       0.0030781      0.00087213
v  Velocity[Z]              1.5658          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4414          4.3406          4.3632
v  Pressure                -36.398          360.08          87.674          169.89
v  r11                   0.0010625        0.081871        0.013077        0.018287
v  r22                   0.0011164        0.082599        0.013357        0.018647
v  r33                   0.0016452         0.17432        0.027256        0.037209
v  r12                   -0.010668        0.013573     -0.00023389     -0.00030934
v  r13                   -0.045507         0.05277      9.3396e-05       0.0010139
v  r23                   -0.046715        0.051177      3.0609e-05      0.00057466
v  epsilon                0.069743          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099183      0.00092539       0.0017429
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017911          5.2785         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8785         0.71352         0.85284


 TIME FOR THE TIME STEP            11245:        0.65205E+02

===============================================================


 INSTANT    0.112460000E-01   TIME STEP NUMBER           11246
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.288266320E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.852873140E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.227851971E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.823704162E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.598472094E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81210E-03   0.44941E-02 0.19862E+01 
c  Velocity[X]                                      0.13712E-03 
c  Velocity[Y]                                      0.12664E-03 
c  Velocity[Z]                                      0.42304E-02 
c  Pressure     0.36084E-04     133   0.91825E-02   0.25450E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54698E-08   0.16380E-08 0.99673E-01 
c  r22          0.10853E-01      13   0.52693E-08   0.18076E-08 0.10136E+00 
c  r33          0.21862E-01      15   0.52724E-08   0.12379E-07 0.12729E+00 
c  r12          0.93881E-03      18   0.55725E-08   0.28903E-09 0.60111E+00 
c  r13          0.46679E-02      18   0.65652E-08   0.14710E-08 0.19981E+00 
c  r23          0.39980E-02      19   0.56014E-08   0.12796E-08 0.19923E+00 
c  epsilon      0.10969E+02      11   0.33787E-08   0.96862E-02 0.16433E+00 
c  TempC        0.25716E+06      16   0.15188E-04   0.83661E-02 0.43127E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361         0.61385       0.0052571       0.0015074
v  Velocity[Y]            -0.57341         0.54391        0.003078      0.00087209
v  Velocity[Z]               1.566          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5798          5.4414          4.3406          4.3632
v  Pressure                -36.459          360.02          87.648          169.84
v  r11                   0.0010625        0.081872        0.013077        0.018287
v  r22                   0.0011164        0.082597        0.013357        0.018647
v  r33                   0.0016452         0.17432        0.027256        0.037209
v  r12                   -0.010673         0.01357     -0.00023389     -0.00030934
v  r13                   -0.045504        0.052773      9.3397e-05       0.0010139
v  r23                   -0.046714        0.051205      3.0609e-05      0.00057466
v  epsilon                0.069744          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099183      0.00092539       0.0017429
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017911          5.2779         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71352         0.85284


 TIME FOR THE TIME STEP            11246:        0.65492E+02

===============================================================


 INSTANT    0.112470000E-01   TIME STEP NUMBER           11247
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.207964393E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.524295732E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.196595591E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.154515607E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.376397170E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69763E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81357E-03   0.44918E-02 0.19847E+01 
c  Velocity[X]                                      0.13688E-03 
c  Velocity[Y]                                      0.12774E-03 
c  Velocity[Z]                                      0.42272E-02 
c  Pressure     0.35980E-04     133   0.91612E-02   0.25377E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56930E-08   0.16058E-08 0.99016E-01 
c  r22          0.10853E-01      13   0.54336E-08   0.18008E-08 0.10105E+00 
c  r33          0.21862E-01      14   0.70566E-08   0.12296E-07 0.12670E+00 
c  r12          0.93881E-03      18   0.58239E-08   0.28802E-09 0.59914E+00 
c  r13          0.46679E-02      19   0.55624E-08   0.14778E-08 0.19987E+00 
c  r23          0.39980E-02      19   0.56683E-08   0.12524E-08 0.19751E+00 
c  epsilon      0.10969E+02      11   0.33894E-08   0.96376E-02 0.16335E+00 
c  TempC        0.25716E+06      16   0.15118E-04   0.84485E-02 0.43365E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361          0.6138       0.0052571       0.0015074
v  Velocity[Y]            -0.57358         0.54401       0.0030779      0.00087208
v  Velocity[Z]              1.5657          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4414          4.3406          4.3632
v  Pressure                -36.393          360.04          87.654          169.87
v  r11                   0.0010625        0.081867        0.013077        0.018287
v  r22                   0.0011164        0.082597        0.013357        0.018647
v  r33                   0.0016452         0.17434        0.027256        0.037209
v  r12                   -0.010671        0.013567     -0.00023389     -0.00030934
v  r13                   -0.045502        0.052774      9.3397e-05       0.0010139
v  r23                   -0.046714        0.051201      3.0609e-05      0.00057466
v  epsilon                0.069745          271.18          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099182      0.00092539       0.0017429
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017912          5.2781         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71353         0.85284


 TIME FOR THE TIME STEP            11247:        0.64997E+02

===============================================================


 INSTANT    0.112480000E-01   TIME STEP NUMBER           11248
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.532311098E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.182558700E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.116778979E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.714461490E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.506651737E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81339E-03   0.44610E-02 0.19761E+01 
c  Velocity[X]                                      0.13687E-03 
c  Velocity[Y]                                      0.12676E-03 
c  Velocity[Z]                                      0.41974E-02 
c  Pressure     0.36226E-04     133   0.92256E-02   0.25550E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.50806E-08   0.16223E-08 0.99017E-01 
c  r22          0.10853E-01      13   0.49242E-08   0.18158E-08 0.10134E+00 
c  r33          0.21862E-01      14   0.64983E-08   0.12427E-07 0.12692E+00 
c  r12          0.93881E-03      18   0.57046E-08   0.29405E-09 0.60265E+00 
c  r13          0.46679E-02      19   0.58076E-08   0.14827E-08 0.19951E+00 
c  r23          0.39980E-02      19   0.62444E-08   0.12739E-08 0.19815E+00 
c  epsilon      0.10969E+02      11   0.32998E-08   0.97997E-02 0.16524E+00 
c  TempC        0.25716E+06      16   0.15168E-04   0.83541E-02 0.43118E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364         0.61386       0.0052571       0.0015073
v  Velocity[Y]            -0.57351         0.54414       0.0030779      0.00087206
v  Velocity[Z]              1.5658          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4414          4.3406          4.3632
v  Pressure                -36.447          359.99          87.631          169.83
v  r11                   0.0010625        0.081867        0.013077        0.018287
v  r22                   0.0011164        0.082598        0.013357        0.018647
v  r33                   0.0016452         0.17436        0.027256        0.037209
v  r12                    -0.01067        0.013573     -0.00023389     -0.00030934
v  r13                   -0.045505        0.052776      9.3397e-05       0.0010139
v  r23                   -0.046714        0.051188      3.0609e-05      0.00057466
v  epsilon                0.069747           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099175      0.00092539       0.0017429
v  CourantNb               0.44233             0.6         0.59908         0.59839
v  FourierNb             0.0017912          5.2778         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85284


 TIME FOR THE TIME STEP            11248:        0.64364E+02

===============================================================


 INSTANT    0.112490000E-01   TIME STEP NUMBER           11249
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.151616884E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203853133E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117114652E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.407406418E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.858207059E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81195E-03   0.45473E-02 0.19952E+01 
c  Velocity[X]                                      0.13862E-03 
c  Velocity[Y]                                      0.12837E-03 
c  Velocity[Z]                                      0.42803E-02 
c  Pressure     0.36772E-04     131   0.93628E-02   0.25936E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.50174E-08   0.16329E-08 0.99031E-01 
c  r22          0.10853E-01      13   0.48913E-08   0.18697E-08 0.10224E+00 
c  r33          0.21862E-01      14   0.67063E-08   0.12634E-07 0.12733E+00 
c  r12          0.93881E-03      18   0.59118E-08   0.29569E-09 0.60174E+00 
c  r13          0.46679E-02      19   0.63544E-08   0.15126E-08 0.20047E+00 
c  r23          0.39980E-02      19   0.63876E-08   0.12871E-08 0.19835E+00 
c  epsilon      0.10969E+02      11   0.32271E-08   0.99848E-02 0.16519E+00 
c  TempC        0.25716E+06      16   0.15166E-04   0.84345E-02 0.43305E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61385       0.0052571       0.0015073
v  Velocity[Y]            -0.57349         0.54397        0.003078      0.00087212
v  Velocity[Z]               1.566          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4414          4.3406          4.3632
v  Pressure                -36.416          360.01          87.649          169.85
v  r11                   0.0010626        0.081867        0.013077        0.018287
v  r22                   0.0011164        0.082595        0.013357        0.018647
v  r33                   0.0016452         0.17438        0.027256        0.037209
v  r12                   -0.010668        0.013575     -0.00023389     -0.00030934
v  r13                   -0.045504        0.052776      9.3398e-05       0.0010139
v  r23                   -0.046714        0.051212      3.0608e-05      0.00057466
v  epsilon                0.069748          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099177      0.00092539       0.0017429
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017912          5.2775         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71353         0.85284


 TIME FOR THE TIME STEP            11249:        0.64966E+02

===============================================================


 INSTANT    0.112500000E-01   TIME STEP NUMBER           11250
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.334151763E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.586815926E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149052636E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.140889832E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.380963326E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81417E-03   0.44930E-02 0.19859E+01 
c  Velocity[X]                                      0.13696E-03 
c  Velocity[Y]                                      0.12765E-03 
c  Velocity[Z]                                      0.42284E-02 
c  Pressure     0.36336E-04     132   0.92520E-02   0.25628E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52313E-08   0.16322E-08 0.99420E-01 
c  r22          0.10853E-01      13   0.46447E-08   0.18349E-08 0.10169E+00 
c  r33          0.21862E-01      14   0.68813E-08   0.12558E-07 0.12764E+00 
c  r12          0.93881E-03      18   0.61947E-08   0.29745E-09 0.60654E+00 
c  r13          0.46679E-02      19   0.58494E-08   0.15021E-08 0.20035E+00 
c  r23          0.39980E-02      19   0.62745E-08   0.12826E-08 0.19937E+00 
c  epsilon      0.10969E+02      11   0.32807E-08   0.10149E-01 0.17055E+00 
c  TempC        0.25716E+06      16   0.15157E-04   0.84472E-02 0.43359E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162016


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63354          0.6138       0.0052571       0.0015074
v  Velocity[Y]            -0.57347         0.54401       0.0030779      0.00087208
v  Velocity[Z]              1.5658          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4414          4.3406          4.3632
v  Pressure                -36.427          360.03          87.664          169.86
v  r11                   0.0010626        0.081872        0.013077        0.018287
v  r22                   0.0011164        0.082598        0.013357        0.018647
v  r33                   0.0016452         0.17439        0.027256        0.037209
v  r12                   -0.010667        0.013574     -0.00023389     -0.00030934
v  r13                   -0.045503        0.052776      9.3399e-05       0.0010139
v  r23                   -0.046714          0.0512      3.0608e-05      0.00057466
v  epsilon                0.069749          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9915e-05       0.0099177      0.00092539       0.0017429
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017912          5.2775         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71352         0.85284


 TIME FOR THE TIME STEP            11250:        0.70651E+02

===============================================================


 INSTANT    0.112510000E-01   TIME STEP NUMBER           11251
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.353505068E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.490155099E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.366264356E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935026E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.180987765E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.458488891E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81312E-03   0.44641E-02 0.19788E+01 
c  Velocity[X]                                      0.13644E-03 
c  Velocity[Y]                                      0.12670E-03 
c  Velocity[Z]                                      0.42010E-02 
c  Pressure     0.36262E-04     132   0.92263E-02   0.25577E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52203E-08   0.16144E-08 0.98816E-01 
c  r22          0.10853E-01      13   0.50210E-08   0.18110E-08 0.10096E+00 
c  r33          0.21862E-01      15   0.55238E-08   0.12308E-07 0.12650E+00 
c  r12          0.93881E-03      18   0.67558E-08   0.29436E-09 0.60331E+00 
c  r13          0.46679E-02      19   0.67669E-08   0.14748E-08 0.19912E+00 
c  r23          0.39980E-02      19   0.62471E-08   0.12538E-08 0.19715E+00 
c  epsilon      0.10969E+02      11   0.34246E-08   0.95138E-02 0.16177E+00 
c  TempC        0.25716E+06      16   0.15137E-04   0.83163E-02 0.43033E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63349         0.61386       0.0052571       0.0015074
v  Velocity[Y]            -0.57355         0.54372        0.003078      0.00087212
v  Velocity[Z]              1.5658          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4414          4.3406          4.3632
v  Pressure                -36.401          359.95          87.582          169.79
v  r11                   0.0010626        0.081877        0.013077        0.018287
v  r22                   0.0011164          0.0826        0.013357        0.018647
v  r33                   0.0016453         0.17436        0.027256        0.037209
v  r12                   -0.010665        0.013579     -0.00023389     -0.00030934
v  r13                   -0.045505        0.052774      9.3399e-05       0.0010139
v  r23                   -0.046715         0.05119      3.0608e-05      0.00057466
v  epsilon                 0.06975          271.17          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9917e-05       0.0099178      0.00092539       0.0017429
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017913          5.2778         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71353         0.85284


 TIME FOR THE TIME STEP            11251:        0.68499E+02

===============================================================


 INSTANT    0.112520000E-01   TIME STEP NUMBER           11252
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.287217624E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.300170922E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934891E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.107111466E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934932E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.237626165E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.384635199E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11558E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15639E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81219E-03   0.44929E-02 0.19864E+01 
c  Velocity[X]                                      0.13731E-03 
c  Velocity[Y]                                      0.12789E-03 
c  Velocity[Z]                                      0.42277E-02 
c  Pressure     0.36159E-04     132   0.92103E-02   0.25503E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54919E-08   0.15950E-08 0.97989E-01 
c  r22          0.10853E-01      13   0.50326E-08   0.18025E-08 0.10056E+00 
c  r33          0.21862E-01      15   0.52844E-08   0.12333E-07 0.12619E+00 
c  r12          0.93881E-03      18   0.64133E-08   0.29301E-09 0.60170E+00 
c  r13          0.46679E-02      19   0.59250E-08   0.14700E-08 0.19881E+00 
c  r23          0.39980E-02      19   0.56503E-08   0.12715E-08 0.19756E+00 
c  epsilon      0.10969E+02      11   0.34818E-08   0.99116E-02 0.16638E+00 
c  TempC        0.25716E+06      16   0.15166E-04   0.83907E-02 0.43226E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162015


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63354         0.61381        0.005257       0.0015073
v  Velocity[Y]            -0.57347         0.54325        0.003078      0.00087209
v  Velocity[Z]              1.5657          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4414          4.3406          4.3632
v  Pressure                 -36.44          359.99          87.637          169.83
v  r11                   0.0010626        0.081877        0.013077        0.018287
v  r22                   0.0011164          0.0826        0.013357        0.018647
v  r33                   0.0016453         0.17431        0.027256        0.037209
v  r12                   -0.010666        0.013578     -0.00023389     -0.00030934
v  r13                   -0.045503        0.052772      9.3399e-05       0.0010139
v  r23                   -0.046714        0.051205      3.0608e-05      0.00057466
v  epsilon                0.069752           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9919e-05       0.0099176      0.00092539       0.0017429
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017913          5.2776         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11252:        0.70039E+02

===============================================================


 INSTANT    0.112530000E-01   TIME STEP NUMBER           11253
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.766213713E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.561027475E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934917E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.224518937E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158580254E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.425035510E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15638E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81269E-03   0.45296E-02 0.19932E+01 
c  Velocity[X]                                      0.13829E-03 
c  Velocity[Y]                                      0.12772E-03 
c  Velocity[Z]                                      0.42636E-02 
c  Pressure     0.36529E-04     132   0.92988E-02   0.25764E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54636E-08   0.16027E-08 0.98622E-01 
c  r22          0.10853E-01      13   0.47967E-08   0.18088E-08 0.10084E+00 
c  r33          0.21862E-01      15   0.59822E-08   0.12239E-07 0.12612E+00 
c  r12          0.93881E-03      18   0.56982E-08   0.29045E-09 0.59955E+00 
c  r13          0.46679E-02      19   0.72147E-08   0.14713E-08 0.19866E+00 
c  r23          0.39980E-02      19   0.58595E-08   0.12402E-08 0.19652E+00 
c  epsilon      0.10969E+02      11   0.34100E-08   0.97720E-02 0.16499E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.84373E-02 0.43374E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162005


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63362         0.61377        0.005257       0.0015073
v  Velocity[Y]             -0.5735         0.54326        0.003078      0.00087209
v  Velocity[Z]              1.5659          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4414          4.3406          4.3632
v  Pressure                 -36.38          360.05           87.69          169.89
v  r11                   0.0010626        0.081876        0.013077        0.018287
v  r22                   0.0011164        0.082599        0.013357        0.018647
v  r33                   0.0016453         0.17431        0.027256        0.037209
v  r12                   -0.010661        0.013582     -0.00023389     -0.00030934
v  r13                   -0.045503        0.052769        9.34e-05       0.0010139
v  r23                   -0.046714        0.051195      3.0608e-05      0.00057466
v  epsilon                0.069753          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099175      0.00092539       0.0017429
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017913          5.2775         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71353         0.85285


 TIME FOR THE TIME STEP            11253:        0.70299E+02

===============================================================


 INSTANT    0.112540000E-01   TIME STEP NUMBER           11254
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.290328777E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934933E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.601896319E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.862940204E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.134813841E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.203392900E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11557E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81372E-03   0.44952E-02 0.19851E+01 
c  Velocity[X]                                      0.13693E-03 
c  Velocity[Y]                                      0.12698E-03 
c  Velocity[Z]                                      0.42313E-02 
c  Pressure     0.35882E-04     133   0.91320E-02   0.25308E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60198E-08   0.16484E-08 0.99250E-01 
c  r22          0.10853E-01      13   0.46993E-08   0.18258E-08 0.10118E+00 
c  r33          0.21862E-01      15   0.59609E-08   0.12507E-07 0.12684E+00 
c  r12          0.93881E-03      18   0.57478E-08   0.29177E-09 0.60286E+00 
c  r13          0.46679E-02      19   0.73321E-08   0.14820E-08 0.19935E+00 
c  r23          0.39980E-02      19   0.60531E-08   0.12741E-08 0.19830E+00 
c  epsilon      0.10969E+02      11   0.34762E-08   0.99977E-02 0.16659E+00 
c  TempC        0.25716E+06      16   0.15156E-04   0.83965E-02 0.43185E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61386        0.005257       0.0015073
v  Velocity[Y]            -0.57345         0.54294        0.003078      0.00087209
v  Velocity[Z]              1.5659          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4414          4.3406          4.3632
v  Pressure                -36.415          359.99          87.647          169.84
v  r11                   0.0010626         0.08188        0.013077        0.018287
v  r22                   0.0011164        0.082597        0.013357        0.018647
v  r33                   0.0016453         0.17433        0.027256        0.037209
v  r12                   -0.010659        0.013578     -0.00023389     -0.00030934
v  r13                   -0.045505         0.05277        9.34e-05       0.0010139
v  r23                   -0.046715        0.051175      3.0608e-05      0.00057466
v  epsilon                0.069755          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05       0.0099174       0.0009254       0.0017429
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017913          5.2778         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71352         0.85284


 TIME FOR THE TIME STEP            11254:        0.68540E+02

===============================================================


 INSTANT    0.112550000E-01   TIME STEP NUMBER           11255
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.175525136E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.365522613E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.498809593E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.124095539E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.144853275E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15637E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81173E-03   0.44714E-02 0.19820E+01 
c  Velocity[X]                                      0.13696E-03 
c  Velocity[Y]                                      0.12787E-03 
c  Velocity[Z]                                      0.42065E-02 
c  Pressure     0.36403E-04     132   0.92666E-02   0.25675E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.63468E-08   0.16152E-08 0.98164E-01 
c  r22          0.10853E-01      13   0.48828E-08   0.18093E-08 0.10060E+00 
c  r33          0.21862E-01      15   0.58044E-08   0.12441E-07 0.12605E+00 
c  r12          0.93881E-03      18   0.66512E-08   0.29533E-09 0.60050E+00 
c  r13          0.46679E-02      19   0.64217E-08   0.14958E-08 0.19927E+00 
c  r23          0.39980E-02      19   0.55256E-08   0.12856E-08 0.19751E+00 
c  epsilon      0.10969E+02      11   0.35147E-08   0.98579E-02 0.16480E+00 
c  TempC        0.25716E+06      16   0.15106E-04   0.84183E-02 0.43243E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63348         0.61381       0.0052571       0.0015073
v  Velocity[Y]            -0.57349         0.54305        0.003078      0.00087209
v  Velocity[Z]              1.5658          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4414          4.3406          4.3632
v  Pressure                -36.412          360.02          87.647          169.86
v  r11                   0.0010626        0.081877        0.013077        0.018287
v  r22                   0.0011164        0.082597        0.013357        0.018647
v  r33                   0.0016453         0.17435        0.027256        0.037209
v  r12                   -0.010661        0.013577     -0.00023389     -0.00030934
v  r13                   -0.045503         0.05277      9.3401e-05       0.0010139
v  r23                   -0.046714        0.051189      3.0607e-05      0.00057466
v  epsilon                0.069756          271.18          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9926e-05       0.0099175       0.0009254       0.0017429
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017914          5.2782         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            11255:        0.71841E+02

===============================================================


 INSTANT    0.112560000E-01   TIME STEP NUMBER           11256
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.267514108E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136787348E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.754617720E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.114557778E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188970625E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81377E-03   0.44809E-02 0.19810E+01 
c  Velocity[X]                                      0.13710E-03 
c  Velocity[Y]                                      0.12727E-03 
c  Velocity[Z]                                      0.42166E-02 
c  Pressure     0.36320E-04     132   0.92457E-02   0.25617E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60577E-08   0.16373E-08 0.98965E-01 
c  r22          0.10853E-01      13   0.53437E-08   0.18226E-08 0.10062E+00 
c  r33          0.21862E-01      15   0.66524E-08   0.12654E-07 0.12691E+00 
c  r12          0.93881E-03      18   0.66142E-08   0.29965E-09 0.60640E+00 
c  r13          0.46679E-02      20   0.57672E-08   0.15134E-08 0.19985E+00 
c  r23          0.39980E-02      19   0.50984E-08   0.12976E-08 0.19962E+00 
c  epsilon      0.10969E+02      11   0.35280E-08   0.10524E-01 0.17320E+00 
c  TempC        0.25716E+06      16   0.15181E-04   0.83848E-02 0.43299E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63351         0.61377       0.0052572       0.0015073
v  Velocity[Y]            -0.57342         0.54295        0.003078      0.00087208
v  Velocity[Z]              1.5658          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4414          4.3406          4.3632
v  Pressure                -36.429          360.03          87.676          169.87
v  r11                   0.0010626        0.081874        0.013077        0.018287
v  r22                   0.0011165        0.082597        0.013357        0.018647
v  r33                   0.0016453         0.17437        0.027256        0.037209
v  r12                   -0.010663        0.013575     -0.00023389     -0.00030934
v  r13                   -0.045502        0.052771      9.3402e-05       0.0010139
v  r23                   -0.046714        0.051166      3.0608e-05      0.00057466
v  epsilon                0.069757          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05       0.0099175       0.0009254       0.0017429
v  CourantNb               0.44229             0.6         0.59908         0.59839
v  FourierNb             0.0017914          5.2786         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8786         0.71353         0.85284


 TIME FOR THE TIME STEP            11256:        0.71442E+02

===============================================================


 INSTANT    0.112570000E-01   TIME STEP NUMBER           11257
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149498785E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172986412E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.276966213E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.847822098E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.173737414E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81187E-03   0.44720E-02 0.19801E+01 
c  Velocity[X]                                      0.13609E-03 
c  Velocity[Y]                                      0.12744E-03 
c  Velocity[Z]                                      0.42085E-02 
c  Pressure     0.36229E-04     134   0.92158E-02   0.25552E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61707E-08   0.16194E-08 0.98722E-01 
c  r22          0.10853E-01      13   0.53136E-08   0.17964E-08 0.99970E-01 
c  r33          0.21862E-01      14   0.70461E-08   0.12277E-07 0.12535E+00 
c  r12          0.93881E-03      18   0.63049E-08   0.29690E-09 0.60122E+00 
c  r13          0.46679E-02      19   0.67414E-08   0.14697E-08 0.19732E+00 
c  r23          0.39980E-02      19   0.52196E-08   0.12689E-08 0.19655E+00 
c  epsilon      0.10969E+02      11   0.34734E-08   0.95701E-02 0.16267E+00 
c  TempC        0.25716E+06      16   0.15145E-04   0.83244E-02 0.43014E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353         0.61383        0.005257       0.0015073
v  Velocity[Y]            -0.57354         0.54296       0.0030779      0.00087206
v  Velocity[Z]              1.5659          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4414          4.3406          4.3632
v  Pressure                -36.391          360.03           87.64          169.85
v  r11                   0.0010626        0.081866        0.013077        0.018287
v  r22                   0.0011165        0.082594        0.013357        0.018647
v  r33                   0.0016453         0.17439        0.027256        0.037209
v  r12                   -0.010664        0.013579     -0.00023389     -0.00030934
v  r13                   -0.045506        0.052771      9.3402e-05       0.0010139
v  r23                   -0.046714        0.051163      3.0608e-05      0.00057466
v  epsilon                0.069758          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9923e-05       0.0099175       0.0009254       0.0017429
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017914          5.2789         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            11257:        0.69656E+02

===============================================================


 INSTANT    0.112580000E-01   TIME STEP NUMBER           11258
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.309653497E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.328967226E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.982283200E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.801347339E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.286088469E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81354E-03   0.45094E-02 0.19889E+01 
c  Velocity[X]                                      0.13729E-03 
c  Velocity[Y]                                      0.12803E-03 
c  Velocity[Z]                                      0.42440E-02 
c  Pressure     0.36288E-04     132   0.92380E-02   0.25595E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.61883E-08   0.15966E-08 0.98061E-01 
c  r22          0.10853E-01      13   0.53779E-08   0.17765E-08 0.99945E-01 
c  r33          0.21862E-01      15   0.62124E-08   0.12184E-07 0.12562E+00 
c  r12          0.93881E-03      18   0.57528E-08   0.29647E-09 0.60569E+00 
c  r13          0.46679E-02      20   0.57977E-08   0.14615E-08 0.19786E+00 
c  r23          0.39980E-02      19   0.60815E-08   0.12743E-08 0.19751E+00 
c  epsilon      0.10969E+02      11   0.34624E-08   0.93698E-02 0.16126E+00 
c  TempC        0.25716E+06      16   0.15158E-04   0.83795E-02 0.43176E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361         0.61383       0.0052571       0.0015073
v  Velocity[Y]             -0.5734         0.54311       0.0030779      0.00087206
v  Velocity[Z]              1.5659          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5797          5.4414          4.3406          4.3632
v  Pressure                 -36.43          359.96          87.631          169.81
v  r11                   0.0010626        0.081858        0.013077        0.018287
v  r22                   0.0011165        0.082596        0.013357        0.018647
v  r33                   0.0016453         0.17435        0.027256        0.037209
v  r12                   -0.010665        0.013582     -0.00023389     -0.00030934
v  r13                   -0.045503         0.05277      9.3402e-05       0.0010139
v  r23                   -0.046714         0.05116      3.0607e-05      0.00057466
v  epsilon                 0.06976          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099176       0.0009254       0.0017429
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017914          5.2792         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8792         0.71353         0.85284


 TIME FOR THE TIME STEP            11258:        0.70556E+02

===============================================================


 INSTANT    0.112590000E-01   TIME STEP NUMBER           11259
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.233873176E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.161757871E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.845623907E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.121421105E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.119909822E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69764E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81250E-03   0.45094E-02 0.19883E+01 
c  Velocity[X]                                      0.13759E-03 
c  Velocity[Y]                                      0.12820E-03 
c  Velocity[Z]                                      0.42436E-02 
c  Pressure     0.36237E-04     131   0.92263E-02   0.25559E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.63509E-08   0.16030E-08 0.97801E-01 
c  r22          0.10853E-01      13   0.52550E-08   0.18396E-08 0.10039E+00 
c  r33          0.21862E-01      15   0.56680E-08   0.12515E-07 0.12617E+00 
c  r12          0.93881E-03      18   0.61423E-08   0.29091E-09 0.59875E+00 
c  r13          0.46679E-02      20   0.58990E-08   0.15087E-08 0.19908E+00 
c  r23          0.39980E-02      19   0.56978E-08   0.12600E-08 0.19643E+00 
c  epsilon      0.10969E+02      11   0.33608E-08   0.10053E-01 0.16541E+00 
c  TempC        0.25716E+06      16   0.15128E-04   0.84633E-02 0.43395E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63345         0.61379       0.0052571       0.0015074
v  Velocity[Y]            -0.57339         0.54304        0.003078       0.0008721
v  Velocity[Z]              1.5658          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4414          4.3406          4.3632
v  Pressure                -36.397          360.01          87.626          169.84
v  r11                   0.0010626        0.081858        0.013077        0.018287
v  r22                   0.0011165        0.082596        0.013357        0.018647
v  r33                   0.0016453         0.17431        0.027256        0.037209
v  r12                   -0.010664        0.013581     -0.00023389     -0.00030934
v  r13                   -0.045502        0.052765      9.3402e-05       0.0010139
v  r23                   -0.046714         0.05119      3.0607e-05      0.00057466
v  epsilon                0.069761           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099176       0.0009254       0.0017429
v  CourantNb               0.44225             0.6         0.59908         0.59839
v  FourierNb             0.0017915          5.2787         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8787         0.71352         0.85284


 TIME FOR THE TIME STEP            11259:        0.68780E+02

===============================================================


 INSTANT    0.112600000E-01   TIME STEP NUMBER           11260
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.203523279E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.593277023E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123527142E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.371946226E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.328583193E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81416E-03   0.44697E-02 0.19800E+01 
c  Velocity[X]                                      0.13684E-03 
c  Velocity[Y]                                      0.12703E-03 
c  Velocity[Z]                                      0.42059E-02 
c  Pressure     0.36206E-04     132   0.92171E-02   0.25537E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.58158E-08   0.16206E-08 0.97939E-01 
c  r22          0.10853E-01      13   0.53013E-08   0.18222E-08 0.10050E+00 
c  r33          0.21862E-01      15   0.75187E-08   0.12470E-07 0.12590E+00 
c  r12          0.93881E-03      18   0.59519E-08   0.29452E-09 0.60012E+00 
c  r13          0.46679E-02      20   0.74383E-08   0.15053E-08 0.19936E+00 
c  r23          0.39980E-02      19   0.55702E-08   0.12835E-08 0.19708E+00 
c  epsilon      0.10969E+02      11   0.36052E-08   0.99540E-02 0.16571E+00 
c  TempC        0.25716E+06      16   0.15154E-04   0.83668E-02 0.43199E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61385        0.005257       0.0015073
v  Velocity[Y]            -0.57327         0.54326        0.003078       0.0008721
v  Velocity[Z]              1.5655          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4414          4.3406          4.3632
v  Pressure                -36.432          360.07          87.681          169.89
v  r11                   0.0010626        0.081855        0.013077        0.018287
v  r22                   0.0011165        0.082596        0.013357        0.018647
v  r33                   0.0016453          0.1743        0.027256        0.037209
v  r12                   -0.010665        0.013587     -0.00023389     -0.00030934
v  r13                   -0.045505        0.052766      9.3402e-05       0.0010139
v  r23                   -0.046713        0.051185      3.0607e-05      0.00057466
v  epsilon                0.069763          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9917e-05       0.0099177       0.0009254       0.0017429
v  CourantNb               0.44223             0.6         0.59908         0.59839
v  FourierNb             0.0017915           5.278         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            11260:        0.69194E+02

===============================================================


 INSTANT    0.112610000E-01   TIME STEP NUMBER           11261
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.526452224E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.387172089E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.426112537E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158777075E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.235575286E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81215E-03   0.45339E-02 0.19910E+01 
c  Velocity[X]                                      0.13728E-03 
c  Velocity[Y]                                      0.12750E-03 
c  Velocity[Z]                                      0.42691E-02 
c  Pressure     0.35903E-04     131   0.91397E-02   0.25323E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55343E-08   0.16373E-08 0.98237E-01 
c  r22          0.10853E-01      13   0.54616E-08   0.18030E-08 0.99913E-01 
c  r33          0.21862E-01      15   0.59919E-08   0.12478E-07 0.12572E+00 
c  r12          0.93881E-03      18   0.54898E-08   0.29328E-09 0.60159E+00 
c  r13          0.46679E-02      19   0.72519E-08   0.14682E-08 0.19764E+00 
c  r23          0.39980E-02      19   0.58761E-08   0.12876E-08 0.19758E+00 
c  epsilon      0.10969E+02      11   0.34449E-08   0.10034E-01 0.16532E+00 
c  TempC        0.25716E+06      16   0.15173E-04   0.83756E-02 0.43216E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63354         0.61383        0.005257       0.0015073
v  Velocity[Y]            -0.57344         0.54361       0.0030779      0.00087209
v  Velocity[Z]              1.5657          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4414          4.3406          4.3632
v  Pressure                -36.406          360.01           87.64          169.84
v  r11                   0.0010626        0.081858        0.013077        0.018287
v  r22                   0.0011165        0.082596        0.013357        0.018647
v  r33                   0.0016453         0.17432        0.027256        0.037209
v  r12                   -0.010666        0.013582     -0.00023389     -0.00030934
v  r13                   -0.045505        0.052767      9.3403e-05       0.0010139
v  r23                   -0.046712        0.051184      3.0606e-05      0.00057466
v  epsilon                0.069764          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9916e-05       0.0099176       0.0009254       0.0017429
v  CourantNb               0.44226             0.6         0.59908         0.59839
v  FourierNb             0.0017915          5.2772         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85284


 TIME FOR THE TIME STEP            11261:        0.18818E+03

===============================================================


 INSTANT    0.112620000E-01   TIME STEP NUMBER           11262
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.231769007E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.438335040E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.307561521E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.649637621E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.133781641E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81280E-03   0.44961E-02 0.19848E+01 
c  Velocity[X]                                      0.13626E-03 
c  Velocity[Y]                                      0.12810E-03 
c  Velocity[Z]                                      0.42317E-02 
c  Pressure     0.36191E-04     133   0.92133E-02   0.25526E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57543E-08   0.16352E-08 0.98935E-01 
c  r22          0.10853E-01      13   0.50167E-08   0.18123E-08 0.10027E+00 
c  r33          0.21862E-01      14   0.71476E-08   0.12498E-07 0.12661E+00 
c  r12          0.93881E-03      18   0.55283E-08   0.29936E-09 0.60723E+00 
c  r13          0.46679E-02      19   0.59010E-08   0.14990E-08 0.19939E+00 
c  r23          0.39980E-02      19   0.55514E-08   0.12965E-08 0.19971E+00 
c  epsilon      0.10969E+02      11   0.34123E-08   0.10153E-01 0.17168E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.83891E-02 0.43164E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63361          0.6138       0.0052571       0.0015074
v  Velocity[Y]            -0.57339         0.54389        0.003078      0.00087209
v  Velocity[Z]              1.5658          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4414          4.3406          4.3632
v  Pressure                 -36.45          359.99          87.638          169.83
v  r11                   0.0010626        0.081859        0.013077        0.018287
v  r22                   0.0011165        0.082596        0.013357        0.018647
v  r33                   0.0016453         0.17434        0.027257        0.037209
v  r12                   -0.010663        0.013575     -0.00023389     -0.00030934
v  r13                   -0.045503         0.05277      9.3403e-05       0.0010139
v  r23                   -0.046713        0.051169      3.0607e-05      0.00057466
v  epsilon                0.069765          271.26          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099177       0.0009254       0.0017429
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017915          5.2776         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11262:        0.15767E+03

===============================================================


 INSTANT    0.112630000E-01   TIME STEP NUMBER           11263
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.114442240E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.153002304E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.378972412E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.381829220E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.307104619E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81269E-03   0.44591E-02 0.19777E+01 
c  Velocity[X]                                      0.13749E-03 
c  Velocity[Y]                                      0.12734E-03 
c  Velocity[Z]                                      0.41943E-02 
c  Pressure     0.36269E-04     131   0.92292E-02   0.25581E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59050E-08   0.15927E-08 0.97273E-01 
c  r22          0.10853E-01      13   0.53268E-08   0.17980E-08 0.10010E+00 
c  r33          0.21862E-01      15   0.56298E-08   0.12276E-07 0.12535E+00 
c  r12          0.93881E-03      18   0.56574E-08   0.28833E-09 0.59826E+00 
c  r13          0.46679E-02      19   0.59050E-08   0.14798E-08 0.19840E+00 
c  r23          0.39980E-02      19   0.57595E-08   0.12556E-08 0.19509E+00 
c  epsilon      0.10969E+02      11   0.32732E-08   0.95044E-02 0.16214E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.83779E-02 0.43175E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162015


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63346         0.61385       0.0052571       0.0015074
v  Velocity[Y]            -0.57347         0.54413        0.003078      0.00087207
v  Velocity[Z]              1.5655          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4414          4.3406          4.3632
v  Pressure                 -36.42          360.02          87.638          169.85
v  r11                   0.0010626        0.081852        0.013077        0.018287
v  r22                   0.0011165        0.082593        0.013357        0.018647
v  r33                   0.0016453         0.17436        0.027257        0.037209
v  r12                   -0.010664        0.013579     -0.00023389     -0.00030934
v  r13                   -0.045505        0.052771      9.3402e-05       0.0010139
v  r23                   -0.046713        0.051203      3.0606e-05      0.00057466
v  epsilon                0.069767          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099177       0.0009254       0.0017429
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017916          5.2778         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8778         0.71353         0.85284


 TIME FOR THE TIME STEP            11263:        0.13776E+03

===============================================================


 INSTANT    0.112640000E-01   TIME STEP NUMBER           11264
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.261734273E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.147672560E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934915E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282266109E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.302818777E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.101638926E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81277E-03   0.45018E-02 0.19867E+01 
c  Velocity[X]                                      0.13702E-03 
c  Velocity[Y]                                      0.12763E-03 
c  Velocity[Z]                                      0.42372E-02 
c  Pressure     0.36401E-04     133   0.92722E-02   0.25674E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56967E-08   0.16388E-08 0.98271E-01 
c  r22          0.10853E-01      13   0.49728E-08   0.18116E-08 0.10045E+00 
c  r33          0.21862E-01      15   0.53373E-08   0.12512E-07 0.12620E+00 
c  r12          0.93881E-03      18   0.54141E-08   0.29885E-09 0.60512E+00 
c  r13          0.46679E-02      18   0.71038E-08   0.14975E-08 0.19944E+00 
c  r23          0.39980E-02      19   0.56451E-08   0.12939E-08 0.19793E+00 
c  epsilon      0.10969E+02      11   0.34464E-08   0.10099E-01 0.16639E+00 
c  TempC        0.25716E+06      16   0.15188E-04   0.84446E-02 0.43369E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162013


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347         0.61382        0.005257       0.0015073
v  Velocity[Y]            -0.57325         0.54398       0.0030779      0.00087203
v  Velocity[Z]              1.5656          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4414          4.3406          4.3632
v  Pressure                -36.466          360.01          87.655          169.85
v  r11                   0.0010626        0.081851        0.013077        0.018287
v  r22                   0.0011165        0.082597        0.013357        0.018647
v  r33                   0.0016453         0.17437        0.027257        0.037209
v  r12                   -0.010665         0.01358     -0.00023389     -0.00030934
v  r13                   -0.045503        0.052772      9.3403e-05       0.0010139
v  r23                   -0.046714        0.051194      3.0606e-05      0.00057466
v  epsilon                0.069768          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.991e-05       0.0099179       0.0009254       0.0017429
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017916          5.2779         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8779         0.71353         0.85284


 TIME FOR THE TIME STEP            11264:        0.12695E+03

===============================================================


 INSTANT    0.112650000E-01   TIME STEP NUMBER           11265
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.556481624E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.492608649E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.102447083E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.642214967E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.887161642E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81305E-03   0.45233E-02 0.19925E+01 
c  Velocity[X]                                      0.13808E-03 
c  Velocity[Y]                                      0.12780E-03 
c  Velocity[Z]                                      0.42574E-02 
c  Pressure     0.36566E-04     132   0.93021E-02   0.25791E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54289E-08   0.16041E-08 0.98240E-01 
c  r22          0.10853E-01      13   0.50875E-08   0.18125E-08 0.10053E+00 
c  r33          0.21862E-01      15   0.59933E-08   0.12331E-07 0.12607E+00 
c  r12          0.93881E-03      18   0.50072E-08   0.29094E-09 0.60174E+00 
c  r13          0.46679E-02      18   0.71608E-08   0.14998E-08 0.19959E+00 
c  r23          0.39980E-02      19   0.64475E-08   0.12685E-08 0.19708E+00 
c  epsilon      0.10969E+02      11   0.34729E-08   0.96029E-02 0.16329E+00 
c  TempC        0.25716E+06      16   0.15127E-04   0.83873E-02 0.43220E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63353          0.6138       0.0052571       0.0015073
v  Velocity[Y]            -0.57334         0.54395       0.0030779      0.00087204
v  Velocity[Z]              1.5656          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4414          4.3406          4.3632
v  Pressure                -36.401          360.03           87.65          169.86
v  r11                   0.0010626        0.081854        0.013077        0.018287
v  r22                   0.0011165        0.082599        0.013357        0.018647
v  r33                   0.0016454         0.17438        0.027257        0.037209
v  r12                   -0.010662        0.013578     -0.00023389     -0.00030934
v  r13                   -0.045503        0.052768      9.3403e-05       0.0010139
v  r23                   -0.046714        0.051182      3.0606e-05      0.00057466
v  epsilon                0.069769           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9909e-05       0.0099178       0.0009254       0.0017429
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017916          5.2784         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8784         0.71352         0.85284


 TIME FOR THE TIME STEP            11265:        0.91677E+02

===============================================================


 INSTANT    0.112660000E-01   TIME STEP NUMBER           11266
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.115911487E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.680566207E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.335375128E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.210697755E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.245095467E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934979E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11556E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15636E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10218E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81379E-03   0.45143E-02 0.19900E+01 
c  Velocity[X]                                      0.13653E-03 
c  Velocity[Y]                                      0.12733E-03 
c  Velocity[Z]                                      0.42505E-02 
c  Pressure     0.36239E-04     132   0.92290E-02   0.25560E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53208E-08   0.16252E-08 0.98561E-01 
c  r22          0.10853E-01      13   0.49501E-08   0.18064E-08 0.10027E+00 
c  r33          0.21862E-01      15   0.60635E-08   0.12403E-07 0.12613E+00 
c  r12          0.93881E-03      17   0.69901E-08   0.29443E-09 0.60016E+00 
c  r13          0.46679E-02      19   0.57943E-08   0.14949E-08 0.19902E+00 
c  r23          0.39980E-02      19   0.55408E-08   0.12686E-08 0.19689E+00 
c  epsilon      0.10969E+02      11   0.33737E-08   0.98780E-02 0.16633E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.83304E-02 0.43076E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162009


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63342         0.61385       0.0052571       0.0015074
v  Velocity[Y]            -0.57335         0.54402       0.0030779      0.00087204
v  Velocity[Z]              1.5657          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4414          4.3406          4.3632
v  Pressure                -36.441          359.96          87.613           169.8
v  r11                   0.0010626        0.081855        0.013077        0.018287
v  r22                   0.0011165          0.0826        0.013357        0.018647
v  r33                   0.0016454         0.17434        0.027257        0.037209
v  r12                   -0.010663        0.013583     -0.00023389     -0.00030934
v  r13                   -0.045507        0.052767      9.3404e-05       0.0010139
v  r23                   -0.046714        0.051201      3.0606e-05      0.00057466
v  epsilon                0.069771          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9906e-05       0.0099178       0.0009254       0.0017429
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017917          5.2776         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71352         0.85284


 TIME FOR THE TIME STEP            11266:        0.96518E+02

===============================================================


 INSTANT    0.112670000E-01   TIME STEP NUMBER           11267
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.166779016E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.275120162E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.560407290E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.503236348E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.303835294E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81178E-03   0.44791E-02 0.19834E+01 
c  Velocity[X]                                      0.13708E-03 
c  Velocity[Y]                                      0.12788E-03 
c  Velocity[Z]                                      0.42141E-02 
c  Pressure     0.36213E-04     133   0.92164E-02   0.25542E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.50875E-08   0.16219E-08 0.98127E-01 
c  r22          0.10853E-01      13   0.54545E-08   0.17972E-08 0.99805E-01 
c  r33          0.21862E-01      15   0.59605E-08   0.12444E-07 0.12591E+00 
c  r12          0.93882E-03      18   0.52141E-08   0.29510E-09 0.60169E+00 
c  r13          0.46679E-02      19   0.72402E-08   0.14850E-08 0.19812E+00 
c  r23          0.39980E-02      19   0.64584E-08   0.12855E-08 0.19728E+00 
c  epsilon      0.10969E+02      11   0.34689E-08   0.99523E-02 0.16605E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.83935E-02 0.43240E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6335         0.61381        0.005257       0.0015073
v  Velocity[Y]            -0.57345         0.54411       0.0030779      0.00087205
v  Velocity[Z]              1.5655          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4414          4.3406          4.3632
v  Pressure                -36.373          360.01           87.65          169.86
v  r11                   0.0010626        0.081857        0.013077        0.018287
v  r22                   0.0011165        0.082598        0.013357        0.018647
v  r33                   0.0016454          0.1743        0.027257        0.037209
v  r12                   -0.010665        0.013581     -0.00023389     -0.00030934
v  r13                   -0.045505        0.052767      9.3404e-05       0.0010139
v  r23                   -0.046714        0.051187      3.0606e-05      0.00057466
v  epsilon                0.069772          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9904e-05       0.0099178       0.0009254       0.0017429
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb             0.0017917          5.2764         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8764         0.71353         0.85284


 TIME FOR THE TIME STEP            11267:        0.17217E+03

===============================================================


 INSTANT    0.112680000E-01   TIME STEP NUMBER           11268
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.398392236E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.227442300E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.193738456E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.967295425E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.583789879E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81385E-03   0.44856E-02 0.19811E+01 
c  Velocity[X]                                      0.13692E-03 
c  Velocity[Y]                                      0.12810E-03 
c  Velocity[Z]                                      0.42206E-02 
c  Pressure     0.36280E-04     132   0.92357E-02   0.25590E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.49924E-08   0.16393E-08 0.98686E-01 
c  r22          0.10853E-01      13   0.52421E-08   0.18405E-08 0.10073E+00 
c  r33          0.21862E-01      15   0.57730E-08   0.12695E-07 0.12705E+00 
c  r12          0.93882E-03      17   0.66673E-08   0.29823E-09 0.60300E+00 
c  r13          0.46679E-02      19   0.58115E-08   0.15157E-08 0.19947E+00 
c  r23          0.39980E-02      19   0.56395E-08   0.12936E-08 0.19904E+00 
c  epsilon      0.10969E+02      11   0.33531E-08   0.10493E-01 0.17270E+00 
c  TempC        0.25716E+06      16   0.15160E-04   0.84684E-02 0.43429E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63364         0.61377       0.0052571       0.0015074
v  Velocity[Y]            -0.57348         0.54419       0.0030779      0.00087205
v  Velocity[Z]              1.5655          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4414          4.3406          4.3632
v  Pressure                -36.442          360.01          87.651          169.85
v  r11                   0.0010626        0.081854        0.013077        0.018287
v  r22                   0.0011165        0.082597        0.013357        0.018647
v  r33                   0.0016454          0.1743        0.027257        0.037209
v  r12                   -0.010664        0.013582     -0.00023389     -0.00030934
v  r13                   -0.045503        0.052769      9.3404e-05       0.0010139
v  r23                   -0.046714         0.05118      3.0606e-05      0.00057466
v  epsilon                0.069773          271.16          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9901e-05       0.0099177       0.0009254       0.0017429
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017917          5.2768         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71353         0.85284


 TIME FOR THE TIME STEP            11268:        0.10691E+03

===============================================================


 INSTANT    0.112690000E-01   TIME STEP NUMBER           11269
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.360852514E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.448382381E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.363851008E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934990E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.238678601E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.434408177E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81252E-03   0.45145E-02 0.19874E+01 
c  Velocity[X]                                      0.13695E-03 
c  Velocity[Y]                                      0.12731E-03 
c  Velocity[Z]                                      0.42503E-02 
c  Pressure     0.36720E-04     132   0.93491E-02   0.25900E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51764E-08   0.16174E-08 0.98301E-01 
c  r22          0.10853E-01      13   0.52382E-08   0.18074E-08 0.10055E+00 
c  r33          0.21862E-01      14   0.67757E-08   0.12380E-07 0.12626E+00 
c  r12          0.93882E-03      18   0.57018E-08   0.29147E-09 0.59672E+00 
c  r13          0.46679E-02      19   0.57633E-08   0.14793E-08 0.19875E+00 
c  r23          0.39980E-02      19   0.53784E-08   0.12638E-08 0.19690E+00 
c  epsilon      0.10969E+02      11   0.32784E-08   0.97600E-02 0.16373E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.83850E-02 0.43197E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61384       0.0052571       0.0015074
v  Velocity[Y]            -0.57358         0.54402       0.0030779      0.00087206
v  Velocity[Z]              1.5659          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4414          4.3406          4.3632
v  Pressure                -36.387          360.07          87.667          169.88
v  r11                   0.0010626        0.081857        0.013077        0.018287
v  r22                   0.0011165        0.082593        0.013357        0.018647
v  r33                   0.0016454         0.17432        0.027257        0.037209
v  r12                   -0.010659        0.013577     -0.00023389     -0.00030934
v  r13                   -0.045507        0.052773      9.3404e-05       0.0010139
v  r23                   -0.046714        0.051211      3.0606e-05      0.00057466
v  epsilon                0.069775          271.17          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9902e-05       0.0099178       0.0009254       0.0017429
v  CourantNb               0.44251             0.6         0.59908         0.59839
v  FourierNb             0.0017917          5.2772         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71353         0.85284


 TIME FOR THE TIME STEP            11269:        0.96030E+02

===============================================================


 INSTANT    0.112700000E-01   TIME STEP NUMBER           11270
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.799805210E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934946E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.330365862E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934914E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.354931579E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.196779542E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.102300575E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      40   0.81314E-03   0.44906E-02 0.19855E+01 
c  Velocity[X]                                      0.13691E-03 
c  Velocity[Y]                                      0.12699E-03 
c  Velocity[Z]                                      0.42267E-02 
c  Pressure     0.36471E-04     133   0.92888E-02   0.25724E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53066E-08   0.16407E-08 0.98591E-01 
c  r22          0.10853E-01      13   0.53623E-08   0.18442E-08 0.10089E+00 
c  r33          0.21862E-01      15   0.54228E-08   0.12627E-07 0.12671E+00 
c  r12          0.93882E-03      18   0.63321E-08   0.29336E-09 0.60038E+00 
c  r13          0.46679E-02      19   0.68997E-08   0.15183E-08 0.19989E+00 
c  r23          0.39980E-02      19   0.63529E-08   0.12831E-08 0.19804E+00 
c  epsilon      0.10969E+02      11   0.34888E-08   0.10218E-01 0.16738E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.83801E-02 0.43175E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61382       0.0052571       0.0015074
v  Velocity[Y]            -0.57337         0.54397       0.0030779      0.00087203
v  Velocity[Z]              1.5657          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4414          4.3406          4.3632
v  Pressure                -36.436          359.99           87.63          169.82
v  r11                   0.0010626        0.081863        0.013077        0.018287
v  r22                   0.0011165        0.082594        0.013357        0.018647
v  r33                   0.0016454         0.17434        0.027257        0.037209
v  r12                   -0.010662        0.013581     -0.00023389     -0.00030934
v  r13                   -0.045504        0.052777      9.3405e-05       0.0010139
v  r23                   -0.046715        0.051205      3.0606e-05      0.00057466
v  epsilon                0.069776           271.2          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9903e-05       0.0099179       0.0009254       0.0017429
v  CourantNb               0.44237             0.6         0.59908         0.59839
v  FourierNb             0.0017918          5.2782         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            11270:        0.93973E+02

===============================================================


 INSTANT    0.112710000E-01   TIME STEP NUMBER           11271
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.690752129E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.413330507E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.293991349E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.117935502E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.771651912E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12299E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69765E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81290E-03   0.44884E-02 0.19842E+01 
c  Velocity[X]                                      0.13835E-03 
c  Velocity[Y]                                      0.12812E-03 
c  Velocity[Z]                                      0.42219E-02 
c  Pressure     0.36078E-04     131   0.91855E-02   0.25446E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57797E-08   0.16251E-08 0.98598E-01 
c  r22          0.10853E-01      13   0.52052E-08   0.18447E-08 0.10067E+00 
c  r33          0.21862E-01      15   0.61251E-08   0.12594E-07 0.12659E+00 
c  r12          0.93882E-03      18   0.51136E-08   0.29667E-09 0.60333E+00 
c  r13          0.46679E-02      20   0.64673E-08   0.15031E-08 0.19920E+00 
c  r23          0.39980E-02      19   0.70314E-08   0.12655E-08 0.19728E+00 
c  epsilon      0.10969E+02      11   0.37214E-08   0.10287E-01 0.16846E+00 
c  TempC        0.25716E+06      16   0.15144E-04   0.84419E-02 0.43362E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61377       0.0052572       0.0015074
v  Velocity[Y]            -0.57338         0.54404       0.0030779      0.00087207
v  Velocity[Z]              1.5658          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4414          4.3406          4.3632
v  Pressure                -36.431          360.08          87.674           169.9
v  r11                   0.0010626         0.08186        0.013077        0.018287
v  r22                   0.0011165        0.082593        0.013357        0.018647
v  r33                   0.0016454         0.17436        0.027257        0.037209
v  r12                   -0.010662        0.013579     -0.00023389     -0.00030934
v  r13                   -0.045503        0.052775      9.3406e-05       0.0010139
v  r23                   -0.046716         0.05119      3.0606e-05      0.00057466
v  epsilon                0.069777          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9906e-05       0.0099179       0.0009254       0.0017429
v  CourantNb               0.44253             0.6         0.59908         0.59839
v  FourierNb             0.0017918          5.2789         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8789         0.71352         0.85284


 TIME FOR THE TIME STEP            11271:        0.90695E+02

===============================================================


 INSTANT    0.112720000E-01   TIME STEP NUMBER           11272
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.350601629E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.239680155E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934926E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.123045531E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.157616079E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.992400577E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12300E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      44   0.81377E-03   0.45106E-02 0.19880E+01 
c  Velocity[X]                                      0.13673E-03 
c  Velocity[Y]                                      0.12837E-03 
c  Velocity[Z]                                      0.42455E-02 
c  Pressure     0.36299E-04     131   0.92468E-02   0.25603E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57025E-08   0.16112E-08 0.97996E-01 
c  r22          0.10853E-01      13   0.52423E-08   0.18028E-08 0.10021E+00 
c  r33          0.21862E-01      15   0.67351E-08   0.12378E-07 0.12593E+00 
c  r12          0.93882E-03      18   0.58008E-08   0.29108E-09 0.60062E+00 
c  r13          0.46679E-02      20   0.64158E-08   0.14761E-08 0.19862E+00 
c  r23          0.39980E-02      20   0.60337E-08   0.12527E-08 0.19635E+00 
c  epsilon      0.10969E+02      11   0.35724E-08   0.99450E-02 0.16659E+00 
c  TempC        0.25716E+06      16   0.15178E-04   0.83352E-02 0.43088E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6336         0.61385       0.0052571       0.0015073
v  Velocity[Y]            -0.57338         0.54413       0.0030778      0.00087203
v  Velocity[Z]              1.5657          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4414          4.3406          4.3632
v  Pressure                -36.435             360          87.633          169.83
v  r11                   0.0010626        0.081852        0.013077        0.018287
v  r22                   0.0011165        0.082597        0.013357        0.018647
v  r33                   0.0016454         0.17438        0.027257        0.037209
v  r12                    -0.01066        0.013584     -0.00023389     -0.00030934
v  r13                   -0.045506        0.052775      9.3406e-05       0.0010139
v  r23                   -0.046716        0.051177      3.0606e-05      0.00057466
v  epsilon                0.069779          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9905e-05        0.009918       0.0009254       0.0017429
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017918          5.2796         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8796         0.71353         0.85284


 TIME FOR THE TIME STEP            11272:        0.95701E+02

===============================================================


 INSTANT    0.112730000E-01   TIME STEP NUMBER           11273
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.137336898E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.368639341E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.211851616E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195066967E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934957E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.323025135E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81290E-03   0.45188E-02 0.19905E+01 
c  Velocity[X]                                      0.13778E-03 
c  Velocity[Y]                                      0.12830E-03 
c  Velocity[Z]                                      0.42528E-02 
c  Pressure     0.36451E-04     132   0.92842E-02   0.25710E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53933E-08   0.16144E-08 0.98486E-01 
c  r22          0.10853E-01      13   0.49979E-08   0.17970E-08 0.10013E+00 
c  r33          0.21862E-01      15   0.64161E-08   0.12285E-07 0.12580E+00 
c  r12          0.93882E-03      18   0.56923E-08   0.29602E-09 0.60408E+00 
c  r13          0.46679E-02      19   0.53936E-08   0.14796E-08 0.19855E+00 
c  r23          0.39980E-02      19   0.56270E-08   0.12591E-08 0.19639E+00 
c  epsilon      0.10969E+02      11   0.33630E-08   0.96865E-02 0.16410E+00 
c  TempC        0.25716E+06      16   0.15151E-04   0.83946E-02 0.43291E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61382       0.0052571       0.0015073
v  Velocity[Y]            -0.57346         0.54392       0.0030779      0.00087204
v  Velocity[Z]              1.5656          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4414          4.3406          4.3632
v  Pressure                -36.396          360.01          87.634          169.83
v  r11                   0.0010626        0.081847        0.013077        0.018287
v  r22                   0.0011165        0.082599        0.013357        0.018647
v  r33                   0.0016454         0.17439        0.027257        0.037209
v  r12                   -0.010661        0.013587     -0.00023389     -0.00030934
v  r13                   -0.045506        0.052773      9.3406e-05       0.0010139
v  r23                   -0.046717        0.051201      3.0606e-05      0.00057466
v  epsilon                 0.06978          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9908e-05       0.0099178       0.0009254       0.0017429
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb             0.0017919          5.2795         0.11445         0.25446
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8795         0.71353         0.85285


 TIME FOR THE TIME STEP            11273:        0.90879E+02

===============================================================


 INSTANT    0.112740000E-01   TIME STEP NUMBER           11274
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.736411312E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.105490423E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.257968164E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.182965883E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.383601588E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15635E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81287E-03   0.45243E-02 0.19920E+01 
c  Velocity[X]                                      0.13759E-03 
c  Velocity[Y]                                      0.12816E-03 
c  Velocity[Z]                                      0.42586E-02 
c  Pressure     0.36388E-04     133   0.92596E-02   0.25666E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54145E-08   0.16529E-08 0.99733E-01 
c  r22          0.10853E-01      13   0.49548E-08   0.17951E-08 0.10044E+00 
c  r33          0.21862E-01      15   0.63849E-08   0.12483E-07 0.12713E+00 
c  r12          0.93882E-03      18   0.60141E-08   0.29845E-09 0.60527E+00 
c  r13          0.46679E-02      19   0.58938E-08   0.14767E-08 0.19895E+00 
c  r23          0.39980E-02      19   0.58319E-08   0.12865E-08 0.19928E+00 
c  epsilon      0.10969E+02      11   0.34294E-08   0.99365E-02 0.16906E+00 
c  TempC        0.25716E+06      16   0.15164E-04   0.83986E-02 0.43232E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63378         0.61377       0.0052571       0.0015074
v  Velocity[Y]            -0.57343         0.54386       0.0030779      0.00087204
v  Velocity[Z]              1.5658          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4414          4.3406          4.3632
v  Pressure                -36.451          360.05          87.695          169.89
v  r11                   0.0010626        0.081841        0.013077        0.018287
v  r22                   0.0011165          0.0826        0.013357        0.018647
v  r33                   0.0016454         0.17435        0.027257        0.037209
v  r12                   -0.010661        0.013587     -0.00023389     -0.00030935
v  r13                   -0.045504        0.052772      9.3406e-05       0.0010139
v  r23                   -0.046717        0.051182      3.0605e-05      0.00057466
v  epsilon                0.069781          271.18          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9911e-05       0.0099177       0.0009254       0.0017429
v  CourantNb               0.44249             0.6         0.59908         0.59839
v  FourierNb             0.0017919           5.279         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.879         0.71353         0.85285


 TIME FOR THE TIME STEP            11274:        0.10829E+03

===============================================================


 INSTANT    0.112750000E-01   TIME STEP NUMBER           11275
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.470789523E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.103096674E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935005E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.158305197E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.364335557E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.263803469E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81297E-03   0.44570E-02 0.19758E+01 
c  Velocity[X]                                      0.13641E-03 
c  Velocity[Y]                                      0.12744E-03 
c  Velocity[Z]                                      0.41932E-02 
c  Pressure     0.35663E-04     133   0.90779E-02   0.25153E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53036E-08   0.16300E-08 0.98730E-01 
c  r22          0.10853E-01      13   0.49825E-08   0.18315E-08 0.10069E+00 
c  r33          0.21862E-01      15   0.54806E-08   0.12576E-07 0.12685E+00 
c  r12          0.93882E-03      18   0.60847E-08   0.29361E-09 0.60052E+00 
c  r13          0.46679E-02      19   0.54391E-08   0.14937E-08 0.19907E+00 
c  r23          0.39980E-02      19   0.54617E-08   0.12821E-08 0.19857E+00 
c  epsilon      0.10969E+02      11   0.34773E-08   0.10066E-01 0.16666E+00 
c  TempC        0.25716E+06      16   0.15105E-04   0.83713E-02 0.43106E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63381         0.61385       0.0052571       0.0015074
v  Velocity[Y]            -0.57345         0.54392       0.0030779      0.00087204
v  Velocity[Z]              1.5659          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5796          5.4414          4.3406          4.3632
v  Pressure                -36.395          360.01          87.636          169.85
v  r11                   0.0010626        0.081834        0.013077        0.018287
v  r22                   0.0011165        0.082601        0.013357        0.018647
v  r33                   0.0016454         0.17431        0.027257        0.037209
v  r12                   -0.010659        0.013595     -0.00023389     -0.00030935
v  r13                   -0.045506        0.052774      9.3406e-05       0.0010139
v  r23                   -0.046717        0.051173      3.0605e-05      0.00057466
v  epsilon                0.069783          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099176       0.0009254       0.0017429
v  CourantNb               0.44257             0.6         0.59908         0.59839
v  FourierNb             0.0017919          5.2783         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71353         0.85284


 TIME FOR THE TIME STEP            11275:        0.12358E+03

===============================================================


 INSTANT    0.112760000E-01   TIME STEP NUMBER           11276
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.510576808E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.106934742E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934908E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.236857550E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.251491226E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.199156905E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11246E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81364E-03   0.44803E-02 0.19820E+01 
c  Velocity[X]                                      0.13652E-03 
c  Velocity[Y]                                      0.12770E-03 
c  Velocity[Z]                                      0.42161E-02 
c  Pressure     0.36246E-04     131   0.92289E-02   0.25564E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54907E-08   0.16171E-08 0.98724E-01 
c  r22          0.10853E-01      13   0.51431E-08   0.17980E-08 0.10048E+00 
c  r33          0.21862E-01      15   0.62765E-08   0.12341E-07 0.12633E+00 
c  r12          0.93882E-03      18   0.68934E-08   0.29109E-09 0.60131E+00 
c  r13          0.46679E-02      19   0.62738E-08   0.14874E-08 0.19951E+00 
c  r23          0.39980E-02      19   0.63630E-08   0.12638E-08 0.19767E+00 
c  epsilon      0.10969E+02      11   0.33743E-08   0.98087E-02 0.16458E+00 
c  TempC        0.25716E+06      16   0.15180E-04   0.84080E-02 0.43259E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384          0.6138       0.0052571       0.0015073
v  Velocity[Y]            -0.57334           0.544       0.0030778        0.000872
v  Velocity[Z]              1.5657          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4414          4.3406          4.3632
v  Pressure                -36.448          360.01          87.662          169.86
v  r11                   0.0010626        0.081825        0.013077        0.018287
v  r22                   0.0011165        0.082601        0.013357        0.018647
v  r33                   0.0016454          0.1743        0.027257        0.037209
v  r12                   -0.010659        0.013602     -0.00023389     -0.00030935
v  r13                   -0.045504        0.052777      9.3406e-05       0.0010139
v  r23                   -0.046717        0.051175      3.0604e-05      0.00057466
v  epsilon                0.069784          271.21          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099177       0.0009254       0.0017429
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017919          5.2775         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71352         0.85284


 TIME FOR THE TIME STEP            11276:        0.16502E+03

===============================================================


 INSTANT    0.112770000E-01   TIME STEP NUMBER           11277
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.849501402E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.195154252E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.288953713E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.412185492E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.127485386E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81244E-03   0.45134E-02 0.19887E+01 
c  Velocity[X]                                      0.13794E-03 
c  Velocity[Y]                                      0.12748E-03 
c  Velocity[Z]                                      0.42479E-02 
c  Pressure     0.36248E-04     131   0.92237E-02   0.25566E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.56599E-08   0.16184E-08 0.98238E-01 
c  r22          0.10853E-01      13   0.53604E-08   0.18133E-08 0.10035E+00 
c  r33          0.21862E-01      15   0.74988E-08   0.12445E-07 0.12596E+00 
c  r12          0.93882E-03      18   0.65908E-08   0.29809E-09 0.60201E+00 
c  r13          0.46679E-02      19   0.64004E-08   0.14943E-08 0.19896E+00 
c  r23          0.39980E-02      19   0.69710E-08   0.12539E-08 0.19546E+00 
c  epsilon      0.10969E+02      11   0.35237E-08   0.10008E-01 0.16636E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.84621E-02 0.43446E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63384         0.61376       0.0052571       0.0015073
v  Velocity[Y]            -0.57357         0.54379       0.0030778      0.00087199
v  Velocity[Z]              1.5657          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4414          4.3406          4.3632
v  Pressure                -36.399          360.05          87.667          169.88
v  r11                   0.0010626        0.081824        0.013077        0.018287
v  r22                   0.0011165        0.082602        0.013357        0.018647
v  r33                   0.0016454         0.17432        0.027257        0.037209
v  r12                   -0.010658        0.013602     -0.00023389     -0.00030935
v  r13                   -0.045504        0.052778      9.3406e-05       0.0010139
v  r23                   -0.046717        0.051203      3.0604e-05      0.00057466
v  epsilon                0.069785          271.14          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9917e-05       0.0099178       0.0009254       0.0017429
v  CourantNb               0.44248             0.6         0.59908         0.59839
v  FourierNb              0.001792          5.2767         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767         0.71353         0.85284


 TIME FOR THE TIME STEP            11277:        0.18723E+03

===============================================================


 INSTANT    0.112780000E-01   TIME STEP NUMBER           11278
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.120994147E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188135636E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.156176747E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.804702831E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.145125338E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81395E-03   0.44746E-02 0.19813E+01 
c  Velocity[X]                                      0.13676E-03 
c  Velocity[Y]                                      0.12650E-03 
c  Velocity[Z]                                      0.42113E-02 
c  Pressure     0.36195E-04     132   0.92093E-02   0.25529E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55600E-08   0.16025E-08 0.97832E-01 
c  r22          0.10853E-01      13   0.52679E-08   0.18080E-08 0.10006E+00 
c  r33          0.21862E-01      15   0.63852E-08   0.12433E-07 0.12603E+00 
c  r12          0.93882E-03      18   0.53698E-08   0.29720E-09 0.60167E+00 
c  r13          0.46679E-02      19   0.56352E-08   0.14872E-08 0.19854E+00 
c  r23          0.39980E-02      19   0.61625E-08   0.12730E-08 0.19724E+00 
c  epsilon      0.10969E+02      11   0.35268E-08   0.99458E-02 0.16518E+00 
c  TempC        0.25716E+06      16   0.15134E-04   0.83384E-02 0.43113E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63389         0.61384       0.0052571       0.0015074
v  Velocity[Y]            -0.57353          0.5439       0.0030778      0.00087197
v  Velocity[Z]              1.5655          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4414          4.3406          4.3632
v  Pressure                -36.419          359.98          87.619          169.81
v  r11                   0.0010626        0.081825        0.013077        0.018287
v  r22                   0.0011165        0.082603        0.013357        0.018647
v  r33                   0.0016454         0.17434        0.027257        0.037209
v  r12                   -0.010658        0.013602     -0.00023389     -0.00030935
v  r13                   -0.045506         0.05278      9.3406e-05       0.0010139
v  r23                   -0.046717        0.051195      3.0604e-05      0.00057466
v  epsilon                0.069787          271.17          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099178      0.00092541       0.0017429
v  CourantNb                0.4425             0.6         0.59908         0.59839
v  FourierNb              0.001792          5.2771         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71353         0.85284


 TIME FOR THE TIME STEP            11278:        0.66239E+02

===============================================================


 INSTANT    0.112790000E-01   TIME STEP NUMBER           11279
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.904135914E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.367639548E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.242249463E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.267044087E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.179980773E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81184E-03   0.45311E-02 0.19908E+01 
c  Velocity[X]                                      0.13699E-03 
c  Velocity[Y]                                      0.12817E-03 
c  Velocity[Z]                                      0.42659E-02 
c  Pressure     0.36481E-04     131   0.92841E-02   0.25731E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54746E-08   0.16325E-08 0.98728E-01 
c  r22          0.10853E-01      13   0.54971E-08   0.17961E-08 0.99875E-01 
c  r33          0.21862E-01      15   0.65810E-08   0.12430E-07 0.12595E+00 
c  r12          0.93882E-03      18   0.52913E-08   0.29126E-09 0.59855E+00 
c  r13          0.46679E-02      19   0.58040E-08   0.14838E-08 0.19800E+00 
c  r23          0.39980E-02      19   0.59867E-08   0.12777E-08 0.19748E+00 
c  epsilon      0.10969E+02      11   0.35379E-08   0.98032E-02 0.16382E+00 
c  TempC        0.25716E+06      16   0.15153E-04   0.84265E-02 0.43253E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162016


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61383       0.0052571       0.0015073
v  Velocity[Y]            -0.57363         0.54406       0.0030778      0.00087199
v  Velocity[Z]              1.5655          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4414          4.3406          4.3632
v  Pressure                  -36.4          359.97          87.608          169.81
v  r11                   0.0010626        0.081838        0.013077        0.018287
v  r22                   0.0011165        0.082596        0.013357        0.018647
v  r33                   0.0016455         0.17435        0.027257        0.037209
v  r12                   -0.010659        0.013607     -0.00023389     -0.00030935
v  r13                   -0.045504         0.05278      9.3406e-05       0.0010139
v  r23                   -0.046716        0.051191      3.0603e-05      0.00057466
v  epsilon                0.069788          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9922e-05       0.0099176      0.00092541       0.0017429
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb              0.001792          5.2768         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8768         0.71353         0.85284


 TIME FOR THE TIME STEP            11279:        0.65670E+02

===============================================================


 INSTANT    0.112800000E-01   TIME STEP NUMBER           11280
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.200843645E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934958E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.129658951E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.235776747E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.841232899E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934931E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.157737295E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81365E-03   0.44634E-02 0.19781E+01 
c  Velocity[X]                                      0.13645E-03 
c  Velocity[Y]                                      0.12803E-03 
c  Velocity[Z]                                      0.41990E-02 
c  Pressure     0.36191E-04     131   0.92189E-02   0.25527E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.49634E-08   0.16345E-08 0.98822E-01 
c  r22          0.10853E-01      13   0.53718E-08   0.17606E-08 0.99500E-01 
c  r33          0.21862E-01      15   0.65930E-08   0.12367E-07 0.12615E+00 
c  r12          0.93882E-03      17   0.70322E-08   0.28958E-09 0.59806E+00 
c  r13          0.46679E-02      19   0.57639E-08   0.14639E-08 0.19781E+00 
c  r23          0.39980E-02      19   0.59495E-08   0.12836E-08 0.19819E+00 
c  epsilon      0.10969E+02      11   0.34971E-08   0.98617E-02 0.16758E+00 
c  TempC        0.25716E+06      16   0.15177E-04   0.84282E-02 0.43329E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63405         0.61378       0.0052572       0.0015074
v  Velocity[Y]             -0.5734         0.54374       0.0030777      0.00087196
v  Velocity[Z]              1.5657          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5795          5.4414          4.3406          4.3632
v  Pressure                 -36.46          360.04          87.667          169.87
v  r11                   0.0010626        0.081851        0.013077        0.018287
v  r22                   0.0011165        0.082599        0.013357        0.018647
v  r33                   0.0016455         0.17436        0.027257        0.037209
v  r12                   -0.010662        0.013605     -0.00023389     -0.00030935
v  r13                   -0.045503        0.052777      9.3406e-05       0.0010139
v  r23                   -0.046716        0.051218      3.0603e-05      0.00057466
v  epsilon                0.069789          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9921e-05       0.0099176      0.00092541       0.0017429
v  CourantNb               0.44247             0.6         0.59908         0.59839
v  FourierNb              0.001792          5.2771         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71353         0.85284


 TIME FOR THE TIME STEP            11280:        0.66988E+02

===============================================================


 INSTANT    0.112810000E-01   TIME STEP NUMBER           11281
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.957140122E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.406064529E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.171386128E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.188198409E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.792308470E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81291E-03   0.45080E-02 0.19887E+01 
c  Velocity[X]                                      0.13724E-03 
c  Velocity[Y]                                      0.12652E-03 
c  Velocity[Z]                                      0.42442E-02 
c  Pressure     0.36598E-04     132   0.93121E-02   0.25813E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54619E-08   0.16337E-08 0.98636E-01 
c  r22          0.10853E-01      13   0.54024E-08   0.18291E-08 0.10066E+00 
c  r33          0.21862E-01      15   0.59792E-08   0.12571E-07 0.12665E+00 
c  r12          0.93882E-03      18   0.56490E-08   0.29854E-09 0.60251E+00 
c  r13          0.46679E-02      19   0.61505E-08   0.15118E-08 0.19938E+00 
c  r23          0.39980E-02      19   0.62600E-08   0.12766E-08 0.19692E+00 
c  epsilon      0.10969E+02      11   0.32843E-08   0.98593E-02 0.16463E+00 
c  TempC        0.25716E+06      16   0.15141E-04   0.83504E-02 0.43162E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161998


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63409         0.61383       0.0052571       0.0015073
v  Velocity[Y]            -0.57335         0.54378       0.0030778      0.00087196
v  Velocity[Z]              1.5655          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4414          4.3406          4.3632
v  Pressure                -36.396          360.09          87.679           169.9
v  r11                   0.0010626        0.081869        0.013077        0.018287
v  r22                   0.0011165          0.0826        0.013357        0.018647
v  r33                   0.0016455         0.17437        0.027257        0.037209
v  r12                   -0.010662        0.013607     -0.00023389     -0.00030935
v  r13                   -0.045507         0.05277      9.3406e-05       0.0010139
v  r23                   -0.046716         0.05121      3.0603e-05      0.00057466
v  epsilon                0.069791          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.992e-05       0.0099176      0.00092541       0.0017429
v  CourantNb               0.44241             0.6         0.59908         0.59839
v  FourierNb             0.0017921          5.2771         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8771         0.71353         0.85284


 TIME FOR THE TIME STEP            11281:        0.67501E+02

===============================================================


 INSTANT    0.112820000E-01   TIME STEP NUMBER           11282
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.100751791E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.946082826E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.279072148E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294543752E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934939E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.386231483E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934960E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      45   0.81303E-03   0.45181E-02 0.19923E+01 
c  Velocity[X]                                      0.13683E-03 
c  Velocity[Y]                                      0.12754E-03 
c  Velocity[Z]                                      0.42537E-02 
c  Pressure     0.36082E-04     131   0.91885E-02   0.25449E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53933E-08   0.16160E-08 0.98295E-01 
c  r22          0.10853E-01      13   0.52389E-08   0.18154E-08 0.10036E+00 
c  r33          0.21862E-01      15   0.52623E-08   0.12340E-07 0.12575E+00 
c  r12          0.93882E-03      18   0.57155E-08   0.29284E-09 0.59905E+00 
c  r13          0.46679E-02      19   0.64451E-08   0.14698E-08 0.19821E+00 
c  r23          0.39980E-02      19   0.65012E-08   0.12503E-08 0.19547E+00 
c  epsilon      0.10969E+02      11   0.32271E-08   0.95599E-02 0.16234E+00 
c  TempC        0.25716E+06      16   0.15150E-04   0.84134E-02 0.43269E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63411         0.61381        0.005257       0.0015073
v  Velocity[Y]            -0.57332         0.54393       0.0030777      0.00087196
v  Velocity[Z]              1.5656          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4414          4.3406          4.3632
v  Pressure                -36.469          359.96          87.624           169.8
v  r11                   0.0010626         0.08188        0.013077        0.018287
v  r22                   0.0011165        0.082599        0.013357        0.018647
v  r33                   0.0016455         0.17433        0.027257        0.037209
v  r12                   -0.010661        0.013609     -0.00023389     -0.00030935
v  r13                   -0.045504        0.052768      9.3407e-05       0.0010139
v  r23                   -0.046715        0.051189      3.0602e-05      0.00057466
v  epsilon                0.069792          271.15          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9918e-05       0.0099176      0.00092541       0.0017429
v  CourantNb               0.44244             0.6         0.59908         0.59839
v  FourierNb             0.0017921          5.2769         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71353         0.85284


 TIME FOR THE TIME STEP            11282:        0.68462E+02

===============================================================


 INSTANT    0.112830000E-01   TIME STEP NUMBER           11283
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.926841641E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.646788170E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934945E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.482759517E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.211076062E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.212569560E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81326E-03   0.45032E-02 0.19853E+01 
c  Velocity[X]                                      0.13703E-03 
c  Velocity[Y]                                      0.12821E-03 
c  Velocity[Z]                                      0.42380E-02 
c  Pressure     0.36100E-04     136   0.91883E-02   0.25462E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55300E-08   0.16322E-08 0.98529E-01 
c  r22          0.10853E-01      13   0.54394E-08   0.17856E-08 0.99741E-01 
c  r33          0.21862E-01      15   0.59165E-08   0.12381E-07 0.12576E+00 
c  r12          0.93882E-03      18   0.56835E-08   0.28961E-09 0.59819E+00 
c  r13          0.46679E-02      19   0.63867E-08   0.14705E-08 0.19783E+00 
c  r23          0.39980E-02      19   0.67642E-08   0.12802E-08 0.19689E+00 
c  epsilon      0.10969E+02      11   0.32855E-08   0.97330E-02 0.16425E+00 
c  TempC        0.25716E+06      16   0.15116E-04   0.84205E-02 0.43309E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161997


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63394         0.61378       0.0052571       0.0015073
v  Velocity[Y]            -0.57342         0.54373       0.0030778      0.00087198
v  Velocity[Z]              1.5655          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4414          4.3406          4.3632
v  Pressure                -36.413          360.06          87.682          169.89
v  r11                   0.0010626        0.081886        0.013077        0.018287
v  r22                   0.0011166        0.082598        0.013357        0.018647
v  r33                   0.0016455          0.1743        0.027257        0.037209
v  r12                   -0.010663        0.013607     -0.00023389     -0.00030935
v  r13                   -0.045503        0.052766      9.3407e-05       0.0010139
v  r23                   -0.046715        0.051178      3.0602e-05      0.00057466
v  epsilon                0.069793          271.16          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9917e-05       0.0099176      0.00092541       0.0017429
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017921          5.2773         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71353         0.85284


 TIME FOR THE TIME STEP            11283:        0.66134E+02

===============================================================


 INSTANT    0.112840000E-01   TIME STEP NUMBER           11284
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.436273101E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934949E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.882566751E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.315802290E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.775328169E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.716806208E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11247E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81314E-03   0.44837E-02 0.19810E+01 
c  Velocity[X]                                      0.13647E-03 
c  Velocity[Y]                                      0.12748E-03 
c  Velocity[Z]                                      0.42197E-02 
c  Pressure     0.36468E-04     133   0.92900E-02   0.25721E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55464E-08   0.16507E-08 0.98857E-01 
c  r22          0.10853E-01      13   0.53188E-08   0.18443E-08 0.10079E+00 
c  r33          0.21862E-01      15   0.68463E-08   0.12699E-07 0.12690E+00 
c  r12          0.93882E-03      18   0.58886E-08   0.29177E-09 0.59707E+00 
c  r13          0.46679E-02      19   0.73690E-08   0.14930E-08 0.19865E+00 
c  r23          0.39980E-02      20   0.59009E-08   0.12783E-08 0.19747E+00 
c  epsilon      0.10969E+02      11   0.33866E-08   0.10211E-01 0.16750E+00 
c  TempC        0.25716E+06      16   0.15186E-04   0.83556E-02 0.43182E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63395         0.61383        0.005257       0.0015073
v  Velocity[Y]            -0.57347         0.54387       0.0030777      0.00087194
v  Velocity[Z]              1.5653          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4414          4.3406          4.3632
v  Pressure                -36.456          360.02          87.644          169.85
v  r11                   0.0010626        0.081891        0.013077        0.018287
v  r22                   0.0011166        0.082597        0.013357        0.018647
v  r33                   0.0016455         0.17429        0.027257        0.037209
v  r12                   -0.010664        0.013602      -0.0002339     -0.00030935
v  r13                   -0.045506        0.052767      9.3407e-05       0.0010139
v  r23                   -0.046714        0.051194      3.0602e-05      0.00057466
v  epsilon                0.069795          271.18          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9914e-05       0.0099175      0.00092541       0.0017429
v  CourantNb               0.44231             0.6         0.59908         0.59839
v  FourierNb             0.0017922          5.2769         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8769         0.71352         0.85284


 TIME FOR THE TIME STEP            11284:        0.68451E+02

===============================================================


 INSTANT    0.112850000E-01   TIME STEP NUMBER           11285
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.811799461E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.371122926E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934980E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.272290530E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934984E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.147078482E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934967E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.182776890E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12295E+00 0.33840E+00
   Friction velocity        uk    :  0.11555E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81268E-03   0.45327E-02 0.19921E+01 
c  Velocity[X]                                      0.13797E-03 
c  Velocity[Y]                                      0.12731E-03 
c  Velocity[Z]                                      0.42674E-02 
c  Pressure     0.36352E-04     132   0.92591E-02   0.25640E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.57634E-08   0.16395E-08 0.99199E-01 
c  r22          0.10853E-01      13   0.57149E-08   0.18362E-08 0.10078E+00 
c  r33          0.21862E-01      15   0.62414E-08   0.12543E-07 0.12666E+00 
c  r12          0.93882E-03      18   0.66561E-08   0.30188E-09 0.60487E+00 
c  r13          0.46679E-02      19   0.66457E-08   0.15017E-08 0.19892E+00 
c  r23          0.39980E-02      19   0.67296E-08   0.12827E-08 0.19766E+00 
c  epsilon      0.10969E+02      11   0.33033E-08   0.99377E-02 0.16469E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.83906E-02 0.43211E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161999


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63385         0.61381       0.0052571       0.0015074
v  Velocity[Y]            -0.57362         0.54407       0.0030777      0.00087194
v  Velocity[Z]              1.5654          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4414          4.3406          4.3632
v  Pressure                -36.438          360.03           87.63          169.85
v  r11                   0.0010626        0.081887        0.013077        0.018287
v  r22                   0.0011166        0.082596        0.013357        0.018647
v  r33                   0.0016455          0.1743        0.027257        0.037209
v  r12                   -0.010661        0.013603      -0.0002339     -0.00030935
v  r13                   -0.045505        0.052767      9.3407e-05       0.0010139
v  r23                   -0.046714        0.051192      3.0601e-05      0.00057466
v  epsilon                0.069796          271.19          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9913e-05       0.0099175      0.00092541       0.0017429
v  CourantNb                0.4424             0.6         0.59908         0.59839
v  FourierNb             0.0017922          5.2773         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8773         0.71353         0.85285


 TIME FOR THE TIME STEP            11285:        0.70275E+02

===============================================================


 INSTANT    0.112860000E-01   TIME STEP NUMBER           11286
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.410554008E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934968E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.203884361E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.331023824E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.169773117E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934935E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.408795797E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11554E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15634E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81349E-03   0.44819E-02 0.19834E+01 
c  Velocity[X]                                      0.13690E-03 
c  Velocity[Y]                                      0.12757E-03 
c  Velocity[Z]                                      0.42174E-02 
c  Pressure     0.35987E-04     132   0.91565E-02   0.25382E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54229E-08   0.16436E-08 0.99487E-01 
c  r22          0.10853E-01      13   0.56741E-08   0.17726E-08 0.10021E+00 
c  r33          0.21862E-01      15   0.58907E-08   0.12272E-07 0.12635E+00 
c  r12          0.93882E-03      18   0.65580E-08   0.29322E-09 0.60148E+00 
c  r13          0.46679E-02      19   0.67148E-08   0.14538E-08 0.19831E+00 
c  r23          0.39980E-02      20   0.60233E-08   0.12870E-08 0.19899E+00 
c  epsilon      0.10969E+02      11   0.33044E-08   0.98813E-02 0.16975E+00 
c  TempC        0.25716E+06      16   0.15146E-04   0.83999E-02 0.43193E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63393         0.61377       0.0052571       0.0015074
v  Velocity[Y]            -0.57351         0.54379       0.0030777      0.00087195
v  Velocity[Z]              1.5654          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4414          4.3406          4.3632
v  Pressure                -36.493          359.94          87.616          169.79
v  r11                   0.0010626        0.081892        0.013077        0.018287
v  r22                   0.0011166        0.082593        0.013357        0.018647
v  r33                   0.0016455         0.17432        0.027257        0.037209
v  r12                   -0.010664        0.013607      -0.0002339     -0.00030935
v  r13                   -0.045503        0.052764      9.3407e-05       0.0010139
v  r23                   -0.046715        0.051185      3.0601e-05      0.00057465
v  epsilon                0.069797          271.15          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9911e-05       0.0099174      0.00092541       0.0017429
v  CourantNb               0.44246             0.6         0.59908         0.59839
v  FourierNb             0.0017922          5.2763         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8763         0.71353         0.85284


 TIME FOR THE TIME STEP            11286:        0.69418E+02

===============================================================


 INSTANT    0.112870000E-01   TIME STEP NUMBER           11287
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.260363123E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934924E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.475935607E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.282948334E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.104183354E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.390189744E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934987E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15633E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81322E-03   0.44726E-02 0.19815E+01 
c  Velocity[X]                                      0.13660E-03 
c  Velocity[Y]                                      0.12787E-03 
c  Velocity[Z]                                      0.42081E-02 
c  Pressure     0.36761E-04     131   0.93584E-02   0.25928E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.59764E-08   0.16183E-08 0.98701E-01 
c  r22          0.10853E-01      13   0.58819E-08   0.18260E-08 0.10100E+00 
c  r33          0.21862E-01      15   0.67188E-08   0.12423E-07 0.12652E+00 
c  r12          0.93882E-03      19   0.56715E-08   0.28999E-09 0.59697E+00 
c  r13          0.46679E-02      19   0.74255E-08   0.14876E-08 0.19887E+00 
c  r23          0.39980E-02      19   0.70880E-08   0.12580E-08 0.19669E+00 
c  epsilon      0.10969E+02      11   0.33906E-08   0.97242E-02 0.16507E+00 
c  TempC        0.25716E+06      16   0.15136E-04   0.84008E-02 0.43196E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162003


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63388         0.61385       0.0052571       0.0015074
v  Velocity[Y]            -0.57353          0.5438       0.0030777      0.00087197
v  Velocity[Z]              1.5655          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4414          4.3406          4.3632
v  Pressure                -36.413          360.04          87.641          169.85
v  r11                   0.0010626        0.081897        0.013077        0.018287
v  r22                   0.0011166        0.082591        0.013357        0.018647
v  r33                   0.0016455         0.17434        0.027257        0.037209
v  r12                   -0.010666        0.013611      -0.0002339     -0.00030935
v  r13                   -0.045506        0.052762      9.3406e-05       0.0010139
v  r23                   -0.046715        0.051209      3.0601e-05      0.00057465
v  epsilon                0.069799          271.17          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.991e-05       0.0099175      0.00092541       0.0017429
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017922          5.2767         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767         0.71352         0.85284


 TIME FOR THE TIME STEP            11287:        0.71634E+02

===============================================================


 INSTANT    0.112880000E-01   TIME STEP NUMBER           11288
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.499310611E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.146428603E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.286542600E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.660230375E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934936E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.190725793E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81254E-03   0.45403E-02 0.19930E+01 
c  Velocity[X]                                      0.13639E-03 
c  Velocity[Y]                                      0.12771E-03 
c  Velocity[Z]                                      0.42762E-02 
c  Pressure     0.35977E-04     132   0.91602E-02   0.25376E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55309E-08   0.16056E-08 0.97868E-01 
c  r22          0.10853E-01      13   0.56404E-08   0.18352E-08 0.10082E+00 
c  r33          0.21862E-01      15   0.64431E-08   0.12408E-07 0.12578E+00 
c  r12          0.93882E-03      19   0.55471E-08   0.29767E-09 0.60463E+00 
c  r13          0.46679E-02      20   0.58109E-08   0.15030E-08 0.19907E+00 
c  r23          0.39980E-02      19   0.68383E-08   0.12569E-08 0.19603E+00 
c  epsilon      0.10969E+02      11   0.34118E-08   0.98753E-02 0.16483E+00 
c  TempC        0.25716E+06      16   0.15166E-04   0.84227E-02 0.43350E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63374         0.61384       0.0052571       0.0015074
v  Velocity[Y]            -0.57346         0.54396       0.0030776      0.00087192
v  Velocity[Z]              1.5654          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4414          4.3406          4.3632
v  Pressure                -36.484          360.04           87.66          169.86
v  r11                   0.0010626        0.081901        0.013077        0.018287
v  r22                   0.0011166        0.082589        0.013357        0.018647
v  r33                   0.0016455         0.17436        0.027257        0.037209
v  r12                   -0.010664        0.013608      -0.0002339     -0.00030935
v  r13                   -0.045503        0.052764      9.3406e-05       0.0010139
v  r23                   -0.046715        0.051202      3.0601e-05      0.00057465
v  epsilon                  0.0698          271.22          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9905e-05       0.0099175      0.00092541       0.0017429
v  CourantNb               0.44224             0.6         0.59908         0.59839
v  FourierNb             0.0017923          5.2776         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8776         0.71353         0.85285


 TIME FOR THE TIME STEP            11288:        0.73588E+02

===============================================================


 INSTANT    0.112890000E-01   TIME STEP NUMBER           11289
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.171101975E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.240227026E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934977E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.608446695E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.480661777E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.294146972E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69767E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81257E-03   0.44977E-02 0.19854E+01 
c  Velocity[X]                                      0.13758E-03 
c  Velocity[Y]                                      0.12825E-03 
c  Velocity[Z]                                      0.42319E-02 
c  Pressure     0.36159E-04     132   0.92009E-02   0.25504E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52361E-08   0.16306E-08 0.98900E-01 
c  r22          0.10853E-01      13   0.54409E-08   0.17951E-08 0.10014E+00 
c  r33          0.21862E-01      15   0.63768E-08   0.12376E-07 0.12617E+00 
c  r12          0.93882E-03      18   0.71588E-08   0.29484E-09 0.60238E+00 
c  r13          0.46679E-02      20   0.66318E-08   0.14795E-08 0.19870E+00 
c  r23          0.39980E-02      20   0.56218E-08   0.12707E-08 0.19723E+00 
c  epsilon      0.10969E+02      11   0.34769E-08   0.97527E-02 0.16383E+00 
c  TempC        0.25716E+06      16   0.15162E-04   0.84278E-02 0.43344E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162012


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63367         0.61378       0.0052571       0.0015074
v  Velocity[Y]            -0.57358          0.5441       0.0030777      0.00087196
v  Velocity[Z]              1.5654          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4414          4.3406          4.3632
v  Pressure                -36.441          360.04          87.643          169.86
v  r11                   0.0010626        0.081906        0.013077        0.018287
v  r22                   0.0011166        0.082586        0.013357        0.018647
v  r33                   0.0016455         0.17438        0.027257        0.037209
v  r12                   -0.010662        0.013605      -0.0002339     -0.00030935
v  r13                   -0.045504        0.052764      9.3406e-05       0.0010139
v  r23                   -0.046715        0.051185        3.06e-05      0.00057465
v  epsilon                0.069801          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9903e-05       0.0099175      0.00092541       0.0017429
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017923          5.2781         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8781         0.71353         0.85284


 TIME FOR THE TIME STEP            11289:        0.74899E+02

===============================================================


 INSTANT    0.112900000E-01   TIME STEP NUMBER           11290
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.459148252E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934969E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.252040335E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934930E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.449556950E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.961632938E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934934E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.240209315E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81386E-03   0.44926E-02 0.19832E+01 
c  Velocity[X]                                      0.13652E-03 
c  Velocity[Y]                                      0.12682E-03 
c  Velocity[Z]                                      0.42292E-02 
c  Pressure     0.36400E-04     132   0.92651E-02   0.25674E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.51438E-08   0.16252E-08 0.98806E-01 
c  r22          0.10853E-01      13   0.56459E-08   0.17919E-08 0.10021E+00 
c  r33          0.21862E-01      15   0.59723E-08   0.12298E-07 0.12602E+00 
c  r12          0.93882E-03      18   0.66791E-08   0.29086E-09 0.59883E+00 
c  r13          0.46679E-02      20   0.55879E-08   0.14580E-08 0.19784E+00 
c  r23          0.39980E-02      19   0.66511E-08   0.12762E-08 0.19755E+00 
c  epsilon      0.10969E+02      11   0.31798E-08   0.96294E-02 0.16379E+00 
c  TempC        0.25716E+06      16   0.15143E-04   0.83478E-02 0.43044E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162011


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63369         0.61384       0.0052572       0.0015074
v  Velocity[Y]            -0.57341         0.54376       0.0030777      0.00087195
v  Velocity[Z]              1.5654          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4414          4.3406          4.3632
v  Pressure                -36.494          360.03          87.652          169.85
v  r11                   0.0010626        0.081898        0.013077        0.018287
v  r22                   0.0011166        0.082586        0.013357        0.018647
v  r33                   0.0016456         0.17439        0.027257        0.037209
v  r12                   -0.010665        0.013596      -0.0002339     -0.00030935
v  r13                   -0.045507        0.052763      9.3405e-05       0.0010139
v  r23                   -0.046716        0.051206      3.0599e-05      0.00057465
v  epsilon                0.069803          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9897e-05       0.0099175      0.00092541       0.0017429
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017923          5.2782         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8782         0.71352         0.85284


 TIME FOR THE TIME STEP            11290:        0.76844E+02

===============================================================


 INSTANT    0.112910000E-01   TIME STEP NUMBER           11291
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.237168349E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934940E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.247011405E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.662284869E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.420013357E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934955E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.346966637E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12294E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15629E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81246E-03   0.45029E-02 0.19876E+01 
c  Velocity[X]                                      0.13730E-03 
c  Velocity[Y]                                      0.12754E-03 
c  Velocity[Z]                                      0.42381E-02 
c  Pressure     0.36184E-04     132   0.92129E-02   0.25522E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53287E-08   0.16315E-08 0.98787E-01 
c  r22          0.10853E-01      13   0.58211E-08   0.18129E-08 0.10050E+00 
c  r33          0.21862E-01      15   0.64372E-08   0.12478E-07 0.12646E+00 
c  r12          0.93882E-03      18   0.71298E-08   0.29550E-09 0.60044E+00 
c  r13          0.46679E-02      20   0.59092E-08   0.14932E-08 0.19865E+00 
c  r23          0.39980E-02      19   0.59915E-08   0.12762E-08 0.19713E+00 
c  epsilon      0.10969E+02      11   0.33008E-08   0.97937E-02 0.16421E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.84197E-02 0.43258E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63375         0.61382       0.0052572       0.0015074
v  Velocity[Y]            -0.57349         0.54378       0.0030777      0.00087198
v  Velocity[Z]              1.5653          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4414          4.3406          4.3632
v  Pressure                -36.419          360.06          87.667          169.88
v  r11                   0.0010626        0.081904        0.013077        0.018287
v  r22                   0.0011166        0.082588        0.013357        0.018647
v  r33                   0.0016456         0.17434        0.027257        0.037209
v  r12                    -0.01067        0.013585      -0.0002339     -0.00030935
v  r13                   -0.045504        0.052764      9.3406e-05       0.0010139
v  r23                   -0.046716        0.051195      3.0599e-05      0.00057465
v  epsilon                0.069804          271.23          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9892e-05       0.0099175      0.00092541       0.0017429
v  CourantNb               0.44239             0.6         0.59908         0.59839
v  FourierNb             0.0017924          5.2772         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71353         0.85284


 TIME FOR THE TIME STEP            11291:        0.74890E+02

===============================================================


 INSTANT    0.112920000E-01   TIME STEP NUMBER           11292
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.110939720E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.594312197E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934985E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.149383943E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.369523016E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934971E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.711322059E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11551E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81293E-03   0.45005E-02 0.19877E+01 
c  Velocity[X]                                      0.13756E-03 
c  Velocity[Y]                                      0.12817E-03 
c  Velocity[Z]                                      0.42348E-02 
c  Pressure     0.36033E-04     133   0.91762E-02   0.25414E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.60356E-08   0.16222E-08 0.98363E-01 
c  r22          0.10853E-01      13   0.54302E-08   0.18147E-08 0.10042E+00 
c  r33          0.21862E-01      15   0.53496E-08   0.12514E-07 0.12658E+00 
c  r12          0.93882E-03      18   0.71494E-08   0.29303E-09 0.59775E+00 
c  r13          0.46679E-02      19   0.74390E-08   0.14875E-08 0.19882E+00 
c  r23          0.39980E-02      19   0.63555E-08   0.12914E-08 0.19822E+00 
c  epsilon      0.10969E+02      11   0.34335E-08   0.10223E-01 0.17075E+00 
c  TempC        0.25716E+06      16   0.15175E-04   0.83534E-02 0.43120E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162002


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63354         0.61379       0.0052572       0.0015074
v  Velocity[Y]             -0.5734         0.54393       0.0030777      0.00087195
v  Velocity[Z]              1.5653          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4414          4.3406          4.3632
v  Pressure                -36.474          359.97          87.596          169.79
v  r11                   0.0010626          0.0819        0.013077        0.018287
v  r22                   0.0011166        0.082589        0.013357        0.018647
v  r33                   0.0016456          0.1743        0.027257        0.037209
v  r12                    -0.01067        0.013585      -0.0002339     -0.00030935
v  r13                   -0.045503        0.052761      9.3405e-05       0.0010139
v  r23                   -0.046716        0.051187      3.0599e-05      0.00057465
v  epsilon                0.069805          271.26          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9887e-05       0.0099175      0.00092541       0.0017429
v  CourantNb               0.44236             0.6         0.59908         0.59839
v  FourierNb             0.0017924          5.2767         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8767         0.71353         0.85284


 TIME FOR THE TIME STEP            11292:        0.74924E+02

===============================================================


 INSTANT    0.112930000E-01   TIME STEP NUMBER           11293
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.136151440E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.225984599E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934927E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.269365830E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934975E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.459982807E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.187046160E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15630E+02 0.40350E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81341E-03   0.44930E-02 0.19820E+01 
c  Velocity[X]                                      0.13629E-03 
c  Velocity[Y]                                      0.12656E-03 
c  Velocity[Z]                                      0.42302E-02 
c  Pressure     0.36263E-04     131   0.92305E-02   0.25577E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.62015E-08   0.16291E-08 0.98282E-01 
c  r22          0.10853E-01      13   0.54887E-08   0.18075E-08 0.10000E+00 
c  r33          0.21862E-01      15   0.54930E-08   0.12420E-07 0.12584E+00 
c  r12          0.93882E-03      19   0.55122E-08   0.29775E-09 0.60096E+00 
c  r13          0.46679E-02      19   0.69299E-08   0.14897E-08 0.19829E+00 
c  r23          0.39980E-02      19   0.57932E-08   0.12857E-08 0.19725E+00 
c  epsilon      0.10969E+02      11   0.34845E-08   0.98784E-02 0.16482E+00 
c  TempC        0.25716E+06      16   0.15132E-04   0.83181E-02 0.43075E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162017


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63358         0.61385       0.0052571       0.0015075
v  Velocity[Y]            -0.57354         0.54406       0.0030777      0.00087192
v  Velocity[Z]              1.5655          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4414          4.3406          4.3632
v  Pressure                -36.441          360.04           87.66          169.87
v  r11                   0.0010627        0.081887        0.013077        0.018287
v  r22                   0.0011166        0.082588        0.013357        0.018647
v  r33                   0.0016456          0.1743        0.027257        0.037209
v  r12                   -0.010669         0.01358      -0.0002339     -0.00030935
v  r13                   -0.045507         0.05276      9.3405e-05       0.0010139
v  r23                   -0.046717        0.051213      3.0598e-05      0.00057465
v  epsilon                0.069806          271.28          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9883e-05       0.0099174      0.00092541       0.0017429
v  CourantNb               0.44242             0.6         0.59908         0.59839
v  FourierNb             0.0017924          5.2764         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8764         0.71352         0.85284


 TIME FOR THE TIME STEP            11293:        0.74762E+02

===============================================================


 INSTANT    0.112940000E-01   TIME STEP NUMBER           11294
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.488258732E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.167440220E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.467784338E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.186470137E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934942E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.572916744E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934989E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11248E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81253E-03   0.44803E-02 0.19833E+01 
c  Velocity[X]                                      0.13670E-03 
c  Velocity[Y]                                      0.12780E-03 
c  Velocity[Z]                                      0.42158E-02 
c  Pressure     0.36302E-04     131   0.92440E-02   0.25605E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.55482E-08   0.16062E-08 0.97960E-01 
c  r22          0.10853E-01      13   0.55528E-08   0.18023E-08 0.10004E+00 
c  r33          0.21862E-01      15   0.52427E-08   0.12329E-07 0.12572E+00 
c  r12          0.93882E-03      18   0.71735E-08   0.28971E-09 0.59723E+00 
c  r13          0.46679E-02      19   0.61639E-08   0.14777E-08 0.19842E+00 
c  r23          0.39980E-02      19   0.69039E-08   0.12594E-08 0.19574E+00 
c  epsilon      0.10969E+02      11   0.34529E-08   0.96573E-02 0.16443E+00 
c  TempC        0.25716E+06      16   0.15170E-04   0.84513E-02 0.43340E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162014


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63357         0.61383       0.0052572       0.0015075
v  Velocity[Y]            -0.57345         0.54384       0.0030776       0.0008719
v  Velocity[Z]              1.5655          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4414          4.3406          4.3632
v  Pressure                -36.469          359.94          87.601          169.78
v  r11                   0.0010627        0.081884        0.013077        0.018287
v  r22                   0.0011166        0.082586        0.013357        0.018647
v  r33                   0.0016456         0.17432        0.027257        0.037209
v  r12                   -0.010672        0.013587      -0.0002339     -0.00030935
v  r13                   -0.045504        0.052762      9.3404e-05       0.0010139
v  r23                   -0.046717        0.051187      3.0598e-05      0.00057465
v  epsilon                0.069808          271.27          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9879e-05       0.0099173      0.00092541       0.0017429
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017924          5.2772         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8772         0.71352         0.85284


 TIME FOR THE TIME STEP            11294:        0.85618E+02

===============================================================


 INSTANT    0.112950000E-01   TIME STEP NUMBER           11295
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.132278930E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.226538519E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934952E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.180194668E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.625582214E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934947E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.948290189E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21882E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69766E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81179E-03   0.45203E-02 0.19917E+01 
c  Velocity[X]                                      0.13749E-03 
c  Velocity[Y]                                      0.12763E-03 
c  Velocity[Z]                                      0.42552E-02 
c  Pressure     0.36071E-04     132   0.91854E-02   0.25442E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54047E-08   0.15982E-08 0.98201E-01 
c  r22          0.10853E-01      13   0.57684E-08   0.18208E-08 0.10045E+00 
c  r33          0.21862E-01      14   0.71082E-08   0.12338E-07 0.12595E+00 
c  r12          0.93882E-03      19   0.56165E-08   0.29485E-09 0.60316E+00 
c  r13          0.46679E-02      19   0.66472E-08   0.14713E-08 0.19797E+00 
c  r23          0.39980E-02      20   0.60611E-08   0.12378E-08 0.19519E+00 
c  epsilon      0.10969E+02      11   0.33273E-08   0.97367E-02 0.16409E+00 
c  TempC        0.25716E+06      16   0.15133E-04   0.84753E-02 0.43448E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162000


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63341         0.61379       0.0052572       0.0015075
v  Velocity[Y]            -0.57345         0.54394       0.0030777      0.00087196
v  Velocity[Z]              1.5653          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5791          5.4414          4.3406          4.3632
v  Pressure                -36.436          360.06          87.654          169.87
v  r11                   0.0010627        0.081872        0.013077        0.018287
v  r22                   0.0011166        0.082585        0.013357        0.018647
v  r33                   0.0016456         0.17434        0.027257        0.037209
v  r12                   -0.010672        0.013583      -0.0002339     -0.00030935
v  r13                   -0.045503         0.05276      9.3405e-05       0.0010139
v  r23                   -0.046717         0.05117      3.0598e-05      0.00057465
v  epsilon                0.069809          271.24          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9877e-05       0.0099175      0.00092541       0.0017429
v  CourantNb               0.44228             0.6         0.59908         0.59839
v  FourierNb             0.0017925          5.2775         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8775         0.71352         0.85284


 TIME FOR THE TIME STEP            11295:        0.10910E+03

===============================================================


 INSTANT    0.112960000E-01   TIME STEP NUMBER           11296
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.179032477E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.459518023E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934941E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.140249231E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.288402940E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934965E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.572868274E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934974E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40351E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81375E-03   0.44766E-02 0.19825E+01 
c  Velocity[X]                                      0.13692E-03 
c  Velocity[Y]                                      0.12617E-03 
c  Velocity[Z]                                      0.42135E-02 
c  Pressure     0.36426E-04     133   0.92740E-02   0.25692E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.53448E-08   0.16363E-08 0.98416E-01 
c  r22          0.10853E-01      13   0.60758E-08   0.18205E-08 0.10058E+00 
c  r33          0.21862E-01      15   0.52163E-08   0.12557E-07 0.12663E+00 
c  r12          0.93882E-03      18   0.73163E-08   0.30391E-09 0.60516E+00 
c  r13          0.46679E-02      19   0.66742E-08   0.14960E-08 0.19889E+00 
c  r23          0.39980E-02      20   0.59004E-08   0.12741E-08 0.19685E+00 
c  epsilon      0.10969E+02      11   0.33186E-08   0.10034E-01 0.16628E+00 
c  TempC        0.25716E+06      16   0.15169E-04   0.83333E-02 0.43097E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63352         0.61384       0.0052571       0.0015075
v  Velocity[Y]            -0.57344         0.54409       0.0030776      0.00087191
v  Velocity[Z]              1.5655          5.4415          4.3387          4.3625
v  ǁVelocityǁ               1.5793          5.4415          4.3406          4.3632
v  Pressure                -36.447          359.98          87.607           169.8
v  r11                   0.0010627        0.081869        0.013077        0.018287
v  r22                   0.0011166        0.082585        0.013357        0.018647
v  r33                   0.0016456         0.17435        0.027257        0.037209
v  r12                   -0.010668        0.013584      -0.0002339     -0.00030935
v  r13                   -0.045506        0.052761      9.3404e-05       0.0010139
v  r23                   -0.046716         0.05119      3.0597e-05      0.00057465
v  epsilon                 0.06981          271.25          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9872e-05       0.0099176      0.00092541       0.0017429
v  CourantNb               0.44232             0.6         0.59908         0.59839
v  FourierNb             0.0017925           5.278         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71353         0.85284


 TIME FOR THE TIME STEP            11296:        0.12970E+03

===============================================================


 INSTANT    0.112970000E-01   TIME STEP NUMBER           11297
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.760124423E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.122122760E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934943E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.147448367E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.511224022E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934962E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.291017641E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12297E+00 0.33840E+00
   Friction velocity        uk    :  0.11552E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15631E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69769E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10216E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      42   0.81255E-03   0.45080E-02 0.19880E+01 
c  Velocity[X]                                      0.13632E-03 
c  Velocity[Y]                                      0.12756E-03 
c  Velocity[Z]                                      0.42441E-02 
c  Pressure     0.36309E-04     132   0.92410E-02   0.25611E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.50342E-08   0.16133E-08 0.98047E-01 
c  r22          0.10853E-01      13   0.57806E-08   0.18073E-08 0.10007E+00 
c  r33          0.21862E-01      15   0.55459E-08   0.12373E-07 0.12569E+00 
c  r12          0.93882E-03      18   0.64058E-08   0.29476E-09 0.60131E+00 
c  r13          0.46679E-02      19   0.73482E-08   0.14791E-08 0.19797E+00 
c  r23          0.39980E-02      20   0.63122E-08   0.12776E-08 0.19718E+00 
c  epsilon      0.10969E+02      11   0.33547E-08   0.98031E-02 0.16381E+00 
c  TempC        0.25716E+06      16   0.15167E-04   0.83913E-02 0.43212E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162010


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63356         0.61382       0.0052571       0.0015075
v  Velocity[Y]             -0.5735         0.54398       0.0030777      0.00087195
v  Velocity[Z]              1.5654          5.4415          4.3387          4.3625
v  ǁVelocityǁ               1.5792          5.4415          4.3406          4.3632
v  Pressure                -36.424          359.95          87.594          169.79
v  r11                   0.0010627        0.081856        0.013077        0.018287
v  r22                   0.0011166        0.082581        0.013357        0.018647
v  r33                   0.0016456         0.17436        0.027257        0.037209
v  r12                   -0.010665         0.01358      -0.0002339     -0.00030935
v  r13                   -0.045506         0.05276      9.3404e-05       0.0010139
v  r23                   -0.046714        0.051179      3.0597e-05      0.00057465
v  epsilon                0.069812          271.29          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9871e-05       0.0099177      0.00092541       0.0017429
v  CourantNb               0.44227             0.6         0.59908         0.59839
v  FourierNb             0.0017925          5.2783         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8783         0.71353         0.85284


 TIME FOR THE TIME STEP            11297:        0.13588E+03

===============================================================


 INSTANT    0.112980000E-01   TIME STEP NUMBER           11298
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.111083924E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934959E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.540572852E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934953E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.756529189E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.927234635E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.153528361E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934978E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12296E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69768E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81352E-03   0.44915E-02 0.19845E+01 
c  Velocity[X]                                      0.13628E-03 
c  Velocity[Y]                                      0.12819E-03 
c  Velocity[Z]                                      0.42270E-02 
c  Pressure     0.36446E-04     132   0.92746E-02   0.25706E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54544E-08   0.16492E-08 0.98832E-01 
c  r22          0.10853E-01      13   0.55671E-08   0.18341E-08 0.10075E+00 
c  r33          0.21862E-01      15   0.62025E-08   0.12687E-07 0.12737E+00 
c  r12          0.93882E-03      18   0.63865E-08   0.30080E-09 0.60541E+00 
c  r13          0.46679E-02      19   0.69638E-08   0.14825E-08 0.19837E+00 
c  r23          0.39980E-02      19   0.60779E-08   0.13103E-08 0.20063E+00 
c  epsilon      0.10969E+02      11   0.34494E-08   0.10195E-01 0.17077E+00 
c  TempC        0.25716E+06      16   0.15148E-04   0.84591E-02 0.43309E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      161995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.6334         0.61377       0.0052572       0.0015075
v  Velocity[Y]            -0.57343         0.54395       0.0030776      0.00087192
v  Velocity[Z]              1.5657          5.4415          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4415          4.3406          4.3632
v  Pressure                -36.481             360          87.637          169.83
v  r11                   0.0010627        0.081839        0.013077        0.018287
v  r22                   0.0011166         0.08258        0.013357        0.018647
v  r33                   0.0016456         0.17437        0.027257        0.037209
v  r12                   -0.010665         0.01357      -0.0002339     -0.00030935
v  r13                   -0.045504        0.052755      9.3404e-05       0.0010139
v  r23                   -0.046712        0.051162      3.0597e-05      0.00057465
v  epsilon                0.069813          271.32          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.987e-05       0.0099178      0.00092541       0.0017429
v  CourantNb               0.44238             0.6         0.59908         0.59839
v  FourierNb             0.0017925          5.2777         0.11445         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71353         0.85285


 TIME FOR THE TIME STEP            11298:        0.20788E+03

===============================================================


 INSTANT    0.112990000E-01   TIME STEP NUMBER           11299
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.172414032E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934937E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.637326408E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934916E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.103581754E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.110546931E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934938E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.573594385E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934973E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40352E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration      11299, Physical time    0.11299E-01


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint/main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary
 End writing


 Time for restart files:    0.14443E+02



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      41   0.81201E-03   0.44707E-02 0.19814E+01 
c  Velocity[X]                                      0.13690E-03 
c  Velocity[Y]                                      0.12740E-03 
c  Velocity[Z]                                      0.42064E-02 
c  Pressure     0.36143E-04     131   0.92003E-02   0.25493E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.54022E-08   0.16026E-08 0.97811E-01 
c  r22          0.10853E-01      13   0.49589E-08   0.18169E-08 0.10051E+00 
c  r33          0.21862E-01      15   0.55313E-08   0.12353E-07 0.12571E+00 
c  r12          0.93882E-03      18   0.51450E-08   0.29659E-09 0.60388E+00 
c  r13          0.46679E-02      19   0.76287E-08   0.14918E-08 0.19850E+00 
c  r23          0.39980E-02      19   0.60483E-08   0.12605E-08 0.19612E+00 
c  epsilon      0.10969E+02      11   0.33949E-08   0.95967E-02 0.16263E+00 
c  TempC        0.25716E+06      16   0.15152E-04   0.84456E-02 0.43347E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162001


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63343         0.61384       0.0052571       0.0015075
v  Velocity[Y]            -0.57352         0.54404       0.0030776      0.00087192
v  Velocity[Z]              1.5656          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4414          4.3406          4.3632
v  Pressure                 -36.42          360.06          87.673          169.89
v  r11                   0.0010627        0.081832        0.013077        0.018287
v  r22                   0.0011166        0.082579        0.013357        0.018647
v  r33                   0.0016456         0.17438        0.027257        0.037209
v  r12                   -0.010666        0.013568      -0.0002339     -0.00030935
v  r13                   -0.045506        0.052753      9.3404e-05       0.0010139
v  r23                   -0.046712        0.051184      3.0596e-05      0.00057465
v  epsilon                0.069815          271.31          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc              5.987e-05       0.0099178      0.00092541       0.0017429
v  CourantNb               0.44234             0.6         0.59908         0.59839
v  FourierNb             0.0017926           5.278         0.11444         0.25445
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179           5.878         0.71352         0.85284


 TIME FOR THE TIME STEP            11299:        0.19872E+03

===============================================================


 INSTANT    0.113000000E-01   TIME STEP NUMBER           11300
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.952724452E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934944E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.161643908E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934956E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.250202675E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527935011E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150         0.262680083E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934954E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        5612        -0.527934962E+00
Smooth wall               5      358150        -0.739354337E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      143448         0.000000000E+00
Free outlet               3        5590         0.527934961E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11249E+01 0.31856E+01
   Friction velocity        uet   :  0.12298E+00 0.33840E+00
   Friction velocity        uk    :  0.11553E+00 0.21883E+00
   Dimensionless distance   yplus :  0.15632E+02 0.40353E+02
   Friction thermal sca.    tstar : -0.69770E+00 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+02 0.12685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     358150
------------------------------------------------------------




 Write final restart files
   checkpoint at iteration      11300, Physical time    0.11300E-01


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint/main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary
 End writing


 Time for restart files:    0.15557E+02



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36451E+01      43   0.81368E-03   0.45078E-02 0.19874E+01 
c  Velocity[X]                                      0.13668E-03 
c  Velocity[Y]                                      0.12674E-03 
c  Velocity[Z]                                      0.42444E-02 
c  Pressure     0.36368E-04     131   0.92611E-02   0.25651E-01 0.00000E+00 
c  r11          0.10586E-01      13   0.52114E-08   0.15757E-08 0.97163E-01 
c  r22          0.10853E-01      13   0.52392E-08   0.17773E-08 0.99706E-01 
c  r33          0.21862E-01      15   0.53069E-08   0.12107E-07 0.12477E+00 
c  r12          0.93882E-03      18   0.53569E-08   0.28562E-09 0.59335E+00 
c  r13          0.46679E-02      19   0.68930E-08   0.14468E-08 0.19667E+00 
c  r23          0.39980E-02      19   0.56936E-08   0.12484E-08 0.19539E+00 
c  epsilon      0.10969E+02      11   0.32928E-08   0.93930E-02 0.16132E+00 
c  TempC        0.25716E+06      16   0.15163E-04   0.83597E-02 0.43195E-01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon        
a  TempC          
a  Local Time Step                          0.0011                      162004


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.63347          0.6138       0.0052571       0.0015075
v  Velocity[Y]            -0.57348         0.54418       0.0030775      0.00087185
v  Velocity[Z]              1.5656          5.4414          4.3387          4.3625
v  ǁVelocityǁ               1.5794          5.4414          4.3406          4.3632
v  Pressure                -36.493          359.98          87.619          169.81
v  r11                   0.0010627        0.081824        0.013077        0.018287
v  r22                   0.0011166        0.082578        0.013357        0.018647
v  r33                   0.0016456         0.17439        0.027257        0.037209
v  r12                   -0.010668        0.013567      -0.0002339     -0.00030935
v  r13                   -0.045503        0.052755      9.3403e-05       0.0010139
v  r23                   -0.046711        0.051177      3.0596e-05      0.00057465
v  epsilon                0.069816          271.27          7.2637          7.8885
v  TempC                       300          311.66          300.73          300.29
v  Density                  32.018          32.718          32.674          32.701
v  LamVisc              2.6684e-05        2.71e-05      2.6711e-05      2.6695e-05
v  TurbVisc             5.9869e-05       0.0099178      0.00092541       0.0017429
v  CourantNb               0.44245             0.6         0.59908         0.59839
v  FourierNb             0.0017926          5.2777         0.11444         0.25444
v  total_pressure          3.5e+06      3.5004e+06      3.5001e+06      3.5002e+06
v  SpecHeat                 1093.3          1098.5          1093.6          1093.4
v  Local Time Step      1.7402e-06           0.001      0.00020961      0.00049497
v  ThermalCond            0.039465        0.040285        0.039516        0.039485

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          32.018          32.718          32.593          32.651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60179          5.8777         0.71352         0.85284


 TIME FOR THE TIME STEP            11300:        0.15584E+03

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.36999E-01
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:         125232.203 s
  System CPU time:         2311.227 s
  Total CPU time:      16635998.602 s

  Elapsed time:          128021.221 s
  CPU / elapsed time          0.996

Memory use summary:

  Total memory used:                              65.575 GiB
                             local minimum:      484.410 MiB  (rank 20)
                             local maximum:      781.637 MiB  (rank 96)
  Theoretical instrumented dynamic memory:        21.331 GiB
                             local minimum:      142.369 MiB  (rank 50)
                             local maximum:      485.672 MiB  (rank 96)
